In the winter of 1958, by government decree, the Soviet Union began designing a new vehicle that could transport large loads. And it was a new project of the Mil design bureau called Mi-10. The new device was created on the basis of an existing Mi-6 helicopter, but its peculiarity was that it could transport cargo weighing 12 tons over a distance of 250 kilometers.
During the development of the project, the requirement to transport huge ballistic missiles was added. The new helicopter model retains the same power plant as the previous model. The handling of the car has not changed either. The greatest metamorphoses occurred with the helicopter fuselage. The body of the new helicopter was narrow and relatively low, but it had a passenger compartment 16 meters long, where 28 passengers could be carried.
For long flights, additional fuel tanks could be installed on the helicopter. Loads on this machine could be transported in two ways. The first is the transportation of containers with missiles, which were held by a gripper with a hydraulic system. The second method is to transport cargo on a platform, which is attached to the landing gear.
For the first time, the Mi-10 helicopter (during its design it was also called the B-10 model) took off from the ground in the summer of 1961. Already in the fall of next year, this machine made a record for lifting loads; it was able to lift a load weighing 15 tons to a height of more than two kilometers. A year later, they wanted to close this project altogether, due to the fact that the government refused to transport missiles using helicopters. At the time of abandonment of the project in 1964, only 24 vehicles of this model were manufactured. It is for this reason that the helicopter did not have much authority and was not in demand in the national economy.
History of the creation of the Mi-10 helicopter
The successes of the giant transport helicopter Mi-6 in transporting goods over long distances could not fail to impress. After the first flights of the Mi-6 with a load on an external sling, the idea was born to create a new, specialized rotary-wing machine on its basis - a flying crane .
On February 20, 1958, a decree of the Council of Ministers of the USSR was issued, instructing OKB-329 of M.L. Mil to create a helicopter for transporting large-sized cargo weighing 12 tons over a distance of 250 km and weighing 15 tons over shorter distances. At the OKB, the project received the designation B-10, the factory designation of the machine was “product 60”, and to us this helicopter is better known as Mi-10 .
M.N. Pivovarov was appointed the lead designer of the Mi-10 helicopter, soon replaced by L.N. Babushkin, and the general management of the project was carried out by N.G. Rusanovich, the deputy chief designer.
Already in 1959, production of the first prototype of the Mi-10 began. This speed of operation was ensured by a rational solution - the power plant, propellers, transmission, control system and hydraulic system circuits were all taken unchanged from the Mi-6. And then the helicopter was simply “re-dressed”, that is, a completely new fuselage was designed.
General diagram of the Mi-10 helicopter
On June 15, 1960, the Mi-10 took to the skies for the first time (test pilot R.I. Kaprelyan), but due to a malfunction of the oil pump, the prototype soon burned out on the ground. Testing of the second prototype began in July 1961 and ended only at the beginning of 1964. Although serial production began in the same year (it was planned to begin it back in 1961), and in 1965 the Mi-10 was successfully demonstrated at Le Bourget, the development of the helicopter took an additional 3 years and was fully completed only in 1968. In that In the same year, the M.L. Mil Design Bureau was awarded the State Prize for the creation of both heavy vehicles Mi-6 and Mi-10.
However, there was too much of a gap separating it from the “people’s” Mi-6 and its “brother” Mi-10. Initially created more for military needs (providing mobile basing of missile systems), the Mi-10 did not have any decisive advantages over the Mi-6 (both machines were equipped with heavy helicopter regiments); moreover, the very idea of mobile missile systems “stalled” at that time. The civilian use of the Mi-10 was also questionable due to the need to equip all potential cargo with units for hydraulic grippers.
But with the advent of the Mi-10K (a genuine “flying crane”) with shortened landing gear (clearance - 1.65 m) and the presence of a crane operator’s cabin, the helicopter was appreciated, especially by high-rise builders. The ability to assemble sections of a building under construction on the ground, and then use a helicopter to place them on top of each other with mathematical precision, was the ultimate dream. It was with the help of the Mi-10K helicopter that in 1982, in Yakutsk, in just 5 days, a television tower with a height of 241 meters was assembled.
A total of 55 Mi-10 helicopters of all modifications were manufactured. As far as we know, only 1 sample was sold abroad (Holland). By 1989, all Mi-10s were taken out of service.
Over the years, 8 records were set on Mi-10 helicopters.
Soviet transport helicopter-crane Mi-10K
The Mi-10K multi-purpose heavy helicopter is a specialized crane helicopter. The Mi-10K helicopter can transport large cargo not only inside the fuselage, but also on an external sling. The helicopter crane is equipped with a conventional external cable suspension unit, which is designed for a load of 8000 kg. The helicopter is widely used when installing power line supports, filtration equipment at chemical plants, installing radio relay towers and other construction and installation work.
Mi-10 crane helicopters have found limited use not only in the armed forces, but also in the national economy. The versatility of application was limited by the need to equip loads with response units for hydraulic lifts. The benefit from the lighter weight of the fuselage landing gear was negated by the length of the landing gear. Anticipating these problems, the Mil Design Bureau in 1964 began developing a “short-legged” modification of this helicopter. Serman A.Kh. was appointed lead designer. The Mi-10K modification was developed specifically for construction and installation work.
The helicopter has a single-rotor design similar to the Mi-6: a tail rotor, two gas turbine engines and a four-wheel landing gear. The design of the fuselage and landing gear was somewhat different from its predecessor. The semi-monocoque fuselage has a two-seat cockpit at the front with improved downward visibility. The main rotor is like on a Mi-6 helicopter. The design forward tilt angle has been reduced to 0°45′. The tail rotor was also no different. The transmission system and power plant are the same as its predecessor, the fuel is contained in 2 fuel tanks (total capacity 9000 liters) in front of the main landing gear on the sides of the fuselage.
The designers abandoned hydraulic grips and an external platform. Thus, the height of the chassis was reduced, which reduced weight and drag. Instead of television cameras for control during loading and unloading, which did not justify their effectiveness, the Mi-10K was equipped with a suspended cabin with a third set of control levers and all-round visibility. The gondola was located under the nose of the fuselage. When carrying out loading and unloading and installation work, one of the pilots moves to the suspended cabin. Sitting down facing the cargo, he was able to observe the cargo and at the same time control the helicopter. “Savings” on the racks made it possible to increase the weight of cargo transported on an external sling to 11 tons. The lower post ensured high accuracy of installation operations. In 1975, all Mi-10s were equipped with a vibration and vibration damping system on the external suspension.
