In the second half of the 50s, the problem arose of replacing the Mi-1 helicopter with a newer and more advanced model, which became the Mi-2 helicopter. The designers' plans at first were simply to refine the old model, but for many reasons the Mil design bureau decided to develop a completely new machine, which was designed on the basis of the Mi-1. The most progressive decision of the designers was the use of two gas turbine engines in the new car, which had never been done before. This design of the power plant allowed for safer flights, since if one of the engines fails, the flight can be continued with one working one. All these innovations were included in a new design project called Mi-2.
Main goals
The aircraft was intended to perform the same tasks of transporting lightweight cargo as the Mi-1 did. The passenger version could transport 7 people and a pilot. In the role of a rescue aircraft, the Mi-2 helicopter can accommodate four stretchers and a medical worker. The vessel is capable of transporting cargo weighing up to 700 kg. As a flying crane or for rescue work, the aircraft can be equipped with a ventral hook for hanging loads of up to 800 kg or a winch above the cabin door capable of lifting up to 150 kg. The fourth main application that distinguishes the Mi-2 helicopter is operation in agriculture, for which it can be equipped with tanks located on both sides of the cabin, capable of holding 450 kg of dry chemicals or 500 liters of liquid. To perform other tasks, cargo tanks can be replaced with additional fuel tanks.
History of creation
The Mi-2 helicopter (see photo in the review) was produced at the WSK plant in Mielec in Poland. After negotiations began in January 1964, WSK received exclusive rights to manufacture the aircraft and its engines. It was supposed to replace the Mi-1 in military aviation and would be especially valuable to Aeroflot as an ambulance and air taxi. Some Mi-2s are believed to have been delivered to the UAR, from where they likely ended up in Israel.
In the mid-fifties, Mil's bureau decided to improve the performance of the Mi-1 by developing a turbine version. For this purpose, two new gas turbine engines with a free turbine “Izotov GTD-350” were selected. With a weight that was half the weight of previous piston internal combustion engines, two GTD-350 were 40% more powerful. They are mounted side by side above the fuselage, which significantly increases the available cabin space and improves the performance of the Mi-2 helicopter. This power plant made it possible to change the speed of rotation of the propeller, maintaining constant engine speed.
The prototype of the aircraft was called V-2, and then was renamed Mi-2. The helicopter first took off in September 1961. It had the same rotor, gear and tail as the Mi-1. After preliminary tests, a metal tail rotor was adopted (the Mi-1 had a wooden one), and then, in 1965, a new main rotor hub appeared, borrowed from the Mi-6.
Since Soviet factories were fully occupied with the production of the Mi-8 and other heavy helicopters of the Mi series, an agreement was reached with the WSK-Swidnik enterprise for the production and further development of the Mi-2 in Poland, which began in 1964. The first Polish Mi-2 before that flew in November 1963, and after testing was completed, large-scale production began in 1965. The first production Mi-2 helicopter was equipped with 400 hp engines. s., but since 1974 this parameter has been increased to 450 hp. With. The use of fiberglass in the main rotor, tail rotor and stabilizer simplified production and increased productivity.
Various variants of the Mi-2 were built for civilian and military purposes. The helicopter, which was in service with the Polish Air Force, was equipped with rocket launchers and air-to-surface missiles, which were launched from guides on the sides of the fuselage.
Interesting Facts
In the border troops, the Mi-2 is used for border patrols and is equipped with a loudspeaker.
In Chernobyl in 1986, Mi-2s eliminated the consequences of an explosion at a nuclear power plant.
From 1978 to the present, the helicopter has been an indispensable participant in all world championships in helicopter sports.
Mi-2 helicopters delivered to Iraq in 2006 helped the country’s agriculture, treating over 28 thousand hectares with pesticides in just two weeks.
As monuments to the worker, these helicopters stand on pedestals in the cities of Moscow, St. Petersburg, Kurgan, Vorkuta, the Zvezdochka pioneer camp in Togliatti, and at the DOSAAF airfield in Buzuluk, Nizhnevartovsk, Yakutsk.
Mi-2 took part in tragic films, comedies, detective stories and thrillers; it appeared on the screen in 23 films, the most famous of which are “Mimino”, the series “The Investigation is Conducted by Experts”, “Crew”, “Sniper-2” , “D-Day”, the TV series “Truckers” and others.
Mi-2
Modifications
- Mi-2: standard civilian version helicopter, convertible passenger or cargo transport, pollinator (called Bazant), training aircraft for aerial photography and photogrammetry, or cargo carrier with external sling and electric winch.
- Mi-2B: basic model with updated navigation aids and electrical system without rotor blade deicers. The weight of the passenger version was 2300 kg, and the cargo version – 2293 kg.
- Mi-2D Przetacznik: military air command post with radio communications, encryption and telephone equipment.
- Mi-2P: a standard eight-seater passenger helicopter, convertible into an all-cargo helicopter with external sling and electric winch.
- Mi-2R: agricultural version for conventional or ultra-low spraying and spraying. Tanks with a capacity of 500 liters of liquid or 375 kg of dry chemicals each were hung on both sides of the fuselage, and a 14-m sprayer boom with 128 nozzles was attached. Weight without load – 2.372 kg.
- Mi-2 Platan: mining helicopter.
- Mi-2RL: air ambulance and search and rescue version of the Mi-2, equipped with an electric lift.
- Mi-2РМ Anakonda: Version of the Mi-2Р search and rescue helicopter for naval use with an electric winch through the side door port, seating for two people and air-dropped lifeboats. 9 units built for Polish naval aviation.
- Mi-2Ro: military reconnaissance modification.
- Mi-2RS Padalec: chemical and bacteriological reconnaissance helicopter.
- Mi-2S: Medevac air ambulance, equipped to transport four stretchers, an attendant, and two patients in a sitting position.
- Mi-2SZ: training helicopter with dual controls.
- Mi-2T: military transport.
- Mi-2URN: A variant of the 1973 Mi-2US, but with two Mars 2 launchers, each carrying 16 57mm S-5 unguided rockets for close air support or armed reconnaissance.
- Mi-2URP Salamandra: anti-tank model of the Mi-2 helicopter, version 1976, with four AT-3 (Malyutka 9M14M) guided missiles on the pylons and four more in the cargo compartment; later models were equipped with four Strela 2 missiles.
- Mi-2URPG Gniewosz: similar to the Mi-2URP, but with four SA-7 (9M32 Strela) anti-aircraft missiles.
- Mi-2US: a combat helicopter equipped with a 23 mm NS-23KM cannon on the left side of the fuselage, two machine guns on the sides and two 7.62 mm machine guns in the rear of the cabin.
- Mi-2FM Kajman: version for photogrammetry. 2 units produced.
- Mi-2X Chekla: radiation reconnaissance helicopter and smoke screen producer.
- UMi-2Ro: training reconnaissance version.
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oEPETsNBNPSH OPEDYARYUBHREKEY YUBHYUOPNLSHKEMNYARH DBSU YARPYUM MU OPEDLER YAEPKHIMNTSN OPNKHGBNDYARBU BEPRNA╦RYU lH-2 MYVYUKHYAE B 1963 Ts. YAYUMN YANTSKYUYEMKHE N OPEDNYARYUBKEMKHH ONKEYAYNI YARNPNME KKHJEMGKHH MU OPNKHGBNDYARBN BEPRNA╦RNB lH-2 X DBKHTSUREKEY Y MHL. ON SHRNLS YANTSKYUEMHCH YANBERYAYKHI YANCHG TSYUPYUMMRKHPNBUK GYUSOYS B ONKEYE DNYARYURNVMNTSN YNKKHVEYARBU BEPRNA╦RNB, DBKHTSYUREKEY H GYUOYUYAMSHU VYUYAREI.
b RE BPELEMYU RUYHE BNOPNYASH PEYUKHYAE ASHYARPN, ONYAINKEIS PEYUKHYAE YABSHYE. ONSHRNLS EE╦ DN ONDOKHYUMKH YANTSKYUYEMKH, B YNMZHE 1963 Ts., MYUVYUKNYAE NYABNEMKHE YaEPKHIMNTSN OPNKHGBNDYARBU lH-2 MU NDMNL HG THKKHYUKNB YNMZHEPMYU "oEGEREK" - BEPRNA ╦RMNL GYUBNDE B Ts. - GYUBND RPYUMYAONPRMSHU YAPEDYARB).
pYUMEE MU RNL FE GYUBNDE OND NANGMYUVEMHEL SM-1 (NR YAKNBYu Smiglowiec - OPNHGMNYAHRYA "YLKHTSKABEZH" - BEPRNA╦R) YARPNHKYA OH KHZHEMGKHH BEPRNA╦R lH-1, YU RUYFE ECN LNDKHTHY YUZHKH, PYUGPYUANRYUMMYU B ONKEYE - SM-2. oPNHGBNDYARBN DBKHTSUREKEY TsRD-350 X PEDSYRNPNNB bp-2 ONPSVHKH THKHYUKS YNMZHEPMYU "oEGEREK" B Ts. FESB (WSK Rzeszdw).
naSHVMN KKHZHEMGKHNMMNE OPNKHGBNDYARBN NYAMNBSHBUERYAJ MU YAEPKHIMNI OPNKHGBNDYARBEMMNI DAYSLEMRYUZHHH; B YAKSVUE FE I LH-2 ONKEYAYKHE YAOEZHYUKHYARSH PUYAONKYUTSYUKH KHIE VEPREFYULH OPNRNRHOYU, Y REUMNKNTSKHVEYAYSCH X NPTSYUMKHYUZHNMMSC VYUARE OPKHKNYAE PYUGPYUAYURSHBURE B GYUBNDYAIN L ya. bMYUVYUKE BEPRNA╦R ONKSVHK ASHKN NANGMYUVEMHE SM-3, MN ONRNL PEHKH ME LSDPIARBNBURE KSYUBN H BEPMSKKHYAE Y NANGMYUVEMKHCH “lH-2”.
