| 发明名称 |
METHOD OF AIRCRAFT TOWING |
| 摘要 |
FIELD: aircraft engineering.SUBSTANCE: proposed method comprises approach of trailer in reverse to aircraft, locking the retainer at aircraft front leg, supporting of undercarriage front leg, carrier fastening by rear main legs of undercarriage and towing the aircraft. Note here that after fastening, brake pads are fitted under aircraft wheels, pull device is driven relative to carrier by its wheel propulsor at the motion start, then brake pads are removed to increase carrier coupling weight owing to fastening of undercarriage front leg.EFFECT: possibility to control towed aircraft initial speed.4 dwg |
| 申请公布号 |
RU2505460(C2) |
申请公布日期 |
2014.01.27 |
| 申请号 |
RU20100153391 |
申请日期 |
2010.12.24 |
| 申请人 |
FEDERAL'NOE GOSUDARSTVENNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA "VOENNYJ AVIATSIONNYJ INZHENERNYJ UNIVERSITET" (G. VORONEZH) MINISTERSTVA OBORONY ROSSIJSKOJ FEDERATSII;GOSUDARSTVENNOE OBRAZOVATEL'NOE UCHREZHDENIE VYSSHEGO PROFESSIONAL'NOGO OBRAZOVANIJA "VORONEZHSKIJ GOSUDARSTVENNYJ TEKHNICHESKIJ UNIVERSITET" |
发明人 |
VELIKANOV ALEKSEJ VIKTOROVICH;NILOV VLADIMIR ALEKSANDROVICH;NOSOV EVGENIJ VIKTOROVICH;LAZAREV SERGEJ VIKTOROVICH;LIKHOVIDOV DMITRIJ VIKTOROVICH;GOLOMAZOV EVGENIJ VALER'EVICH;ELFIMOV VITALIJ VLADIMIROVICH |
| 分类号 |
B64F1/22 |
主分类号 |
B64F1/22 |
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