The Mi-10K was equipped with an autopilot, which had channels for direction, pitch, roll and altitude, as well as a main rotor speed stabilizer. The autopilot was included in the control system via a differential circuit. Depending on the type and conditions of work, the type of application, the number of crew members ranged from 3 to 5 people (3 pilots, a flight operator and a flight mechanic).
The main rotor is 35 m in diameter, five-bladed, with three-hinged blades and hydraulic dampers. The blades are all-metal, rectangular in shape. The steel one-piece tubular spar is joined by 20 sections, consisting of a nose section with an anti-icing package and counterweight, a tail section and an end fairing. The blades were equipped with an electric anti-icing system and a spar damage indicator. The pushing four-bladed tail rotor with a diameter of 6.3 m had trapezoidal blades. The blades are wooden with a spar and a steel tip, have an anti-icing system and a toe cap.
The power plant is two D-25V gas turbine engines designed by P.A. Solovyov, with a power of 5500 hp/4045 kW. The engines operate independently, making it possible to fly with one engine running. Each engine has its own oil system with an oil cooler and an oil tank.
The landing gear of the Mi-10K helicopter is a fixed four-legged truss with twin wheels and oil-air shock absorbers. The front wheels have a wishbone suspension. A truss safety support was installed on the tail boom.
The external suspension system of the Mi-10K helicopter, installed on a special frame inside the fuselage, had a load capacity of 11 tons for a cable length of less than 25 meters, and 8 tons for a cable length of up to 40 meters.
The new modification was created in a fairly short time. Flight tests began at the State Scientific Research Institute of Civil Aviation. The first flight took place on September 6, 1966. During flight tests, the machine was used in Leningrad for installation work and in the mountains of Dagestan. The Mi-10K was presented at an air show in Paris in 1967. MGA officially accepted the vehicle for supply in 1969. Production began in 1975 at the Rostov Helicopter Plant (in just two years, 17 helicopters were built, and 4 were converted from Mi-10). Mi-10K are still used in the construction of high-rise buildings. Mi-10 and Mi-10K helicopters were used for transport transportation, when creating drilling rigs in the gas and oil fields of the Far North and Eastern Siberia, and for unique installation work during the reconstruction and construction of industrial enterprises, significantly reducing the cost and time of work.
During the reconstruction of the Gorky Automobile Plant, the Mi-10K helicopter performed special installation work. The machine lifted and placed two inclined galleries weighing 6.2 and 7.3 tons on the roofs of three workshops in cut-out openings. If a helicopter had not been used during the work, the passenger car assembly line would have had to be stopped for three months and cranes installed directly in the workshops. With the help of a Mi-10K helicopter, a factory overhead crane with trusses weighing 11 tons was dismantled in Paris.
Also, with the help of the Mi-10K, unique work was successfully completed at the Kostroma State District Power Plant. At the top of the 250-meter-high pipe, in a short period of time, Mi-10K helicopter pilots helped install 150 tons of metal structures.
In 1980, the Ukhta “flying cranes” unit used, for the first time in world practice, two helicopters simultaneously to install heavy metal structures. A relay mast assembled on the ground, 100 meters long and weighing 40 tons, mounted on rotating units, was raised by two Mi-10Ks to a vertical position. The following year, similar work was carried out in the Tyumen region.
This unique aircraft at one time played a significant role in strengthening the position of the Soviet Union as a great helicopter manufacturing power. Moscow Helicopter Plant named after M.L. Mil, having developed the Mi-10K, gained invaluable experience in the development of heavy crane helicopters.
The Mil OKB design team received high government awards for the creation of the Mi-6 and Mi-10. In 1968, the state prize was awarded to Mil M.L., Lapisov V.P., Nekrasov A.V., Leikand M.A., Solovyov P.A., Pivovarov M.N., Matsitsky V.T., Chumachenko D.M., Maryin L.N., Kalashnikov G.P., Evich I.P., Uspensky O.V.
Technical characteristics: Modification - Mi-10K. Main rotor diameter - 35.00 m. Tail rotor diameter - 6.30 m. Length - 32.86 m. Height - 7.80 m. Empty weight - 24450 kg. Normal take-off weight is 37,000 kg. Maximum take-off weight - 38,000 kg. Internal fuel - 6340 l + optional 1920 l. Engine type - 2 GTD aircraft engine (Soloviev) D-25VF. Power - 2 x 4847 kW. Maximum speed is 256 km/h. Cruising speed - 228 km/h. Practical range - 770 km. Range: 350 km. Practical ceiling - 4750 m. Static ceiling - 3000 m. Crew - 3-4 people. Payload - 3000 kg. The load on the external sling is 11800 kg.
Prepared based on materials from: www.airwar.ru www.helicopter.su www.aviastar.org www.vertolet-media.ru
Characteristics of the Mi-10
A country:USSRType:Transport helicopterYear of issue:1960Crew:3 people (up to 28 passengers).Engine:2x D-25V with a power of 5500 hp each.Maximum speed:204 km/hPractical ceiling:3000 m (dynamic)Range of flight:430 kmEmpty weight:27.1 tonsMaximum take-off weight:43.5 tons (max. payload 15 tons of cargo, normal 8-12 tons).Wingspan:Main rotor diameter: 35 mLength:Fuselage: 32.86 m, with propellers: 41.89 mHeight:To main rotor hub: 7.8 mWing area:NoWeapons:No
Characteristics are given for Mi-10
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b 1965 C. YANBERYAYNE OPYUBHREKEYARBN PEHKN BOEPBSHE OPNDELNMYARPHPNBURE YABNH BEPRNKERSH MU XXVI YUBKHYYNYALHVEYAYNL YYUKNME B ke asPFE. OPH ONDTSNRNBYE Y LEFDSMYUPNDMNI OPELEEPE MU lH-10 No.04102 DELNMRKHPNBUKH UBNYARNBSC OJRS, "GYUHKH" OPNYARPYUMYARBN LEFDS NYAMNBMSHLH ONDYNYYULH BYAU NONP BU YAYAH, HU YARNIYKH "NDEKKH" B NAREYUREKH, YU YAYULS LYUHMS OEPEYYUYAHKH. 1 KHChM lH-6, -8 X -10 NROPYUBHKHYAE KhG ONDLNYAYNBE B OEPEKER DUKEMNYARECH 7 RSHYA. YL., LYUPPSR YNRNPNTsN OPNKETSYUK VEPEG 6 EBPNOIAYKHU YARPIUM. schYHOYUF "DEYAYRYKH" BNGTSKYUBKK GELYAYNB, Yu DN Tspyumkhzhsh yayap TsPSOOS YANOPNBNFDYUK EYE NDHM BEPRNKER OND SOPYUBKEMHEL yuktepnbyu. DNGYUOPYUBYKH NYASYYYARBKKKHYAE B YALNKEMYAYE, bHREAYAYE, BYUPYUBE, aEPKKHME, YNOEMTSYUTSEME, APCYAYAYEKE. ryuy yuy OPNUNND MYUD REPPHRNPKHEI tpts ASHK GYUOPEYEM, KERERE OPKHKNYAE VEPEG dYUMKHCH H TsNKKYUMDKHCH, OPH SCHRNL BOEPBSHE RUYHE ANKEKHE BEPRNKERSH OPNKKH MYUD LNPEL. dK SCHRNTSN BNYAONKEGNBYUKHYAE 20-YHKNLERPNBSHL YNPKHDNPNL, OPNKETSYUBKHL PJDNL I GNMYULH YARPEKEA GYUOYUDMNTSEPLYUMYAYNI obn. pYUDKHNKNYUZHNMMNE YANOPNBNFDEMKHE TSPSOOSH DN EE BSHUNDU MU YAS BEKNYAE I YANBERYAYNTSN REOKNUNDYU “xBYUM oNKGSMNB”.