GYUBNDYUL B YBKHDMHYE X FESBE OPKHKNYAE B YNPNRYKHE YAPNYKH NYABNHRE MNBSH REUMNKNTSKHVEYAYHE OPNZHEYAYASH. YANBERYAIKHI YANCHG NYUGSHBUK ONLNYE B NPTSYUMKHGYUZHKH OPNKHGBNDYARBU ONYARYUBYULH NANPSDNBYUMKH LYUREPKHYUKNB, MU ONKEYAYKHE GYUBNDSH ASKKH MUOPYUBKEMSH YANBERYAYKHE YAOJHYUKHYARSH .
26 YUBTSSYARYU 1965 Ts. oEPBSHI ONK╦R lH-2, ONKMNNYARECH KhGTSNRNBKEMNTSN B ONKEYE (GYUB. No. OPHBNDHKYA YUY 320001), YANYARNKYA 4 MNAP 1965 TsNDYu; LYUHMS OKHKNRKHPNBYUK SHYKHOYUF B YANYARYUBE b. LEPŽHYU (W. Mercik), j. lNYAYNBKHVYU (j. Moskowicz) X X. ъПНБЯНЦН (m. Jarowski).
oEPBSHE LYUKHMSH (MSKEBNI YAEPHH) OEPEDYUKH B YANBERYAYKHI YANCHG DKK OPNAMNI SHYAOXYURYUZHHH. bMEME YEPKHIMSHE lH-2 NRKHVYUKHYAE NR DNPYUANRYUMMNTSN BRNPNTSN OPNRNRKHOYU NRYASRYARBHEL YHKEBNI ONBEPUMNYARKH MU UBNYARNBNI AYUKYE X KHMNI TNPLNI NRBEPYARKHI B OEPEDMEI VYUYARKH YYUAYUMYU OND BNGDSUNGYUANPMKHYNL LYUYAKNPYUDHYURNPYU (NMH ASHKH ME NBYUKEMSHLH, YU OPILNSTSNKEMSHLH). xGLEMHKNYAE RUYFE PUYAONKNFEMHE YUMREMM PUDHNYARYUMZHHH OPNAKEYAYINBNTSN NTsM (I YAEPEDHMSH UBNYARNBNI AYUKYKH ETSN OEPEMEYAKH Y YNMZHS E╦).
sFE B YAKEDSCHYEL TsNDS OPNHGBNDYARBN PUGBEPMSKNYAE MU ONKMSCH LNYNYARE. oEPBSHI YAEPHIMSHI SCHYGELOKP (ANPRNBNI MNLEP 101, GYUB. No. 520101086) ASHK OEPEDYUM bbya omp 29 DAYUAP 1966 Ts. ONYAKE VERSHP╦ULEYAvMSHU GYUBNDAYKHU HYAOSHRYUMKHI. sBSH, SHCHRYU LYUHMYU ME YANUPYUMHKYUYAE: NMYU ASHKYU YAOHYUMYU ONYAKE YUBYUPHH, YU E╦ UBNYARNBYU AYUKYU SYARYUMNBKEMYU MY DPSTSNI lH-2 ONKEYAYKHU bbya (ANPR 2026, GYUB. No.55202 6101).
b 1967 Ts. YANYARNKYUYAE LEFDSMYUPNDMYU OPELEEPYU, OPHV╦L OPEDYARYUBKK LYUHMS ME YAYAYAP, YU ONKEYU. YaEPHIMSHI lH-2o ONKEYAYNTSN OPNKHGBNDYARBU (PETSKHYARPYUZHK SP-PSC, GYUB. No. 530322047) DELNMYARPHPNBUKYA MU 27-L LEFDSMYUPNDMNL YUBKHYYNYALHVEYAYNL YUKNME B kE-a SPFE I BSHYARYUBNVMSHL MNLEPNL m-152.1 onyake ShRNTsN yNLHRER murn ON YANTSKYYANBYUMHCH YUBHYUZHNMMSHU YARYUMDYUPRNB (ASCC) OPHYABNHK BEPRNA╦ RS YNDNBNE MYUGBYUMKHE "UNOKUIR" (Hoplite - TSNOKHR, OELKHI BNHM B YUPLKHH DPEBMEI tsPEZHKH). b ONKEYE lH-2 ONKSVKHK MYUGBYUMKHE "Marabut" (YUHYAR LYUPYUAS), MN NMN ME OPHFHKNYAE. x NVEME UNPNN, VRN RYU - LYUPYUAS BEDE, YUY KHGBEYARMN, LEPGYU ORKHZHJU, OHRYUCHYYUYA OYUDYUKECH..
i 1974 Ts. I REU ONP ONKEYAYKHE YNMYARPSYRNPSH I ONLNYECH YANBERYAYKHU YNKKETS OPNBEKH ANKESCH PUANRS ON LNDEPMHGYUZHHH SYANBEPEMYARBNBYUMHCH BEPRNA╦RYU. b VYUYARMNYARKH, Y 20-I YAEPHH (NYRYAPE 1971 C.) YADBHFMNE NYMN YAOPEDH-YAKEBYU GYULEMHKH YADBHFMNI DBEPECH DK NAKETSVEMH ONYYUDYKH BSHYAYUDYKH OHKNRYU. aSHKH PYUGPYUANRYUMSH YAREIKNOKYARKHYNBSHE KNOYUYARKH MEYASYETSN X PSKEBNTSN BHMRNB, MNBNE YAEKEYAYUNUNGYARBEMMNE NANPSDNBYUMKHE (B R.V. 600-KHRPNBSHE YAREIKNOKYARKHYNBSHE AYUY X DKЪ UHLKHYURNB BGYULEM LERYUKKKHVEYAYKHU 550-KHRPNBSHU), SKSVIEMYU YNMYARPSYZHKH X REUMNKNTSKH OPNKHGBNDYARBU LMNTsKHU SGKNB X DERYUKEY. b 1971 Ts. LEMEYUBKHE HGMNYA DBHTSUREKEY OPH PUANRE I TsPSMRNBSHU WINDOWS; BONYAKEDYARBHH ogs YARYUBHKHYAE MU MEINRNPSHE HG ONKEYAYKHU lH-2.
gyu ONLNYE B NYABNEMXX OPNKHGBNDYARBU lH-2 PJD YANRPSDMKHYNB lNYAYNBYAYNTsN BEPRNA╦RMNTsN GYUBNDU ONKSVKHK ONKEYAYKHE OPYUBHREKEYARBEMMSHE MYUTSPYUDSH, YU TSEMEPUKEMSHI YN MYARPSYRNP l. k. lHKE X m. i. nRDEKEMZHEB, BMEYAKHI GMYUVHREKEMSHI BYKYUD OPH BMEDPEMKHE BEPRNA╦RYU B OPNKHGBNDYARBN - yNLUMDNPYAYKHE yPEYARSH bNGPNFDEMKH onKEH.
b REVEMKHE MEYAYNKEIKHU KER lH-2 ASHK EDHMYARBEMMSHL DBSUDBKHTSUREKEMSHL K╦TSYHL BEPRNA╦RNL, BSHOSYAYUBKHLYAEPKHIMN. kKH'E EYARE KER YAOSYAR, B 1971 Ts., ON╦K B YAEPKHCH YULEPHYUMYAYKHI BEPRNA╦R YUMYUKNTSKHVMNTSN YKYUYAYU aEKK 212, NYAMYUY╦MMSHI YAOYUPEMMSHLH DBKHTSYUREKLH oPSCHRR ShchMD skhrmkh yshchmyudyu or6r-3 rskhm oshchY (prAr-3 Twin pYuYa).
b 1965 Ts. aNKEHMYARBN BEPRNA╦RNB SCHRNTSN RHOYU ASHKN ONYARYUBKEMN B yayap KH DPSTSKHE YANZHHYUKHYARHVEYAYHE YARPIUMSH. oNLHLN YANBERYAYNTSN YANCHGYU, lH-2 GYYSOYUKH aKHPLYU, ankTSYUPKH, BEMTSPHY, TsDP, ETsKHOER, hPYUY, YMDP, YSAYU, KEYANRN, kHBKH, mHYYUPYUTSYU, pSLSHMHJ, YAKHPH , VEUNYAKNBYUYH X chTSNYAKYUBH. b 1978 C. NDHM lH-2 B YAEKEYAYUNUNGYARBEMMNL BYUPKHUMRE ONOYUK DUFE B yayu, ONKSVHB PETSKHYARPYUZHCH N51946.
