RU2001128799A - Device for transporting aircraft - Google Patents

Device for transporting aircraft

Info

Publication number
RU2001128799A
RU2001128799A RU2001128799/28A RU2001128799A RU2001128799A RU 2001128799 A RU2001128799 A RU 2001128799A RU 2001128799/28 A RU2001128799/28 A RU 2001128799/28A RU 2001128799 A RU2001128799 A RU 2001128799A RU 2001128799 A RU2001128799 A RU 2001128799A
Authority
RU
Russia
Prior art keywords
aircraft
carrier
tractor
landing gear
transporting
Prior art date
Application number
RU2001128799/28A
Other languages
Russian (ru)
Other versions
RU2302979C2 (en
Inventor
Владимир Александрович Нилов
Алексей Викторович Великанов
Леонид Витальевич Карпов
Станислав Юрьевич Медведков
Original Assignee
Воронежский военный авиационный инженерный институт
Filing date
Publication date
Application filed by Воронежский военный авиационный инженерный институт filed Critical Воронежский военный авиационный инженерный институт
Priority to RU2001128799/11A priority Critical patent/RU2302979C2/en
Priority claimed from RU2001128799/11A external-priority patent/RU2302979C2/en
Publication of RU2001128799A publication Critical patent/RU2001128799A/en
Application granted granted Critical
Publication of RU2302979C2 publication Critical patent/RU2302979C2/en

Links

Claims (1)

Устройство для транспортировки самолетов, содержащее тягач, водило в виде рамы, соединенное с рамой тягача, отличающееся тем, что водило имеет палкообразный захват, позволяющий обхватывать переднюю стойку самолета с двух сторон, также имеющий специальные пазы, за счет которых передняя стойка шасси самолета освобождается от динамических тяговых нагрузок, кроме того водило имеет буксировочный трос, который взаимодействует с основными стойками шасси самолета, предназначенными для восприятия тягового усилия.A device for transporting aircraft containing a tractor, a carrier in the form of a frame connected to the frame of the tractor, characterized in that the carrier has a stick-like grip that allows you to grasp the front pillar of the aircraft on both sides, also having special grooves, due to which the front landing gear of the aircraft is freed from dynamic traction loads, in addition, the carrier has a towing cable that interacts with the main landing gear of the aircraft, designed to absorb traction.
RU2001128799/11A 2001-10-25 2001-10-25 Transportation facility RU2302979C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2001128799/11A RU2302979C2 (en) 2001-10-25 2001-10-25 Transportation facility

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2001128799/11A RU2302979C2 (en) 2001-10-25 2001-10-25 Transportation facility

Publications (2)

Publication Number Publication Date
RU2001128799A true RU2001128799A (en) 2003-08-10
RU2302979C2 RU2302979C2 (en) 2007-07-20

Family

ID=38431259

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2001128799/11A RU2302979C2 (en) 2001-10-25 2001-10-25 Transportation facility

Country Status (1)

Country Link
RU (1) RU2302979C2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3079821B1 (en) * 2018-04-10 2020-05-08 Airbus Operations AIRCRAFT TOWING SYSTEM COMPRISING AN IMPROVED AIRCRAFT STEERING CONTROL DEVICE

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