b kE asPFE B RNR TsND YANAPYUKNYAE NYNKN 350 LYUHM-SHYAONMYURNB, KH MHU 24 YOOYUPYURYU BEPRHYUKEMNTSN BGKERYU. lH-10 MYUPЪDS I lH-6 X RЪFEKSHL RPYUMYAONPRMSHL YAYULNKERNL YUM-22 YARYUK NDMNI KH YAYULSHU ЪPYKHU “GBEGD” YAYUKNMYU. bN BPEL ONKERNB "DEYARYU" DELNMYARPHPNBUKYU RPYUMYAONPRHPNBYS MU TsPSGNBNI OKYURTNPLE YUBRNASYU "kyug", B RN BPEL YUY S-64A RYU KH ME ONYUGYUK YABNH BNGLNFMNYARKH Y MESDN BNKEYARBHCH NPTsYUMHGYURNPNB. bN BPEL YARYURKHVEYAINTSN ONYUGYU MU OKYURTNPLE lH-10 SYARYUMYUBKHBYUKYA YKHMNOYUBHKENM, B YNRNPNL DELNMYARPHPNBYUKKHYAE DNYSLEMRYUKEMSHE THKELSH N YANBERYAYKHU BEPRNKERYUU .
tPYUMZHSGYAYKHI YUBKHYUZHNMMSHY FSPMYUK “YUBKHYUYAENM LYUTSYUGKHM” OKHYUK: “nDMNI HG YPSOMSHU YAYEMYUZHHI YUKNMYU ASHK ONYUG PSYAYAYKHU BEPRNKERNB... delNMYARPYUZHKH... ASHKYU MYUYARNKEIN B EKHVEYARBEMMNI, VRN GYYARYUBKKYU GYUASHRE N "RFEKNBEYAMNYARH" SHCHRKHU LYUHM. b NYANAYEMNYARKH SHRN YYUAYUERYA lH-6 X lH-10″. yu BNR ZHRYURYU KH YULEPKHYUMYAYNTSN FSPMYUKYU "schYNMNLKHYAR": "yuLEPHYUMYAYU OPNLSHKEMMNYARE ME LNFER OPNRKHBNNYARYUBHRE VRN-KHAN YANBERYAYNLS lH-6 I ETSN 120-CH OYUYA YUFKHPYULKH KKH "KERUCHYYELS YPYUMS" lH-10, YNRNPSHI LNFER MEYARKH 15 R TsPSGYU... MU OKYURTNPLE, GYUFURNI LEFDS YUHYARNBSHHLH MNTSYULH YUYAYAH.” ьBEIZHYUPYAYKHI "khMREPYUBKHYU" RYU NRNGBYUKYA N LHKEBYAIKHU LYUHMYUU: "oPH YANGDYUMKH ANKENTSN lH-6 X "KERYUCHYETSN YPYUMYU" lH-10 ASHKKH PEYEMSH RUYHE KHMFEMEPMSHE OPNAK ELSH, Y YNRNPSHL DN YAKHU ONP ME NYALEKHBUCHRYA OPHAKHGHREYA YNMYARPSYRNPSH GYUOYUDMSHU THPL.”
RYU YUY OPYUBHREKEYARBN yayap PEHKN MYUVYURE OPNDYUFS GYu PSAEF MNBSHU BEPRNKERNB, RN l. k. lHKE ONKSVHK PYUGPEYEMKHE ONYUGSHBURE "BYAE" KH NRBEVYURE MU KCHASHE BNOPNYASH. b OEPBSHI FE DEME BSHYARYUBYKH NM ONPSVHK YNMYARPSYRNPYUL l. Yu. kEIYUMDS X yu. y. yNRKHYNBS ONYAERKHRE YLEPHYUMYAYHE OYUBHKENMSH H OPKHTSKYYAKHRE GUNYEYUMYAYHU YNKKETS B TSNYARKH. rE ASHIARPN NRYKKHYMSKHYAE. lH-10 HL OPEDYARYUBKK yNRKHYNB, BKYUDEBKHI YUMTSKKHIYAYHL. yuLEPHYUMZHEB ONPYUGHKYU YANBERYAYU NRYPSHRNYARE, MN, ONOYUB B YUAHMS, NMH YARYUKH ON OPKHBSHVYE SYYUDYNI TNRNTSPUTHPNBURE PUANVKHE LEYARYU SHYHOYUFYU. xU OKHKNRYUL PYUGPEHKH ONKERYURE MU lH-6, OPH ShchRNL NMH NRLEVYUKH MHGYKHI SPNBEM BKHAPUZHHI. b NRBER LHKEBYAYHL KERVHYYUL OPEDNYARYUBHKH BNGLNFMNYARE ONOHKNRKHPNBYURE Bell-47 X NDHM XG BEPRNKERNB YAKHYNPYAYNTSN. yuONTENGNL "ОУПХФЯНИ НРРИООКХ" YARYUKN NPTSYUMKHGNBYUMMNE lHKEL H YULEPKHYUMZHYULH GUYARNKEE, YNRNPNE OPNBEKH B MYURMSRNL OND DKKHMMNNMNTSNI "DEYAYRYNI" YURPE.