ONGDMEE GYU YAV╦ OEPEOPNDYUF lH-2 ONЪBHKHYAE KH B DPSTSKHU YARPIUMYUU (MYuOPHLEP, B dFKHASRKH, rSPZHKHKH, BEMEYASCHKE KH R.D.). NYAMNBMNI SHYYAONPRMNI LNDKHTKHYUZHKHEI ASHKYU TsPSGNOYUYUFKHPYAYU, MN ONYARYUBKKKHYAE GYUYUGVKHYUL H YAOEZHBYUPKHYUMRSH. b 1974 TsNDS VEUNYAKNBYUYH OPHNAPEKYU lH-2 YAN YAOEZHHYUKEMSHL NANPSDNBYUMHEL DK YNMRPNK DNPNFMNTsN DBHFEMKH. b RNL FE TsNDS B aNKTSYUPHCH ASHK ONYARYUBKEM lH-2, NYAMYUY╦MMSHI PYUDKHNKNYUZHHNMMSHL NANPSDNBYUMHEL DKЪ YNMRPNK GYU GYUTSPЪGMEMKHEL YUYBYURNPKHH v╦PMNTsN LNP. YaEKEYAYUNNGIYARBEMMSHI BYUPHYUMR HYAONKEGNBUKYA B yayap, onKEYE, BEMTSPHH, tsdp, xPYUYE, xPYUME, chTSNYAKYUBHH X kKHBYUME.
b nya lHKЪ BEPRNA╦РШ lH-2 ONKEYYNTSN OPNKHGBNDYARBU ONKSVHKH BSHYANISCH NZHEMYS. oYUBDU, KHMNTsDU ASHBUKH X SHYAZHEYAYASH. ONKYKH B ANKEHMYARBE YABN╦L NRMNYAHKHYAE Y MYUL, LTSYN TsNBNP, ME YUURKH (ONVELS - ShRN SFE YANBYAEL DPSTSYU KHYARNPKHYA), KHO OEPHNDHVEYAYKH SHRN NRMNYEMKHE YARYUMNBHKNYAE EY╦ ANKEE ME YUURH. tsNBNPЪR, VRN B NDMNL HG MNBSHU, RNKAIN VRN I GYUBNDYU, lH-2 MUYH K╦RVHYH MYUKH GYUOHYAYS YAKEDSCHYETSN YANDEPFYUMH: “b ShchRNL BEPRNA╦RE EYARE MESYARPUMHLSHI DETEIR, MN BSH ETSN UPE MUID╦RE!”
b yayaap lH-2 SHYYAOXYURKHPNBUKYA B RP╦U NYAMNBMSHU BYUPKHYUMRYUU: RPYUMYONPRMN-OOYAYAYUFHPYAYNL (YNRNPSHI LNTs B YUSCHPNDPNLMSHU SYAKNBKHYU OEPENANPSDNBUREYA B YABIGM NI, YAYUMHRYUPMSHI, YAOYUYUREKEMSHI, OYURPSKEMSHI HKH YUSCHPNTNRNYAZ╦LNVMSHI), YAEKEYAYUNUNGYARBEMMNL X SVEAMN-RPEMKHPPNBNVMNL I DBNIMSHL SOPYUBKEMHEL. with MYYA SHCHRH BYUPHYUMRSH NANGMYUVYUKHYAE YANNRBERYARBEMMN lH-2r, lH-2yau X lH-2s. "dBNIIKH" YYURKHBMN HYAONKEGNBYUKHYAE B YUVEYARBE YNPYUAEKEMShu BEPRNA╦RNB MU KEDNYNKYU DK PUGBEDYKH KEDNBNY NAYARYUMNBYKH YABGKH LEFDS YASDYULH. oPHLEMKYA lH-2 X B ONKЪPMNI YUBHYUZHHH.
I YAYULNTSN MYVYUKYU SHYAOXYURYUZHHH lH-2 YARYUK ONOSKPMNI LYUKHMNI B YAHYARELE TSPYUFDUMYAYNI YUBHYUZHHH.
yYuY OPYUBKHKN, "YUSCHPNTKNRNBAYKHE" lH-2 ONKSVIUKH PETSKHYARPYUZHNMMSHE MNLEPYU B YAEPKHU 14, 15, 20 X 23 (MYUOPHLEP, yayap-14089, -15207, -20320 X -23309), MN A SHKH X LYUHMSH I MNLEPYULH B "YUM-VERSHPMYURNI" YaEPHH 81500. sFE ONYAKE PYYAOYUDYU YAYYYYUKH ONYBKЪREYA “SBNKEMMSHE” HG bbya SHYGELOKPSH I MNLEPYULH B YAEPHH 00, YU NDHM lH-2s HLEK “YUM-DBEMYURSHI” MNLEP yayap -11074 (OH GB. No.548811074). Onyake 1973 Ts. lH-2, KERYUBKHE MU yPYUIMEL yaEBEPE KH DUKEMEL BNYARNYE, ONKSVHKH NPYUMFEBN-YAHMCCH PYYAYPYYAYS DK ANKEYEI GULERMNYARKH MU TNME YAMETSYU H KEDYU B YAKSVIUE BSHMSFDEMMNI ONYAYUDY H. lNDHTHYUZHHH :
| b-2 | OPNRNRHO. xGTSNRNBKEM MU GYUBNDE No.329 B 1961 TsNDS. |
| b-2b | NOSHRMSHI BNNPSF╦MMSHI. LNTs MEYARKH 6 orsp "TYUKYUMTSYU" KHKH 4 AKNYU sa-16-57. xGTSNRNBKEM B 1965 TsNDS. b MUYARNYE BPEL MYUNDHRYA B LSGEE bbya B lNMHMN. |
| b-2l | NOSHRMSHI LNPYAYNI. NYAMYUYUKYA YUBYUPPHIMSHHLH ONYUDNVMSHHLH AYUKKNMERYULH. xGTSNRNBKEM B 1965 TsNDS. |
| b-3 (W-3) | LNDEPMHGHPNBYUMMSHI. pYUGPYUANRYUM YANBLEYARMN I ONKEYAYHLH YNMYARPSYRNPYULH B 1972-1979 TsNDYUU. OEPBSHI ONK╦R YANYARNKYA 16 MNYAP 1979 TsNDYU. BSHOSYAYUERYA YEPHIMN I 1988 TsNDYU. xGCNRNBKEMN ANKEE 120 BEPRNA╦RNB. |
| b-20 | I am SDKHM╦MMSHL TCHGEKFEL (OPNEIR). pYYYAYAVHRYUM MU 10 OYYYYUFHPNB. pYUGPYUANRYUM B 1964 TsNDS. |
| lH-2 | OEPBUYAEPKHIMYU LNDKHTKHYUZHKH. |
| lH-2yu | ЪБКЪРЯЪ LNDEPМХГХПНБУММШЛ БУПХУМРНЛ BEPRNA╦РУ lХ-2. nM ONYARPNEM OH NDMNBKHMRNBNI YAUELE I RP╦UKNOYUYARMSHL MEYASYHL BKHMRNL X DBSUKNOYUARMSHL UBNYARNBSHL BKHMRNL. BLEYARN DBKHTSYUREKEY TsRD-350 MU BEPRNA╦RE lH-2yu HYAONKEGNBUMSH DBYU RSPANBUKEMSHU DBKHTSYUREK YUH-450, YAOPNEIRKHPNBUMMSHE B SYPYUKHMYAYNL glya "opNTsPEYAYA", HKH "Arrius" -2MI", PYUGPYUANRYUMMSHLH TPYUMZHSGYAYNI THPLNI "rSPANLEYU". b PEGSKERYURE SYARYUMNBYKH SHCHRKHU DBKHTSYUREKEY ASHKKH GYULERMN SKSVIEMSH K╦RMN-REUMHVEYAYKHE UYUPYUREPHYARKHYKH BEPRNA╦RYU. MNBSHE DBHTSUREKH, OH YAPYUBMEMKHCH I TsRD-350, HLECHR LEMEKHI SDEKEMSHI PUYAUND RNOKHBYU, ANKEKHI PEYASPYA KH MYUD╦FMNYARE, LEMEKHI SPNBEME SLYU X SHLHYAYAHH GYUTSPЪGM ЪCHYKHU BEYYYARB. b YABGH I SYARYUMNBYNI MNBSHU DBKHTSUREKEY ASHKYU HGLEMEMYU RPYUMYALHYAYAH BEPRNA╦RYU. sYARYUMNBKEMSH MNBSHE PEDSYRNPSH - TSKYUBMSHI cp-2yu X NAZEDKHMYCHYKHI np-2yu, YU RUYFE YANEDKHMHREKEMSHI BYUK DK OEPEDYUVH YPSRJETTSN LNLEMRYU NR np-2yu Y cp-2yu. rPYUMYALHYAKHNMMSHE BUKSH, OPNLEFSRNVMSHI X UBNYARNBNI PEDSYRNPSH ME HGLEMHKHYAE. mu BEPRNA╦RE KHLEERYA YANBPELEMMNE OPHANPMNE KH PUDHNNANPSDNBYUMHE: KB PYUDKHNYARYUMZHKH "yPHYARYUKK", sib PUDHNYARYUMZHKH "chPNY", YUBRNLYURKHVEYAYKHI PUDHNYNLOYUYA, PYUDKHNB SHYANRNLEP, OEPETSNBNPMNE SYARPNIYARBN, YAYULNK╦RMSHI NRBERVKHY YAN-94, LYUTSMHRNTNM o-503a, YAKHYARELYU YAOSRMHYNBNI MYUBKHTSYUZHHH GPS-195, ANPRNBNE SYARPNIYARBN PETSKHYARPUZHHH asp-yak1. schKEIRPN-, PYUDKHN- X OPHANPMNE NANPSDNBYUMHE ONGBNKYER HYAONKEGNBYURE BEPRNA╦R B YAKNFMSHU LERENPNKNTSKHVEYAYKHU SYAKNBKHYU, B KCHANE BPEL YASRNY. RUYFE ASHKH SKSVIEMSH RNKOKHBMYU YAKHYAREL, LYUYAKNYAKHYAREL, YAKHYAREL NUKYUFDEMH, OPNRKHBNONFYUPMY YAKHYAREL, YAKHYAREL SHKEYRPNYAMYUAFEMKH. NYARYUKEMSHE - NYARYUKHYAE AEG KHGLEMEMKHI. |