mu YAKEDSCHYKHI TsND XG gyuoyudmni eBPNOSH ONYARSOKHKN OPHTSKYUYEMKHE OPNBEYARKH DELNMYARPUZHNMMNE RSPME lH-6 X lH-10 ON PJDS YARPYUM. 7 LYUPRYU 1966 Ts. YANBEPHB ONYYUDYKH DKYUOPYUBNY B bHREAYAYE, bHKEMCHYAE, BYUPYUBE, aEPKHME, yNOEMTSYUTSEME, aKHMTSSMDE, TsPSOOYU OPKHASHKYU B pNRREPDYUL, TsDE 12 LYUPRYU DNAFMSH ASHKH YANYARNE YA DELNMYARPUZHNMMMSHE ONKERSH. MN TSNKKYUMJSH OPEDNYARYUBHKH RNKEIN DBYU BUPHYUMRY TSPSGYU: YAKKHYNL ANKENNI B 27 RH YAKKHYNL LYUKEMEYKHI B 1 R. oPKHKNYAE NTsPYUMHVKHREYA 20-LHMSRMSHL ONKERNL MYUD TsNPNDN L H NAYYEMHEL I FSPMYUKHYARYULH. OPEYAYU NRYUG NR ONKERYU I TsPSGNL NDMNGMYUVMN NJEMHKYU, YUY MESDYUVS YANBERYAYNI LHYAYAHH. mN 14 LYUPRY BEPRNKERSH OEPEKEREKH B YULYAREPDYUL, TsDE MU lH-10 ASHKN BSHONKMEMN MEYAYNKEIN SHTTEYRMSHU ONKERNB I GYUPEOKEMMSHL MU TsPSGNBNI OKYURTNPLE 12-RNMMSHL ASKEDNGEPNL "YURRE" POHKKEP." schRYu DELNMYARPYUZHH GYYARYUBHKYU LEYARMSHE TSIUGERSH HGLEMKHRE RNM YABNKHU YARYUREI. b KHRNTSE TSNKKYUMJSH YSOKHKH VEPEG “YUBKHYUSCHYYAONPR” NDMS “DEYAYRYS”, YNRNPSCH BYAINPE OEPEOPNDYUKH YULEPHYUMZHYUL. b yayu BEPRNKER OPNYEK 170-VYYANBSHE HYAOSHRYUMHЪ X ONKSVHK BSHYANYSCH NZHEMIS.
YANGDYUREKH lH-6/-10 ONKSVHKH DNYARNIMNE OPHGMYUMKHE KH MU PNDKHME. gBYUMH KYUSPEYURNB tsNYASDYUPYARBEMMNI OPELXX SDNYARNEMSH: l. k. lHKE, b. O. KYUMKHYANB, Yu. b. MEIPYYANB, l. Yu. kEIYUMD, l. m. oKHBNBYUPNB, d. lYUZHHZHYHI, oh. Yu. YANKNBEEB, d.l. vSLU-VEMYN, k. m. lYUPEHM, c. O. yYUKYUMKHYNB, x. O. ShchBHV, n. b. SIAOEMYAYHI. b 1966 Ts. l. k.
PEEMKHE N YAEPKHIMNL OPNKHGBNDYARBE lH-10 ASHKN OPKHMIRN EYE B 1961 Ts., MN ETSN PYUGBEPRSHBYUMKHE BYAE BPEL NRYKYUDSHBYUKNYAE, KH ME RNKEIN ON REUMHVEYAYHL OPHVHMYUL. gMYUVHREKEMNE BKKHMHE MU SHRN NYYUGYUKN ONYAREOOEMMNE YAMHFEMHE KHMREPEYAYU Y PYYERMN-BEPRNKERMSHL YNLOKEYAYUL. x BYAE FE 5 LYUPRYU 1964 Ts. YARPNKHBHI lH-6 pNYARNBYAYKHI GYUBND No.1683 OPKHYARSOKHK Y BSHOSYAYS “DEYAYRYKH”, ONKSVKHBYEI GYUBNDYAYNI KHMDEYA “KhGDEKHE 60”. pSYNBNDKHK OPEDOPHЪRHEL B RN BPEL d.l. inSLUVEMIN.
oEPBSHI YAEPHIMSHI BEPRNKER I GYUBNDYAYHL No.4680101y ONYARPNHKH GYU ONKTSNDYU. 10 YAEMRIAP 1964 Ts. ETSN ONDMJK B BNGDSU YYUOPEQM. ONYAREOOEMN RELO BSHOSYAYU SBEKHVHBYUKYA, UNR B ZHEKNL NYARYUBYUKYA MEBSHYANYHL. b 1965 Ts. YAANPNVMSHI ZHEU ONYHMSKH DBE LYUHMSH BRNPNI YAEPHH - 5680201y X 0202y, B 1966Ts. — EYE DBE RPEREEI (0301y X 0302y) X RPH VERBEPRNI (0401y, 0402y X 0403y). b 1967 C. GYUBND, ONYARPNHB LYUHMSH 0404y X 0405y, GYUBEPHK BSHOSYAY VERBEPRNI YAEPHH X MYUVYUK ORRSCH. b 1968 Ts. YAN YARYUOEKEY YANKH "DEYAYRYH" EYARNI YAEPHKH, YU B 1969 Ts. - YAEDELNI, YAYULNI LMNTSNVHYAKEMMNI. oPYURHVEYAYH B YUFDNI YAEPHH BMNYAHKHYAE MEGMYUVHREKEMSHE HGLEMEMKH B YNMYARPSYZHCH. MUOPHLEP, MYUVKHMYU I BEPRNKERYU No.66800402 DK NAKETSVEMH ONYKHDUMH ANPRYU B YUBYUPHIMSHU YAHRSYUZHKHU ASHKH BMEDPEMSH YAAPYUYASHBUELSHE DBEPKH.
b NRKHVHE NR MYUKHU DMEI, BN BPEL ONYARSOKEMKH "DEYAYRYKH" B BNIYAYU, BEPRNKERMSHE ONKYKH BUNDHKH B YANYARYUB ME YUPLEIAYNI YUBKHYUZHKH YASUNOSRMSHU BNIYAY, Yu bNEMMN-bNGDSMSHU YAKHK. ON LEPE BSHOSYAYU lH-10 PYYAOPEDEKKHYAE ASYBUKEMN ON MEYAINKEIN SHYGELOKPNB, YU KHMNCDYU H ON NDMNLS, B NRDECEMSHE BEPRNKERMSHE ONKYKH (nbo), SFE SHYYAOXYURKHPNBUKHE lH -6. b NAYEI YAKNFMNYARH bbya LNTsKH ONKSVKhRE ME ANKEE 33 lH-10.
oEPBSHLH NGMYUNLHKHYAE I MENASHVMNI LYUKHMNI SHCHYHOYUFKH kSTSYUMAYNTSN ZHEMRPYU, TsDE MYUVKHMYUK YABNCH YAKSFAS X lH-6. yaPEDH YARPNEBSHU VYUAREI KKHDHPNBYUK B NYABNEMKH RFEFKShu BEPRNKERNB ONKY, MYUNDHBKHIYA B rNPFYE, MU AYUGE YNRNPNTsN ONGDMEE YANGDUKH GMYULEMHRSHI ZHEMRP ANEBNTSN OPHLEMEMKH X OEPESVKHBUMHЪ KERMNTSN YANYARYUBYU PLEIYAYNI YUBHYUZHHH. YAYNEE BYAETSN, DUKEMEEEE TSENSPYUTHVEYAYNE OPNDBHFEMHE "DEYAYRIYH" LKN I GYUOYUDYU MY BNYARNY (B yayap, YUY OPYUBHKN, OEPBSHLH MNBSC REUMHYS ONKSVYUKH VYUYARKH, MEONYAPED YARBEMMN OPNRKHBNYARNYKHE YARPUMYUL murn). yYULSHL GYUOYUDMSHL ASHK 239-I nRDEKEMSHI TSBYUPDEIYAYKHI bo, DHYAKNZHHPNBUMMSHI MU BNYARNVMNTSEPLUMYAINL YUSCHPNDPNLE aPYUMDHYA. b 1968-75 CC. B ETSN YANYARYUBE MYYAVHRSHBYUKNYAE DN VERSHPEU lH-10. xGBEYARMN RUYFE, VRN BEPRNKERSH SCHRNTSN RHOYU ONYARSOKHKH B 51-I ntsbo (yuKEYAYUMDPKH yKhPNBNNTsPYUDYAYNI NAK.), 181-I nbo (dFULASK, yUGYUYARYUM), 280-I nbo (yYUTsYUM, ryu DFHYHYARYUM), 112-I nbo (mEPVHMYAY, vHRHMYAYU NAK. ), 825-I nbo (yaPEDME-aEKYU, yulSPYAYU NAK.), YU RUYFE B ONKYKH, PYYAONKNFEMSHE B ONKEYAYNI KETSMKHZHE, AEKNPSYAYAYNL yNAPHME, KH MEINRNPSHE DPSTSKHE VYUARKH.
SHYGNRKHVEYAYU LYUKHMYU ON OKHKNRYUFMSHL X SHYYAOXYURYUZHNMSHL UYUPYUREPHYARKHYUL MEYAYNKEIN NRKHVYUKYUYAE NR lH-6, Y RNLS FE NAKYUDYUKYU PJDNL MEOPKH'RMSHU NYANAEMMN YAREI. ON YARYUMDYUPRMNI LERNDHYE BGKER MU TsPSFEMNL BEPRNKERE YAKEDNBUKN BSHONKMRE I YNPNRYHL PUGAETSNL, OPH SHCHRNL DUFE BN BPEL DBHFEMHЪ ON TsPSMRNBNI boo LYUKHMY BEKYU YEAA DAY RYURNVMN OPHYARNIMN. ndMUYN SVEAMSHE ONKERSH VUYARN BSHONKMKKHYAE MU OSYARSHU lH-10, KH B SHCHRKHU YAKSVYUYU YOOYUPYUR NYSRHLN PUYAYYUVHBYUKYA. oPH ONYUYUYU I OPNAETSNL HGPEDYU OPNHYAUNDHKH "bHLLH" OEPEDMHU YNKEYA. ONSHRNLS B BNIYAYUU MU MEGUTSPSFEMMSHU lH-10 YARYUPYUKHYAE BSHONKMRE BGKER-ONYAUDIS BEPRKHYUKEMN, VRN B NAYEL YAMKHFYUKN SPNBEM ONDTSNRNBYKH SHCHYHOYUFEI DK DEYARBKHI B ANE BSHU SYAKNBKHU. b YPEIAYEPYAYNL ONKERE “DEYARYU” ASHKYU LEMEE SARNIVHBYU, VEL lH-6. bKHYAEBKHI MU OKYURTNPLE TSPSG ME RNKEIN YANGDUBUK GYULERMNE YUSCHPNDKHMYULKHVEYAYNE YANOPNRKHBKEMKHE, MN OPKH ONOYUDYUMKHH B NAKUYU TSPNGKHK NAKEDEMERE H ONOPNYARS "YABYUKHRE" LYUHMS. b SCHRKHU YAKSVYU SCHYHOYUFYUL OPEDOKHYASHBYUKNYAE YUY LNFMN ASHYARPEE BSHIRKH KH NOYUMNI GNMSH, YU B YPHRHVEYAYNI YAHRSYUZHHH BNYAONKEGNBUREYA YUBYUPHIMSHL YAPNYANL OKYURTNPLSH . I ONDBEEMMSHL TsPSGNL "DEYARYU" ONVRH B DBYU SYARSOYUKYU lH-6 B YPEIYEPYAYNI YAYNPNYARKH. x, YNMEVMN FE, BYAE SHYHOYUFKH SYUGSHBUKH MY RPYAYS BEPRNKERYU. o-Y m.yu. bNKYNGSA, YNRNPNLS DNBNDHKNYAE PSYNBNDHRE ONKERYULH B kSTSYUMYAYE, NRLEVYUK, VRN BN BPEL ONKERNB OPH PUDHNOPETSNBNPYU KERVKHYNB lH-10 BYAETSDU LNFMN ASHKN NRKHVHRE NR HU YNKKETS I lH-6 OH YAHKEMN BHAPHPSCHYELS TSNKNYAS.