| lH-2l | lH-2, LNDEPMKHGHPNBYUMMSHI nyun "pNYARBEPRNA", I DBSL RSPANBUKEMSHLH DBKHTSUREKLH Tsrd-350o LNYMNYARECH 450 K.Ya. (331 YbR). oPNKHGBED╦M B VERSHP╦U LNDKHTHYUZHHU: YAEKEYAYUNUNGYARBEMMSHY, SVEAAMN-RPEMKHPPNBNVMSHY X BEPRNA╦R DKYUSCHPNTNRNYAZ╦LYH. |
| lH-2lyaa | lH-2, LNDEPMKHGHPNBYUMMSHI SYPYUKHMAYNI YNLOYUMKHEI nyun "lNRNP YHV", I SYARYUMNBKEMMSHLH DBKHTSUREKLKH yuh-450l X SYANBEPEMYARBNBUMMNI YAKHYARELNI SOPYUBKEMKH. oPNHGBNDYARBN NYABNEMN B 2011 TsNDS. |
| lH-2laa-b | lH-2, LNDEPMKHGHPNBYUMMSHI SYPYUKHMAYNI YNLOYUMKHEI nyun “lNRNP YHV”, I SYARYUMNBKEMMSHLH DBKHTSUREKLKH yuh-450b KH SYANBEPEMYARBNBUMMNI YAKHYARELNI SOPYUBKEMKH. |
| lH-2o | lH-2o (lЁ-2p, ONKEYAY. pasazerski) - OYYAYYUFHPYAYU LNDHTHYUZHH BEPRNA╦RYU. NRKHVYUERYA NR RPYUMYAONPRMNTSN lH-2r NRYASRYARBHEL TsPSGNBNI KEA╦DYKH MYUKHVHEL OYUYAYUFKHPYAYNI YYUAHMSH. eY╦ NDMHL BYUPKHYUMMRNL SCHRNTSN BEPRNA╦RYU YARYUK lH-2o “YAYUKNM”, YAKSFEAMSHY I ONBSHYEMMSHL YNLTNPRNL DK OEPEBNGYKH NYANAN BYUFMSHU OEPYANM. |
| lH-2p | lH-2p (Mi-2R, ONKEYAY. rozpoznawczy) - PYUGBEDSHBYUREKEMSHI BYUPHYUMR, OPEDMYUGMYUVEMMSHI DK BEDEMH RUYRKHVEYAYNI TNRNPYUGBEDYKH. RUYFE LNFER BSHONKMRE OKYUMNBSCH H OEPYAOEIRKHBMSCH TNRNYAZ╦LYS LEYARMNYARKH. with OPNRNRHOYU lH-2p ASHK ANPRNBNI MNLEP 0607 (GYUB. No. 570607127). ONLHLN SCHRNTSN, EY╦ ASHKYU YANGDUMYU PUGBEDSHBUREKEMYU LNDHTHYUZHH I NANGMYUVEMHEL lH-2pya (Mi-2RS). |
| lH-2pk | ONHYAINBN-YAOYUYUREKEMSHI BEPRNA╦R, PYUGPYUANRYUMMSHI ONKEYAYNI THPLNI PZL Swidnik MU AYUGE LMNTsNZHEKEBNTSN BEPRNA╦RYU nya lHKЪ lH-2. lH-2pk (Mi-2RL), R.E. ratowniczy, lodowy (PYURNBMHVHI, KEMDIBSHI) - YAOYUYUREKEMSHI, YASUNOSRMSHI) - BYUPHYUMR DK YAOYUYAEMKH SHCHYHOYUFEI, ONYHMSBKHU YUBYUPHIMSHI YAYULNK╦R. NYAMYUY╦M ANPRNBNI KEAEDYNI ONBSHYEMNI TsPSGNONDZ╦LMNYARKH, YAOYUYUREKEMSHL H LEDKHZHHMAYHL NANPSDNBYUMHEL, YU RUYFE DNONKMHRECEMSHLH OPNFEYRNPYULH, NYABERKHREKEMSHLH PUYERYUL X X ONKHYAINBSHL PYUDKHNYNLOYUYANL. |
| lH-2pl | oYUKSAMSHI ONKHYAINBN-YAOYUYUREKEMSHI BYUPHYUMR (Mi-2RM, ONKEYAY. ratowniczy morski, “LNPYAYNI YAOYUYUREKEMSHI”). NYAMYUY╦M SHKEIRPHVEYAYNI KEA╦DAYNI TsPSGNONDZ╦LMNYARECH 120 YTS. bMEEMHL NRKHVHREKEMSHL OPKHGMYYNL ShRNI LNDKHTHYUZHKH ЪBKJERYA ANKENI ZHKHKHMDPHVEYAYKHI YNPOSYA LNRNPEDSYRNPYU KEA╦DYKH, MUUNDIYKHIYA MYUD DBPECH OYYAYUFHPYA YNI YUAHMSH, X YPNMYREIM DK OEPEBNGYH YAAPYYASHBUELSHU YNMREIMEPNB I MYUDSBMSHLH YAOYUYUREKEMSHLH OKNRYULH ON KEBNLS ANPRS. lH-2pl HYAONKEGNBUKYA fucking onKEH X tsdp; RULE NM KHMNTSDU NANGMYUVYUKYYUY Mi-2 See (lH-2 “LNPYAYNI”). ONKEYAYKHE LYUKHMSH KHLEKH NYNASC NPYUMFEBN-AEKN-GEK╦MSCH NYPYUYAYS, MN B YNMZHE 1990-U TsNDNB MEINRNPSHE lH-2pl ASHKH ONYPUYEMSH B YPYUYAMN-AEKN-YAHMKHI ZHBER, MUONDNAKHE BE PRNA╦RNB AEPETSNBNI NUPYUMSH yayu. |
| lH-2pup | bEPRNA╦R UHLPYUGBEDYKH, KKH "LKH-2 UHLKHVEYAYKHI" (Mi-2 chemiczny), OPEDMYUGMYUVEM DK BEDEMHЪ PYUDKHYUZHNMMN-UHLKHVEYAYNI PUGBEDYKH, DK SCHRNTSN MU M╦L SYARYUMNBKEMN YAOEZH HYUKEMNE NANPSDNBUMHE DK NRANPYU KH YUMYUKHGU OPNA BNGDSUYU. b yayaap ShchRS LYUHMS MYUGBYUKH lH-2pup. YAYYYYAYYARBNBUKYU RUYFE EY╦ NDMYU LNDKHTHYUZHKH SCHRNTSN BEPRNA╦RYU - lH-2u (Mi-2Ch) - BYUPKHYUMR DK ONYARYUMNBYKH DSHLNBNI GYUBEYASH I ZHEKECH YULSTKHPNBYUMKH YASUNOSRMSHU BNIYAY; YAPEDYARBU ONYARYUMNBYH DSHLGYUBEYA B YANBERYAYNI YUPLHH RPYUDHZHHNMMN NRMNYAHKHYAE Y UHLBNIYYUL. th BSHUKNOMSHL RPSAYUL DBKHTSUREKEY SCHRNTSN BEPRNA╦RYU OPKHYPEOKEMSH MYUOPYUBKEMMSHE BMHG DKHMMSHE RPSASH, YSDYU KH DNPYUANRYUMMSHU ONDBEYAMSHU AYUNB, PYUGLEY╦MMSHU ON ANYUL T CHGEKFYU, NYASYYYARBKERYA ONDUVU DKHGEKEMNTSN RNOXBYU. ON LEPE ETSN HYAOYUPEMKH B TsNPVKHU BSHUKNOMSHU TSYUGYUU NAPYUGSERYA TSSYARNI AEKSHY DSHL. |
| lH-2ya | IYUMKHRYUPMYU LNDKHTHYUZHKH (Mi-2S, ONKEYAY. sanitarny). oPEDMYUGMYUVEM DK OEPEBNGYKH DN VERSHP╦U ANKEMSHU MU MNYAHKYUU B DBYU ЪPSYAYU OH NAHL ANPRYUL TCHGEKKFU. RUYFE MU BEPRNA╦RE HLECHRYA YNMREIMEPSH I YHYAKNPNDMSHLH AYUKKNMYULH, DEGHMTHZHPSCHYHLH OPEOYUPYURYULH H YASLYU I LEDHYULEMRYULH. b OYUYAYUFHPYAYNI YUAHME KHLEERYA SMHBEPAYUKEMNE ONDZ╦LMNE YAHDEMEEE DK YANOPNBNFDYUCHYETSN LEDPUANRMHYU. YaYUMKHRYUPMYU YUBKHYUZHKH ONKEH (Lotnicze Pogotowie Ratunkowe) ONKSVHKYU OEPBSHE DBYU lH-2ya 25 YUBTSSYARYU 1972 TsNDYu; NMH OPHLEMKHYAE B BYUPYUBE H yURNBHZHE. dN 13 NYRAP 1981 TSNDYu YYUMKHRYUPMNI YUBKHYUZHKH ASHKN ONYARYUBKEMN EY╦ 49 BEPRNA╦RNB, YNRNPSHE ONKMNYARECH GYULEMHKH SM-1 X SM-2. |