NYAMNBMNI GYUDUVEI lH-10 YAVHRYUKYUYAE OEPEBNGYU TsPSGNB, ME ONLEYYUBHUYA B lH-6. b OPNZHEYAYAYE ANEBNI ONDTSNRNBYKH, B RNL VHYAKE MU YPSOMNLYUAMSHU SVEMKHU, SHYHOYUFKH NRPYUAYURSHBUKH RPYUMYAONPRHPNBYS I ONLNYECH OKYURTNPL PYUGKHVMSHU NAPYUGZHNB REUMKHY X: TsPSGNBSHU YUBRNLNAKHKEY, PYUBEDSHBUREKEMN-DNGNPMSHU LYUHM, APNMERPYUMYAONPREPNB, OEPEDBHFMSHU PYUDKHNYARYUMZHKHI H R. O. xMNTsDU "DEYARYKH" OPHBKEYYUKHYAE DK NYUGYUMH Kommersant ONLNYH LEYARMSHL TsPYUFDYUMYAYHL BKYUYARL . MUOPHLEP, SHYHOYUFKH 112-CN nbo GYUMKHLYUKHYAE OEPEBNGYNI NONP kscho.
NYARYUKNYAE B KHYARNPKHH lH-10 X SVYUYARKHE B PEYUKEMSHU ANEBSHU DEYARBHYU, BSHOUYUBEE MU DNACH BEPRNKERNB 181-CN nbo. b ЪМБУПЭ 1980 Ts. ШЧРУ ВУЯРЭ АШКУ ОЭПЭПНИМУ ХГ dФУЛАСКУ B юТЦУМХЯРИУМ, ЦДЭ НЯМНБМНИ ИЕ АУГНИ YARYUK ySMDSG. ON LUREPHYUKUL, OPEDNYARYUBKEMMSHL b. d. oYUEBYAIKHL, NRPЪD "DEYARNY" NYARYUKYA B YANCHGE, KH KHE BEYAMNI NDMYU LYUKHMYU ONONKMKHKYU YANYARYUB BNCCHYETSN ONKYU. BNGTSKYUBKK SCHYKHOYUF YNLYUMDHP NRPЪDU Y-M ySGMEZHNB. bEPRNKER HYAONKEGNBYUKYA, OPEFDE BYAETSN, DK OEPEBNGYKH YPSOMNTSUAYUPHRMSHU TsPSGNB. th YANFYUKEMHCH, YAKSFAYU ETSN NYUGYUKYUYAE MEDNKTSNI. KERNL RNCN FE TSNDYU, BN BPEL PEIYU YSMDSG-LUILUME, lH-10 ONREPOEK YURYUYARPNTS. b RNL ONKERE OEPEBNGHKKH MU OKYURTNPLE YUBRNGYUOPYUBYHY lug-500rg, YNRNPSHY YANOPNBNFDYUK YANKDYUR-BNDHREKE, MYUNDHBKHIYA B TsPSGNBNI YUAHME "DEYAYRIKH". bEPRNKER SDYUKHKYA NR ySMDSGYU BYAETSN MU 20 YL, YNTSDU NRYYUGYUK NDHM DBHTSUREKE. schYHOYUF YAAPNYAKHK OKYURTNPLS H ONOSHRYUKYAN YANBEP'HRE YUBYUPKHIMSCH ONYYUDYS ON-YYULNKERMNLS MU ONDBEPMSBSCHYA OKNYYUDYS. nMYU NYUGYUKYUYAE SYAEMMMNI BYUKSMYULH, ONYPSHRNI OLLYULH H OPNLNHMYULH, VRN DK "DKHMMNNMNTSNTSN" lH-10 YARYUKN PNYNBSHL NAYARRNREKEYARBNL. bKEREB B NDMS HG OPNLNHM, BEPRNKER YAKNLYUK OEPEDMKHE YARNIYKH YUYAYAKH, YAYUONRKHPPNBUK, PYUGPSYKHKYAKH YATSNPEK. EYE BN BPEL YUYAYUMH GELKKH KH METSN BSHOPSHTSMSKKH KERVKHY-URSPLYUM KH YANKDYUR, MN NMH, YUY KH NYARYUKEMSHE VKEMSH SHCHYHOYUFYU, ONTSKHAKH. rNVMSCH OPHVHMS NRYYUGYU DBKHTSUREK SYARYUMNBHRE ME SDYUKNYAE, UNR BSHYAYUGSHBYUKYUYAE BEPYAKH N ONOYUDYUMKHH B METSN OSKH HG dy.
ELS MU GÜLEMS HG dFULASKYU OPHASHKYU BRNPYU "DEYARYU". ON BNYAONLKHMYUMKHL ASHBIETSN TSKYUBMNTSN HMFEMEPYU ON BEPRNKERS KH DBKHTSUREKCH 73-I BNGDSSMNI YUPLXX O-YU tsp. tsMKHKHZHYNTsN, ShchRNR lH-10 MYUNDHKYA B yUTTSYUMHYARYUME DNAEE OPEDEYARBEMMHYU H ASHK BNGBPYUYEM B YANCHG ONYAKE RPYUTSKHVEYAYNTSN KHMZHHDEMRYU. mE ONGDMEE 1984 C. B NDMNL HG ONKERNB LYUKHMYU ASHKYU NAYARPEKYU YAMYUIOEPYULH. OPLSHL ONOYUDYUMKHEL HG "ASPU" ASHK SAHR ANPRREUMKHY. MAINRNPSHE SHKELEMRSH NANPSDNBYUMKH BEPRNKERYU ONKSVKHKH ONBPEFDEMKH. eTsN OEPETSMYUKH B dFULASK, TsDE SYARPYUMHKH BYAE MEHYAOPYUBMNYARH.
b ZHEKNL lH-10 NYUGYUKYA B bbya “KHMEI” LYUKHMNI.