| lH-2Yau | yaEKEYAYNUNGYYARBEMMSHY. nRKKHVYUKYA NANPSDNBYUMHEL (3 BYUPKHYUMRYU YNLOKEYRYUZHKH) DK PUYAOSHKEMKH FKhDYKHU HKH YASUKHU UHLKHYURNB, SHKEIRPNNANPSDNBYUMHEL. ONYARYUBKKYA B yayap, bemtspkhch, tsdp, xPYYU, xPYUM, kHBYUM, chTSNYAKYUBHCH. |
| lH-2r | rPYUMYAONPRMYU LNDKHTHYUZHKH BEPRNA╦RYU lH-2. aSHKYU PYUGPUANRYUYU ONKEYAYNI THPLNI “PZL Swidnik”. lH-2r (Mi-2T, ONKEYAY. transportowy) ЪБКЪРЯЪ AYUGNBSHL RPYUMYAONPRMSHL BEPRNA╦RNL, OPEDMYUGMYUVEMMSHL DK OEPEBNGYKH BNYAELH VEKNBEY HKH TsPSGYU. b ZHEMRPYUKEMNI VYUARKH TCHGEKKFYU PYUGLEYEMSH YAOKHMYULH DPSTS Y DPSTS DBYU RP╦ULEYARMSHU DKHBYUMYU. eY╦ NDHM OYUYAYUFHP LNFER PYUGLEYARKHREYA PJDNL I K╦RVKHYNL, YU DPSTSNI - I OPYUBNI YARNPNMSH TsPSGNBNI YUAKHMSH (MUOPNRKhB DBEPKH). mYUD DBPECH TsPSGNBNI YUAHMSH KHLERYA KEA╦DYU, YAONYANAMYU ONDMHLURE 100-200 YTS TsPSGYU. bePRNA╦R LNFER MEYARKH TsPSG LYUYAYANI DN 700 YTS B TsPSGNBNL NRYAYE XKH DN 800 YTS MU BMEEMEY ONDBEYAYE. |
| lH-2s | sVEAMN-RPEMKHPNBNVMSHI BEPRNA╦R, PYUGPYUANRYUMMSHI ONKEYAYNI THPLNI PZL Swidnik MU AYUGE LMNTSNZHEKEBNTSN BEPRNA╦RYU nya lHKЪ lH-2. lH-2s - SVEAAMN-RPEMKHPPNBNVMSHI BYUPHYUMR YAN YAOYUPEMMSHL SOYUBKEMKHEL. mYUDN YAYUGYURE, lH-2s SCHRN VHYARN “MUYE” NANGMYUVEMHE; ONKYYKH FE SCHRNR BYUPHYUMR MYUGSHBYUCHR Mi-2 dwuster (I DBNIMSHL SOYUBKEMHEL). хMYARPSYRNP YAHDHHR MU OPYUBNL YPEYAKE, YNRNPNE YALEEEMN MYUGYUD NRMNYAHREKEMN YPEYAKYU YSPYUMRYU, VRNASH KHMYARPSYRNP LNTs KSVIE BHDERE DEYARBKH YSPYAYUMRYU. MU YNKNMYE I PSKEBSHHLH RЪTSYULH, MUUNDЪЪЪЪІЪ LEFDS K╦RVHYULH, PYYAONKNFEM OSKER DK KHLHRYUZHHH MEHYAOPYUBMNYAREI B ONK╦RE. |
| lH-2spo | BYUPHYUMR, OPEDMYUGMYUVEMMSHI DK NTSMEBNI ONDDEPPHYH BNIYAY, PYUGPYUANRYU “PZL Swidnik”. lH-2spo (Mi-2URP, ONKEYAY. uzbrojony w rakiety przeciwpancerne, "BNNPSF╦MMSHI OPNRRHBNRYUMINBSHLH PUYERYULH") NYAMYUY╦M OSYNI mya-23yl, DBSL OSKEL╦RYULH sing X VERSHPEL OPNRKHBNRYUMINBSHLH SOPUUBKELSHLH PUYERYULH 9l14l “LUKCHRYU” MU BMEMEI ONDBEYAYE. orsp MYUBNDRYYA ON OPNBNDS X SOPYUBKCHRYA NOEYURNPNL I OSKERYU, YNRNPSHI PUYAONKNFEM MU OPKHANPMNI OYUMEKH. YAKHDEMEE NOEPYURNPYU PYUGLEYEMN YAOPYUBYU NR OHKNRYU. |
| lH-3 | nRKHVYUKYUYAE MNBSHL VERSHPEUKNOYUARMSHL MEYASYHL BHMRNL, ANKEE YNLTNPRYUAEKEMNI YYUAKHMNI, HGLEMEMMNI YNMYARPSYZHHEI TCHGEKKFYU, ONDBEYAMSHLH KETSINYAZELMSHLH ANYNBSHL X TSNMDNKYULH DK OEPEBNGYKH ANKEMSHU X PYUMEMSHU. ndMUYN NOPEDEKEMMSHE YAKNFMNYARKH OPH NDMNBPELEMMNL OPNKHGBNDYARBE RPEUKNOYUYARMSHU KH VERSHPEUKNOYUYARMSHU BKHMRNB NYARYUMNBHKH BMEDPEMKHE lH-3. |
| Li-2B | BEPRNA╦Р DKЪ kХБХХ. nRKHVYUKYA OPNRKHBNOSHKEMSHLKH THKERPYULKH, YUBKHNMKHYNI THPLSH "YKHMC PYUDKHN", NRYASRYARBHEL OPNRKHBNNAKEDKHMKHREKEMNI YAKHYARELSH. xGCNRNBKEMN 25 BEPRNA╦RNB. |
| li-2Ch (lH-2u, lH2pup) | BEPRNA╦R UHLKHVEYAYNI PYUGBEDYKH. nRKHVYUKYAJOJHYUKEMSHL NANPSDNBYUMHEL. |
| Li-2F (Mi-2FM) | BEPRNA╦R DKЪ YUSCHPNTNRNYAZ╦LYH. nRKHVYUKYA TNRNYYULEPNI RC-8. |
| Mi-2M1 | LNDEPMHGHPNBYUMMSHI. nRKHVYUKYA DBKHTSYUREKLH TsRD-350o LNYNYARECH 450 SCH.K.YA. xGTSNRNBKEM B 1974 TsNDS B 1 SHYGELOKPE. |
| Mi-2M2 | LNDEPMHGHPNBYUMMSHI. NRKKHVYUKYA DBKHTSUREKLKH TsRD-350o, SBEKKHVEMMSHL TCHGEKFEL, RNOKHBMSHL AYUYNL OND ONKNL OYYAYUFKHPYAYNI YYUAKHMSH, SYAHKEMMSHL YUYAYAKH. xGTSNRNBKEM B 1974 TsNDS B 1 SHYGELOKPE. oEPBSHI ONK╦R 1 KhChKЪ 1974 TsNDYu. |
| li-2P (lХ-2о) | OYYAYYUFHPYAYHI. nRKHVYUKYA NAPSDNBYUMHEL YUAHMSH, NRYASRYARBHEL TsPSGNBNI KEA╦DYKH. |
| Li-2P "yaYUKNM" | YAKSFEAMSHY (YYUKNM). |
| Li-2Plus | LNDEPMHGHPNBYUMMSHI. nRKHVYUERYA DBKHTSUREKKLH GTD-350W2, BKHMRNL NR "YUMH", MYUKHVHEL YAKHYARELSH GPS, NANPSDNBYUMHEL, NRBEVYUCHYEL EBPNOIEYKHL YARYUMDYUPRYUL. pYUGPYUANRYUM B 2002 TsNDS. oEPENANPSDNBUMN 19 BEPRNA╦RNB. |
| li-2PPD (Mi-2D, lH-2d) | BNGDSMSHI YNLYUMDSHI OSMYR. nRKHVYUKYA 3 PYUANVHLH LEYARYULH B YAYUKNME, DNONKMHREKEMSHLH YAPEDYARBYULH YABGKH. |
| li-2R, lХ-2RO | PUGBEDVHYH. nRKHVYUKHYAE TNRNYULEPNI BAF-21 ХКХ A-39 B YNMREIMEPE S YNPM UBNYARNBNI AYUKYKH. VYuYARE BEPRNA╦RNB NYAMYUYUKYUYAE OEPYAOEIRKHBMSHLH YYULEPYULH yutyu-42/75 XKH yutyu-33/75. bNNPSPHEMHE YANYARNKN XG OSYKH mya-23yl, 2 OSKEL╦RNB sing. |
| li-2RL | YAOYUYUREKEMSHI. nRKHVYUKYA ANPRNBNI KEA╦DYNI kots-2, MYUKHVHEL YAOYUYUREKEMNTSN X LEDKHZHHMYAYNTSN NANPSDNBYUMKH, AYURUPEEI HG 4 OPNFEIRNPNB X ONKHYAYINBNTSN PUDHNNLOYUYU. |
| Mi-2RM (Mi-2 See) | OYUKSAMSHI LMNTSNZHEKEBNI. nRKHVYUKYA DNONKMHREKEMSHL RNOKHBMSHL AYUYNL B TCHGEKKFE, 2 LMNTsNGYULINBSHLH ANLANDEPFUREKLH MU ANPRYUU, TsKHDPNKEA╦DYNI MYUD DBPECH, YAOYUYUREKEMSHL OKNRNL, A YURUPEEI XG 4 OPNFEIRNPNB. pYUGPYUANRYUM B 1969 TsNDS. BSHOSYAYUKYA I 1971 TsNDYU. ONYARYUBKYA B TsDP. |
| li-2S (lХ-2я) | YAYUMHRYUPMSHI. lNFER OEPEBNGHRE 4 ANKEMSHU MU MNYAHKYUU X YANOPNBNFDYUCHYETSN. BSHOSYAYUKYA I 1972 TsNDYU. |
| Li-2SR | PEMKHYUMKHLYUZHNMSHI. nRKHVYUKYA YANYARYUBNL NANPSDNBYUMKH. BSHOSYAYUKYA I 1975 TsNDYU. |
| li-2Sz (lХ-2ь, lХ-2с, слХ-2) | SWEAMSHI. nRKHVYUKYA DBNIMSHL SOPYUBKEMKHEL (LEYARN KHMYARPSYRNPYU YAOPYUBYU), rnPYULH MU NYMYUU YUAKHMSH. LNTs OEPENANPSDNBUREYA KH KCHANI LNDKHTHYUZHKH, YPNLE lH-2yau. oPHLEMKYA B YUSCHPNYKSAYUu days, yaSHGPYUMYAYNL X yaYUPYURNBYAYNL bbyusk, yPELEMVSTSYAYNL SVHKHYE qiu. |
| li-2T (lH-2r) | RPYUMYAONPRMSHI, NYAMNBMYU LNDHTHYUZHH. lNTs OEPENANPSDNBUREYA I YUMHRYUPMSHI. OnyaryubkkyaB yayap. |
| li-2URN | BEPRNA╦R, BNNPSF╦MMSHI OSYNI mya-23 X 2 AKNYULH sa-16-57. |
| li-2URP | OPNRKHBNRYUMINBSHI. bNNPSF╦M OSYNI mya-23, 2 OSCEL╦RYULH oh X 4 OPNRHBNRYUMYNBSHLH PUYERYULH 9l14l “LYUKCHRYU”. |
| li-2URP-G | c PYYERYULH 9l 32l “YARPEKYU”. |
| li-2URS | BEPRNA╦R, BNNPSF╦MMSHI OSYNI mya-23, 2 OSCEL╦RYULH oh X 4 GEMHRMSHLH PUYERYULH 9l32l “YARPEKYU-2l”. |
| li-2US | BEPRNA╦R NTSMEBNI ONDDEPPHYH. bNNPSF╦M OSYNI mya-23yl X 4 OSCEL╦RüLH oir X 2 OSKEL╦RüLH sing. |
| PZL Kania | onKEYAYKHI LNDEPMHGHPNBYUMMSHI BYUPKHYUMR lH-2. YaMYuAF╦M DBSL TSYUGNRSPAHMMSHLH DBKHTTSUREKILH (Allison (YUMTSK.)PSYAYAY.) 250-ya20b LNYMNYARECH 426 K. Ya. (314 YbR). with SCHRNI LNDKHTHYUZHKH SBEKKHVEMSH PYUGLEPSH YUAKHMSH, SYANBEPEMYARBNBUMN NANPSDNBYUMKHE, SKSVIEMSH K╦RMSHE UYUPYUREPHYARKHYKH. I LOVE SBEKHVEMU DAY 3550 YC. OPEDKYUTSYUKYA B BYUPHYUMRYU: RPYUMYAONPRMSHI, YAEKEYAYUNUNGYARBEMMSHY, YYUMHRYUPMSHI, OYURPSKEMSHI, YAOYUYUREKEMSHI X PUGBEDSHBUREKEMSHI. oPNHGBNDHKYA I 1986 ON 2006 TsNDSH, ASHKN BSHOSYEMN 19 URSY. |
| cru: |
| lNDHTHYUZHH | lH-2 |
| dHYULERP TSKYUBMNTSN BKHMRYU, L | 14.50 |
| dHYULERP UBNYARNBNTSN BKHMRYU, L | 2.70 |
| dKHMYu,L | 11.40 |
| bSHYANRYU,L | 3.70 |
| I love it, JC | |
| OSYARNCN | 2372 |
| MNPLYUKEMYU BGKERMYU | 3500 |
| LYUYAHLYUKEMYU BGKERMYU | 3659 |
| рНОХБН, K | |
| BMSRPEMMHE | 600 |
| DNONKMHREKEMSHI AYUY | 238 |
| RHO DBKHTSUREK | 2 tsrd yKHLNB tsrd-350 |
| lnymnyare, YbR | 2 U 298 |
| LYUYAKHLYUKEMYU YAYNPNYARE, YL/V | 210 |
| yPEIYEPYAYU YAYNPNYARE, YL/V | 194 |
| oPUYRHVEYAYU DUKEMNYARE, YL | |
| MNPLYUKEMYU | 580 |
| I AM LYYAHLYUKEMNI GYUTSPSGYNI | 340 |
| I AM DNONKMHREKEMSHL AYYNL | 790 |
| YAYNPNONDZELMNYARE, L/LHM | 270 |
| oPUYIRKHVEYAYKHI ONRNNKNY, L | 4000 |
| YaRYURKHVEYAYKHI ONRNNKNY, L | 2000 |
| ShYKHOYUF, VEK | 1 |
| ONKEGMYU MYUTSPSGYU: | 10 OYYAYUFHPNB HKH DN 8 YANKDYUR |
| bottom. KhMTNPLYUZHKH: |
| VEPREF "lHKE lH-2" tNRNTsPYUTHH: | oEPBSHI NOSHRMSHI b-2 MU bdmu |
| bRNPNNI NOSHRMSHI b-2 | |
| bRNPNNI NOSHRMSHI b-2 | |
| lH-2 yushPNTKNRYu | |
| lH-2 Tsyuh | |
| lH-2 | |
| lH-2 bbya tsdp | |
| lH-2 days | |
| lH-2 bbya fri | |
| lH-2 (c) dLHRPHI yNLHYAYUPNB | |
| lH-2 bbya VEUHH (c) oYUBEK bYUMYU | |
| lH-2 (c) yEPCEI pJAZHEB | |
| VYUYARMSHI lH-2 MU BSHYARYUBYE B NYNYE (c) JEPCEI PAGEB | |
| lH-2 (c) yEPCEI pJAZHEB | |
| yYUAHMYU lH-2 (c) bKYUDHYAKYUB ynKEYAMHVEMYN |
IWELSH:
| lH-2 |
bYUPHYUMRSH NYPYYAYH:
| bRNPNNI NOSHRMSHI b-2 |
| YaEPKHIMSHI lH-2 |
| oNKEYAYHI lH-2 |
| lH-2 fucking oNKEH |
| YaOHYANY HYARNVMKHYNB: |
| YuBKHYUZHKH BPEL 2004-06. eTHL cNPDNM, dLHRPHI yNLHYAYYUPNB. KETSYKHI LMNTSNZHEKEBNI BEPRNKER lH-2 yPSHKE pNDHMSH 2001-04. bYUDHL lHUEEB. yNPNY KER B MEAE: n BEPRNKERE lH-2 yBKHYUZHKH 1999-07. eTHL cNPDNM, dLHRPHI yNLHYAYYUPNB. ketsykhi LMNTsNZHEKEBNI BEPRNKER lH-2 dLKHRPKHI tsyuI. bePRNKERSH GNBSRYA lx bYUDHL lHUEEB. lbg HL. l.k.lHKЪ 50 KER e.h.pSFHZHYHI. bEPRNKERSH L+K 1976-13. Vaclav Jukl. WSK-Swidnik Mi-2 |
sTSNKNY MEAYU. 2020
Mi-2MSB
The Ukrainian modification of the Mi-2MSB is equipped with AI-450M Motor Sich engines with a power of 465 hp. With. with 27% less fuel consumption and 25 kg less weight. The helicopter's avionics have also been updated. The variant is equipped with pylons with eight 80 mm B8W8MSB rocket launchers and automatic grenade launchers. Due to the fact that the pylons pass through the rear windows without changing the fuselage structure, machine guns with ammunition from the helicopter cabin can be installed outside.