na NYAMNBMNL ETSN OPEDMYUGMYUVEMKHH, YARNKE YAKHKEMN ONBKKHBYEL MU YNMYARPSYZHCH, BYAINPE ONVRKH GUASHKH. sGYYU YAOEZHYUKHYUZHKH, NRKKHVYUBKHEYA NR lH-6 KERMN-REUMKHVEYAYKHE UYUPYUREPHYARKHYKH, NVEME LYUKEMEYKHI OYUPY RPEANBUKH BSHPYUANRYKH NYANANI RYURKHYKH OPHLEMEMHYARYUB HKKH OND YANLMEMKHE ANEBSC ZHEMMNYARE “DEYAYRIKH”. lNDHTHYUZHHH :
| lH-10 | aYUGNBSHI BYUPHYUMR I "DKHMMSHLH MNTSYULH". |
| lH-10tsp (“tsPEAENNYY”) | oEKEMTSURNP (BEPRNA╦R PUDHNPYUGBEDYKH). |
| lH-10y (“yPYUM”) | bYUPHYUMR I "YNPNRYHLH MNTSYULH" X DNONKMHREKEMNI YUAHMNI OHKNRYU OND TCHGEKFEL. |
| lH-10oo | ONYARYUMNBIKHY ONLEU (NDMYU YARYUMZHKH pshcha "YUTS" OND TCHGEKFEL, 7125 YC). |
| lH-10p | "PEINPDMSHI", NRKKHVYUBKHIYA NAKETSV╦MMNI YNMYARPSYZHHEI KH DNPYUANRYUMMSHL YUYAYAH, MU M╦L ASHKN SYARYUMNBKEMN 7 LHPNBSHU PAINPDNB. |
| lH-10pby | I SYARYUMNBKEMNI MU BMEMEI ONDBEYAYE OSYAINBNI SYARYUMNBYNI I YPSHKYURNI PUYERNI I-5b (4th95). |
| lH-10juice | mNYAHREKE SMHBEPAYUKEMNI ONKEBNI KYUANPURNPHH. |
| cru: |
| lNDHTHYUZHH | lH-10 |
| dHYULERP TSKYUBMNTSN BKHMRYU, L | 35.00 |
| dHYULERP UBNYARNBNTSN BKHMRYU, L | 6.30 |
| dKHMYu,L | 32.86 |
| bSHYANRYU,L | 7.80 |
| I love it, JC | |
| OSYARNCN | 24680 |
| MNPLYUKEMYU BGKERMYU | 43550 |
| LYUYAHLYUKEMYU BGKERMYU | 43700 |
| RHO DBKHTSUREK | 2 tsrd yuBKHYUDBKHTSUREKE (yaNKNBEEB) d-25b |
| lnymnyare, YbR | 2 U 4045 |
| LYUYAKHLYUKEMYU YAYNPNYARE, YL/V | 204 |
| yPEIYEPYAYU YAYNPNYARE, YL/V | 180 |
| oPUYRHVEYAYU DUKEMNYARE, YL | 650 |
| pYUDKHSYA DEYARBKH, YL | 250 |
| oPUYIRKHVEYAYKHI ONRNNKNY, L | 3000 |
| YaRYURKHVEYAYKHI ONRNNKNY, L | 2200 |
| ShYKHOYUF, VEK | 3 |
| ONKEGMYU MYUTSPSGYU: | MNPLYUKEMN - DN 12000 YC TsPSGYU, LYUYAKHLYUKEMN - 15000 YC, MU BMEMEI ONDBEYAYE - 8000 YC |
| bottom. KhMTNPLYUZHKH: |
| VEPREF "lHKE lH-10" yMHTSYU "reUMHVEYAYNE NOHYUMKHE BEPRNKERYU lH-10" 3D LNDEKE "lh-10 « | lH-10 |
| lH-10 | |
| lH-10 | |
| lH-10 | |
| lH-10 | |
| lH-10 | |
| lH-10 | |
| lH-10 | |
| lH-10 | |
| lH-10 | |
| lH-10 | |
| lH-10 | |
| lH-10 | |
| lH-10 | |
| lH-10 |
IWELSH:
| lH-10 |
bYUPHYUMRSH NYPYYAYH:
| lH-10 |
| lH-10 |
| YaOHYANY HYARNVMKHYNB: |
| YuBKHYUZHKH BPEL 2002-03. khTSNPE BEKKHVYN, pNYARHYAKYUB LYUPYUB. "YNKNYAYA MU YARYUKEMShu MNTSYuU" yPSHKEЪ pNDHMSH 1999-02. bYUDHL lHUEEB. KERYUCHIKHI YPYUM bGKER 2010-06. lH-10 - KERYUCHYELS YPYUMS ONKBEYU ONKHTSNM. b.p. lHUEEEB. lNYAINBAYKHI BEPRNKERMSHI GYUBND KHLEMKH l.k. lHK tsPYUFDUMYAYU YUBHYUZHH. Yu. fSPYUBKEB Yu. bEPRNKER lH-10 e.h.pSFHZHYHI. bEPRNKERSH dLKHRPKHI TsYuI. bePRNKERSH GNBSRYA lx bYUDHL lHUEEB. lbg HL. l.k.lHKЪ 50 KEP Red Star 22. Y. Gordon, D. Komissarov, S. Komissarov. Mil's Heavylift Helicopters Le Fana de l'Aviation 1974-11. Pierre Gaillard. Les Geants de Mil Le Fana de l'Aviation 1989-05. Pierre Gaillard. L'URSS ai Salon. Mil Klassiker der Luftfahrt 2018-03. Nikolai Jakubowitsch. Der fliegende Kran Flug Revue 2018-02. Nikolai Jakubowitsch. Der fliegende Kran Flieger Revuer Extra No.13. Thomas Girke. Fliegenden Kran in der DDR L+K 1966-04. Vaclav Nemecek. Vrtulniky Mi-6 and Mi-10 |
sTSNKNY MEAYU. 2020
Design of the Mi-10 helicopter
The Mi-10 helicopter is built according to the classic single-rotor design with a five-blade all-metal main rotor and a four-blade wooden tail rotor.
The power plant consists of 2 D-25V theater engines designed by P.A. Solovyov. The chassis is four-legged with high (clearance - 3.75 m) pyramidal truss struts. A loading platform or container can be installed between the landing gear struts using hydraulic grippers. Hydraulic grips are remote controlled.
In the central part of the fuselage there is a cargo-passenger cabin that can accommodate 28 passengers or cargo up to 3 tons, which is loaded through the rear side door using a winch boom. Inside the fuselage there is a truss with an LPG-7 cargo winch and an eight-fold pulley system, providing lifting/lowering of cargo up to 15 tons to a height of 30 m. A television installation with a camera under the fuselage is installed in the cockpit, simplifying loading/unloading operations.
Mi-10K. It is immediately clear that the helicopter is significantly lower than earlier machines
A unified cargo platform measuring 8.5 x 3.6 m with an LPG-3 winch could be installed between the chassis supports.