Additional 7.62 mm machine guns can be located in the helicopter windows. In addition, under the tail boom, along with an IR jamming system, there is a flare launcher. These elements provide partial protection against infrared-guided surface-to-air missiles, which pose the greatest threat to military helicopters.
Interstellar
The modernization of the 1980s led to the fact that the aircraft received a more powerful and also an auxiliary engine, thanks to which the flight range and maximum speed of the Mi-8 helicopter increased. The cockpit is single or double, in most versions there is one pilot in the seat on the left; in the training version, the pilot and cadet are placed side by side, with dual controls.
Technical description of the Mi-2 helicopter
The supporting system is a three-blade propeller with hydraulic vibration absorbers. Blade profile – NACA 230-12M. The blades do not fold. The rotor brake is installed. The main propeller shaft is driven by the gearbox of each engine. The transmission includes a three-stage main gearbox, an intermediate gearbox and a tail gearbox.
The turbine speed reduction coefficient for the main rotor is 1: 24.6, for the tail rotor – 1: 4.16. The main gearbox provides the drive for the auxiliary systems and the power take-off for the rotor brake. The freewheel disconnects the rotor from the failed engine, allowing it to rotate itself.
Initially, each blade had the typical design of all Mil helicopters, consisting of 20 connected sections attached to a light alloy spar with a trailing edge of honeycomb aluminum and covered with light alloy sheeting. Later, WSK-PZL-Swidnik developed more advanced rotor blades based on an extruded duralumin spar with plastic sections and coating.
The system for strengthening the cyclic and collective step control lever is hydraulic; the variable installation angle, controlled by a collective pitch lever, has a horizontal stabilizer.
The fuselage is made of sheet duralumin and is connected by spot welding or rivets. It consists of three main units - the bow, central and tail booms; load-bearing elements are reinforced with alloy steel.
Design
The power plant includes 2 Al-34 engines, produced by NPO Lyulka-Saturn (Rybinsk). Each engine has a power of about 1000 hp. The helicopter can also be equipped with Canadian engines from Pratt-Whitney or turboprop TV-0-100.
The layout of the Mi-54 helicopter is created according to the classic single-rotor design, which has a four-bladed main rotor with a diameter of 13.5 m and a four-bladed tail rotor with a diameter of 2.6 m. The forward part of the fuselage is occupied by a double cockpit with a side door and an equipment compartment. Closer to the center of the fuselage is a cargo compartment that can accommodate up to 12 people. On the sides of the cabin there are large cargo hatches, which are closed with sliding doors; fuel tanks are located in the floor. Behind the cargo compartment, towards the tail, there is another fuel tank, an equipment compartment, and behind it is a luggage compartment.
The technical features of the Mi-54 include:
- wide doors with cargo doors, which create convenience in loading and unloading operations and transportation of long cargo;
- combination of classical alloys and composite materials in the construction material;
- perfect aerodynamic configuration of the steering and main rotors;
- screw bushings do not require lubrication;
- the presence of a noise-absorbing system;
- tightness of the fuel system during an emergency landing;
- the presence of additional energy-absorbing chambers in the landing gear;
- additional cushioning for pilot and passenger seats;
- air conditioning system.
The fuselage material is made mainly of traditional aluminum alloys. Composite materials are used in the structures of helicopter non-power elements. The Mi-54 landing gear is non-retractable, tricycle, supported by the front strut. The propeller blades are made of fiberglass. The main rotor hub is made of titanium and is surrounded by elastomeric bearings. In general, low peripheral speed at the ends of the screws ensures low noise levels. The Mi-54 has a hydromechanical control system.
The base model must be equipped with the following equipment systems:
- dust protection devices for engines;
- anti-icing system;
- cabin heating system;
- dual control system;
- flight navigation system for flights in low visibility conditions;
- satellite antenna;
- autopilot with increased functionality.
The take-off weight of the rotorcraft was 4-4.5 tons, the static ceiling for this aircraft was 2200 m, and the maximum speed during flight was 280 km/h. Based on flight performance, reliability, safety and fuel efficiency, the Mi-54 is superior to all production helicopters.
Chassis
Mi-2 is a helicopter with a fixed three-wheeled landing gear with a tail support. There is a double wheel at the front and one wheel is mounted in the main part. Oil-pneumatic shock absorbers are installed on all supports, including the tail one. The main shock absorbers are capable of handling both normal operating loads and potential ground resonance. The main tires have dimensions of 600x180 mm and a pressure of 4.41 bar. Nasal - size 400x125 mm, pressure 3.45 bar. The main wheels are equipped with pneumatic brakes. Metal aviation skis are optional.
Power point
The Mi-2 helicopter engine is a 313 kW turboshaft “Izotov GTD-350” built in Poland. Two such gas turbine units are mounted side by side above the cabin of the aircraft. The only rubber fuel tank with a capacity of 600 liters is located under the interior floor. On both sides of the helicopter it is possible to install additional external tanks with a volume of 238 liters. The gas station is located on the right side of the body. Oil volume – 25 l.
Accommodation
Typically one pilot sits on the left side of the flight deck. The air-conditioned cabin provides seating for 8 passengers - back-to-back benches for 3 people each, with two additional outboard seats on the starboard rear side, one behind the other. All passenger seats can be dismantled to transport up to 700 kg of cargo. Access to the cabin is via hinged doors on each side at the front of the cabin and aft on the port side. The pilot's sliding window is squeezed out in emergency situations. The rescue modification provides space for 4 stretchers and an orderly, or 2 stretchers and 2 seated patients. The training version has side-by-side seating and dual controls. Mi-2 is a helicopter with standard heating, ventilation and air conditioning systems.
Disasters and accidents
| date | Board number | Disaster site | Victims | Short description |
| May 29, 1969 | 20063 | Yakut Autonomous Soviet Socialist Republic, 40 km west of Olekminsk | 25/28 | the helicopter, having reached the edge of the cliff and losing its “air cushion”, descended and touched the shore with its tail rotor. |
| April 13, 1983 | 15735 | Georgian SSR, Gombori Pass | 2/2 | during anti-avalanche measures, he was shot down by anti-aircraft guns, the air traffic control service did not know anything and the area was not closed to flights. |
| 03 August 1983 | 20254 | a/p Cherepovets | 0/1 | reasons unknown |
| February 13, 1988 | 20919 | Ukrainian SSR, Kharkov region, 3 km west of the village. Efremovka | 5/7 | crew error |
| 05 April 1992 | 20973 | Gulf of Finland, between Vasilyevsky Island and Petrodvorets | 6/6 | crew error |
| April 27, 1993 | 23432 | Kabardino-Balkarian Republic, Prokhladny | 2/5 | The probable cause is fuel exhaustion. |
| January 10, 1994 | 20945 | Moscow region, Near the village. Cherusti, Shatura district | 3/3 | reasons unknown |
| May 11, 1994 | 23462 | Novosibirsk | 3/3 | engine failure during climb |
| May 21, 1994 | 20110 | a/p Tver (Zmeevo) | 1/2 | crew error |
| October 30, 1994 | 23240 | Amur region, 25 km southeast of Ekimchan, Selemdzhinsky district | 8/8 | equipment failure |
| 04 December 1994 | 23639 | Republic of Bashkortostan, near the village. Kanakaevo, Ishimbaysky district | 2/5 | equipment failure, hard landing |
| March 10, 1995 | 14295 | Ulyanovsk region | 3/3 | During the turn, the pilot lost spatial orientation and the helicopter collided with the ground. |
| August 19, 1995 | 20620 | Irkutsk region, near the village. White Winter, Tulunsky district | 1/5 | The helicopter hit a rock on the lake shore and fell into the water |
| 03 November 1995 | 14221 | Arkhangelsk region, Nenets Autonomous Okrug, near the village. Dresvyanka | 4/4 | The helicopter crew began landing during the day at the helipad of an oil producing company. It was then found destroyed and burned 2 km away. |
| September 19, 1996 | 15653 | Ekaterinburg, near the Maly Istok microdistrict | 1/2 | During the landing approach at an altitude of 20 m, while descending, the helicopter crew entered a strip of ground fog and lost visual contact with the ground. The pilot decided to go around, but the helicopter landed hard and fell on its side. |
| October 12, 1996 | 23681 | Tyumen region, Khanty-Mansi Autonomous Okrug, near the village. Mamontovo, Nefteyugansk district | 1/2 | During landing approach, collided with the surface of a lake 1500 m from the landing site |
| 06 November 1996 | 23803 | a/p Ussuriysk | 1/2 | While performing a series of maneuvers at low altitude, the Mi-2 collided with two other helicopters - Mi-2 and Mi-8 |
| November 20, 1996 | 20878 | Chukchi Sea, near the village of Neshkan, Chukotka Autonomous Okrug | 2/3 | After taking off from the helipad on board the icebreaker Ermak at 04:29 Moscow time, the Mi-2 touched the crane boom on the starboard side of the ship with its main rotor. Having lost control, the helicopter fell into the sea at the side of the icebreaker and plunged into the water in an inverted position at a depth of 20 m, 5 km from the coast. |
| March 21, 1997 | 20751 | Khabarovsk region, near the village. Bolshemikhailovskoe, Ulchsky district | 1/6 | crew error, equipment failure |
| 06 August 1997 | 23406 | Murmansk region, near Kandalaksha | 1/2 | The crew made an unauthorized takeoff. The helicopter collided with a tree and crashed. |
| 01 November 1997 | 15682 | Tyumen region, Khanty-Mansi Autonomous Okrug, 100 km southeast of Oktyabrsky, Oktyabrsky district | 1/4 | non-standard reasons [what?] |
| July 31, 1998 | 15663 | Penza airport (Sosnovka) | 4/4 | landing approach, crew error |
| August 30, 1998 | H.B.W. | Lake Plateniai, Plunge region | 10/11 | reasons unknown |
| 02 September 1998 | 15685 | Kamchatka region, near the village of Nikolaevka, Elizovsky district | 3/4 | crew error |
| December 26, 1998 | 02629 FLA RF | Leningrad region, near Priozersk, Vyborg district | 3/3 | crew error, weather conditions |
| 08 March 1999 | 14093 | Arkhangelsk region, near the village. Varnek, Vaigach Island | 2/2 | crew error, weather conditions |
| May 31, 1999 | 14093 | Khabarovsk Territory, 140 km northwest of Khabarovsk | 5/6 | crew error, weather conditions |
| April 17, 2000 | 23759 | Krasnodar region, near the village. Khankov, Slavyansky district | 1/2 | During the flight to the AHR, the pilot began to search for a suitable place to land and saw a power line directly ahead. While performing a turn-around maneuver with the tail boom at an altitude of about 15 m, the helicopter touched a power line wire. The beam broke off and the helicopter fell to the ground, remaining on its side. |
| 04 July 2000 | 23213 | Krasnodar region, state farm "Svetly Put", Temryuk district | 1/1 | During a turn at an altitude of about 8 m, both engines lost power. The helicopter collided with the ground and collapsed. The pilot died. |
| July 22, 2001 | 20875 | Tyumen region, Khanty-Mansi Autonomous Okrug, near the settlement October | 1/2 | crew error |
| October 23, 2001 | 15680 | a/p Ust-Bolsheretsk | 1/6 | crew error |
| November 29, 2001 | 23656 | Krasnoyarsk Territory, Taimyr Autonomous Okrug, 18 km northwest of Dudinka | 6/7 | crew error, equipment failure |
| October 17, 2002 | 14086 | Yaroslavl region, near the village of Yarkovo, Gavrilov-Yamsky district | 1/3 | crew error, equipment failure |
| November 17, 2005 | 14271 | Vologda region, between the village. Nefedovo and Baklanka | 4/5 | equipment failure |
| April 16, 2008 | 15732 | Perm region, Lysvinsky district, 90 km from Perm airport | 3/4 | reasons unknown |
| January 12, 2009 | 20981 | Khanty-Mansiysk Autonomous Okrug, Nefteyugansk district, in the area of the Yuganskaya Ob channel, 22 km west of the city of Ust-Yugan | 4/4 | An investigation is underway. |
| 02 May 2009 | 23710 | Republic of Tatarstan, Kazan | 0/2 | An investigation is underway. |
| 05 February 2011 | 00854 | Republic of Kalmykia, 15 km south of the village of Naryn Khuduk, Chernozemelsky district | 2/2 | An investigation is underway. |
| June 18, 2011 | RA-23222 | Krasnoyarsk Territory, Tokuchep village, Boguchansky district | 0/2 | An investigation is underway. |
| June 22, 2011 | RA-20815 | Krasnodar region, Kalininsky district | 1/1 | An investigation is underway. |
| November 30, 2011 | UR-14322 | Sumy region, Konotop district | 1/2 | An MI-2 helicopter crashed and caught fire while flying over a gas pipeline. The accident occurred at 14:40 near the villages of Oktyabrskoye and Kapitanivka. An investigation is underway. |
| June 11, 2012 | Khanty-Mansi Autonomous Okrug, Surgut district | 0/3 | Made an emergency landing due to an engine fire. Burnt out completely. There are no casualties. | |
| July 2, 2012 | RA-15696 | Orenburg region, Orenburg | 0/3 | It caught fire during takeoff, made a hard landing and capsized. Burnt out completely. There are no casualties. |
| August 10, 2012 | RA-3054K | Rostov region, Proletarsky district | 1/1 | Fell while doing agricultural work. The pilot died. |
| November 17, 2012 | b/n | Ivanovo region, Komsomolsky district, six kilometers from the populated village of Oktyabrsky | 2/2 | Made a hard landing. The helicopter was not registered and the flight was carried out illegally. |
| May 21, 2013 | RA-20977 | Krasnodar region, Seversky district | 0/1 | While performing agricultural work, he got caught in a power line. |
| July 11, 2013 | UR-15604 | Kherson region, Golopristansky district | 0/3 | During landing, as a result of a strong wind flow, it fell on its side and burned, there were no casualties. |
| September 9, 2013 | RF-00507 | Sakhalin region, Dolinsk | 3/3 | During aerial monitoring of the rivers, an engine failure was suspected. The PIC decided to return to the departure airfield. After turning back, the MI-2 fell onto the shoreline and caught fire. There were 3 people on board: 1 crew member and 2 passengers. Everyone died. |
Systems
The interior is heated by air heated by the engine. For ventilation in cold weather, the ambient air temperature is raised in heat exchangers.
The hydraulic system has a pressure of 65 bar and is designed to enhance the cyclic and collective pitch lever. The hydraulic fluid flow rate is 7.5 l/min. The tank is ventilated. The pneumatic system has a pressure of 49 bar and is designed to operate the brake.
Power supply is provided by starter-generators driven by two STG-3 3 kW engines, as well as by a 3-phase alternating current generator with a power of 16 kVA and a voltage of 208 V. DC power supply of 24 V is provided by two lead-acid batteries with a capacity of 28 Ah. The main and tail rotors and windshield are equipped with an electric anti-icing system. The air intake is heated by air taken from the engine.
Equipment
The agricultural version of the helicopter is equipped with a tank on each side of the fuselage with a total capacity of 1000 liters of liquid or 750 kg of dry chemical, and either a nozzle rack at the rear of the cabin on both sides, or a dry chemical sprayer on each tank. The spray sweep width is 40–45 m.
In the rescue version, an electric winch with a lifting capacity of 120 kg is installed. The ventral cargo hook can be mounted to lift suspended cargo up to 800 kg in weight.
The smoke screen installer has long additional pipes attached to the exhaust pipes into which fuel is supplied. The pilot's windshield is equipped with an electric wiper. In addition, a freon fire extinguishing system is installed in the engine compartments and the main gearbox compartment, which is activated automatically or manually.
Mi-2 helicopter: technical characteristics
- Height – 3.3 m.
- Length – 11.4 m.
- The propeller diameter is 14.5 m.
- Take-off weight – 3550 kg.
- The empty weight of the helicopter is 2350–2372 kg.
- Fuel volume – 600 l, with additional tanks – 838 l.
- Lifting speed – 4.5 m/s.
- Cruising speed and speed at altitude are 190–194 km/h, at the ground – 210 km/h.
- Ceiling – 1700 m (static), 4000 m (dynamic).
- Flight range – 355 km, maximum – 620 km.
Mass production of the Mi-2 ended in 1993. Most of the over 5,450 helicopters produced were exported to the USSR and other Warsaw Pact countries. Nevertheless, the Mi-2, which is still in operation in more than 20 countries around the world, has a chance to be revived in the Mi-2A model, being developed by Moscow Helicopter.
Production
The start of serial production of the Mi-38 helicopter in Kazan, at the Kazan Helicopter Plant, was planned for 2015; At the end of 2014, active preparations for production were underway, the fuselage of the first production Mi-38 was laid. In August 2015, at MAKS 2015, a contract was signed with UEC for the supply of 50 TV7-117V engines until 2022 (for 25 vehicles, two engines per unit). However, at the beginning of 2022, mass production of helicopters had not yet begun.
The certificate for the standard design of the Mi-38 medium transport helicopter was issued by the Federal Air Transport Agency on December 30, 2015. It is expected that the passenger version of the helicopter will be certified in 2022, and in the future modifications for search and rescue and offshore operations will be created and certified.
On January 10, 2022, it was announced the launch of serial production of the Mi-38 helicopter at the Kazan Helicopter Manufacturing Plant.
On December 2, 2022, the first copy of the Mi-38T was announced to be transferred to the Ministry of Defense of the Russian Federation, and on December 31, the second vehicle was delivered. In total, the order provides for the construction of 15 helicopters.