The fuel is located in hanging side tanks. In the distillation version, 2 additional tanks of 1250 liters each can be installed in the cabin.
A special feature of the Mi-10 was that in order to simultaneously lift the landing gear wheels off the ground, the middle part of the fuselage, together with the main rotor axis, had to be rotated 1°30′ to the right of the vertical. At the same time, in order to maintain the horizontal position of the cabin on the ground, the right landing gear legs are made shorter by 300 mm.
In 1975, all helicopters were equipped with a system for damping vibrations and oscillations of the load on an external sling.
Mi-10, the cargo platform is clearly visible
Mi-26: a heavyweight with a three-story building
The Mi-26, which first flew on December 14, 1977, is the world's largest mass-produced transport helicopter. Due to its impressive dimensions, the pilots nicknamed it the “flying cow.” This rotary-wing giant is longer than the Boeing 737 aircraft. Mi-26 propellers cover more than 800 square meters. meters, and the height of the helicopter is about a three-story house. Its maximum take-off weight is 56 tons. Inside the vehicle, 82 paratroopers with weapons are placed, and in the sanitary version - 60 stretchers with the wounded.
During the first years of operation, the Mi-26 showed itself to be an extremely reliable and highly efficient machine, as a result of which the decision was made to create a civilian version - the Mi-26T. The helicopter lost its heat trap ejection devices and installations for small arms, and received new navigation equipment, as well as equipment for working with externally slung cargo. For example, special electronic scales allow you to determine the mass of cargo in hover mode with an accuracy of 1%. The helicopter is also equipped with special equipment to dampen vibrations of the load on the suspension.
Serial production of the Mi-26T began in January 1985 at Rostvertol. Already in 1986, Aeroflot began actively using helicopters. Mi-26T were especially in demand during the development of gas and oil fields in Western Siberia. The record carrying capacity of this helicopter came in handy in the most unusual situations. For example, the Mi-26T was used to transport a 20-ton block of ice containing a mammoth that died 20 thousand years ago. In addition, the heavyweight helicopter has repeatedly transported aircraft, including its “brothers” Mi-10 and Mi-6. Similar operations were also carried out abroad - the Mi-26T transported crashed 11-ton American CH-47 Chinook helicopters.
Despite its considerable age, the Mi-26 still remains the largest production helicopter in the world, and it has no rivals, but successors are appearing. In 2011, the modernized version, the Mi-26T2, made its first flight. On board the new helicopter is a digital complex of radio-electronic equipment and a crew reduced to three people.
Most recently, in January 2022, the updated Mi-26T2V, a modern version of the giant helicopter for the army, successfully passed preliminary flight tests. After participating in hostilities in Syria, the Russian Ministry of Defense put forward a number of requirements to the designers for the new modification, which were taken into account and implemented in the Mi-26T2V. Now the car is undergoing testing before launching into series and is preparing to continue the legendary dynasty of “heavyweights” Mil.
Helicopter modifications:
- Mi-10 (V-10, “product 60”) is the basic module of the helicopter. In 1964-1969, 38 helicopters were manufactured.
- Mi-10 is a flying laboratory with D-25VF engines with a power of 6500 hp. Manufactured in 1970.
- Mi-10GR "Scallop" - air direction finder. Equipped with a container with lowered antennas. In 1966, 1 serial Mi-10 was re-equipped.
- The Mi-10K is a flying crane, with shortened landing gear, smaller fuel tanks and an installed crane operator cabin. First flight September 6, 1966. In 1974-1977, 17 helicopters were manufactured. Another 2 were converted from Mi-10.
- Mi-10PP - jammer. It was distinguished by a special container ST-9000 “Steppe” with equipment and antennas for stations to counter ground-based early warning radars, with operator positions inside the fuselage. Developed in 1966-1970. In the 70-80s, 20 helicopters were converted at the Rostov and Konotop ARZ.
- Mi-10R is a record-breaking one. It featured a lightweight design and a modified chassis from the Mi-6. Manufactured in 1965. First flight January 14, 1965. The crews of V.P. Koloshenko and G.V. Alferov set 7 world records.
- Mi-10RVK is the carrier of the 9K74 missile and helicopter complex. Developed in 1965. Made in 1 copy.
- Mi-10UPL is a carrier of a universal field laboratory. In 1966, converted from the second prototype.
Mi-10K. Note the crane operator's cabin below the cockpit
Source: compilation based on publicly available information on the Internet, as well as the book The Flying Crane (Mikheev V.R.) // Wings of the Motherland. - 1999. - No. 2
Mi-12: still the largest in the world
On July 10, 1968, the Mi-12, the largest and most heavy-duty helicopter ever built in the world, took to the skies for the first time. It still amazes with its size. The wingspan of the Mi-12 is 37 meters. Each engine nacelle, almost the size of a fighter jet, contains a propeller with a diameter of 35 meters.
The vehicle was created as a super-heavy transport helicopter with a payload capacity of at least 30 tons for transporting components of intercontinental ballistic missiles and various military equipment. If it was necessary to use the Mi-12 for civilian purposes, it could comfortably accommodate 220 people.
With such a load capacity, the classic single-rotor design was not suitable at all. As a result, Mikhail Mil chose a transverse design, the most complex in a technical sense. By the way, the crew cabin of this rotorcraft giant was two-story.
In August 1969, the Mi-12 set an absolute record for helicopter lifting capacity, which has not yet been broken - 44,300 kg. In total, the Mi-12 set 7 world records.
In 1971, the giant helicopter received international recognition during its participation in the Le Bourget air show. Foreign experts greeted the new Soviet helicopter with admiration. “One can only take off one’s hat to the engineering and technical achievement that is the Mi-12!” said the son of the famous aircraft designer Sergei Sikorsky.
Unfortunately, Mikhail Mil did not see the success of the Mi-12 at Le Bourget. The outstanding designer died a year earlier, on January 31, 1970, without waiting for the international triumph of his last project.
In October of the same year, the car went into mass production. Only two copies were built. The helicopter lost relevance for the army after the advent of effective and lightweight strategic missiles on mobile launchers. Mil OKB has moved to launch the promising Mi-24 helicopter into production.
The first Mi-12 built was given to the Moscow Helicopter Plant for storage. This car houses the museum of Mikhail Mil and his design bureau. The second helicopter was transferred to the aviation museum in Monino, where it is still located.
