RU2007128718A - CLEANABLE CHASSIS OF THE AIRCRAFT - Google Patents

CLEANABLE CHASSIS OF THE AIRCRAFT Download PDF

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Publication number
RU2007128718A
RU2007128718A RU2007128718/11A RU2007128718A RU2007128718A RU 2007128718 A RU2007128718 A RU 2007128718A RU 2007128718/11 A RU2007128718/11 A RU 2007128718/11A RU 2007128718 A RU2007128718 A RU 2007128718A RU 2007128718 A RU2007128718 A RU 2007128718A
Authority
RU
Russia
Prior art keywords
lever
shock absorber
wheels
rack
strut
Prior art date
Application number
RU2007128718/11A
Other languages
Russian (ru)
Other versions
RU2389650C2 (en
Inventor
Сергей Викторович Тюрин (RU)
Сергей Викторович Тюрин
Юрий Александрович Шубин (RU)
Юрий Александрович Шубин
Original Assignee
Закрытое акционерное общество "Гражданские самолеты Сухого" (RU)
Закрытое акционерное общество "Гражданские самолеты Сухого"
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Закрытое акционерное общество "Гражданские самолеты Сухого" (RU), Закрытое акционерное общество "Гражданские самолеты Сухого" filed Critical Закрытое акционерное общество "Гражданские самолеты Сухого" (RU)
Priority to RU2007128718/11A priority Critical patent/RU2389650C2/en
Publication of RU2007128718A publication Critical patent/RU2007128718A/en
Application granted granted Critical
Publication of RU2389650C2 publication Critical patent/RU2389650C2/en

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Claims (2)

1. Убирающееся шасси летательного аппарата, содержащее стойку, закрепленную посредством узлов навески на фюзеляже и шарнирно связанную со складывающимся подкосом, колесную тележку, амортизатор, а также механизм разворота колесной тележки с рычагом и тягой, которая шарнирно одним концом закреплена на фюзеляже, отличающееся тем, что рычаг установлен на оси колес тележки, ориентирован вперед по направлению полета и расположен в плоскости вращения колес, при этом конец рычага шарнирно соединен со стойкой и между шарниром соединения со стойкой и осью колес на рычаге шарнирно закреплен амортизатор, причем между указанными шарнирами рычага на ней жестко закреплен поводок, расположенный в плоскости, перпендикулярной плоскости расположения рычага, а тяга механизма разворота колесной тележки другим концом шарнирно соединена с рычагом.1. A retractable landing gear of the aircraft, comprising a rack fixed by means of hinge assemblies on the fuselage and pivotally connected to a folding strut, a wheeled trolley, a shock absorber, and also a turning mechanism of a wheeled trolley with a lever and a rod, which is pivotally attached at one end to the fuselage, characterized in that that the lever is mounted on the axis of the wheels of the trolley, oriented forward in the direction of flight and is located in the plane of rotation of the wheels, while the end of the lever is pivotally connected to the rack and between the hinge of connection with the rack the shock absorber is pivotally fixed on the lever and the axle of the wheels, and a leash is rigidly fixed to it between the indicated hinges of the lever on it, located in a plane perpendicular to the plane of the lever arrangement, and the thrust of the mechanism for turning the wheel carriage at the other end is pivotally connected to the lever. 2. Убирающееся шасси по п.1, отличающееся тем, что амортизатор связан со стойкой через кронштейн, имеющий шарнир для связи с амортизатором, при этом кронштейн жестко закреплен другим концом на стойке. 2. The retractable chassis according to claim 1, characterized in that the shock absorber is connected to the strut through a bracket having a hinge for communication with the shock absorber, while the bracket is rigidly fixed at the other end to the strut.
RU2007128718/11A 2007-07-26 2007-07-26 Aircraft retractable landing gear RU2389650C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2007128718/11A RU2389650C2 (en) 2007-07-26 2007-07-26 Aircraft retractable landing gear

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2007128718/11A RU2389650C2 (en) 2007-07-26 2007-07-26 Aircraft retractable landing gear

Publications (2)

Publication Number Publication Date
RU2007128718A true RU2007128718A (en) 2009-02-10
RU2389650C2 RU2389650C2 (en) 2010-05-20

Family

ID=40546162

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2007128718/11A RU2389650C2 (en) 2007-07-26 2007-07-26 Aircraft retractable landing gear

Country Status (1)

Country Link
RU (1) RU2389650C2 (en)

Also Published As

Publication number Publication date
RU2389650C2 (en) 2010-05-20

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Legal Events

Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20170727

NF4A Reinstatement of patent

Effective date: 20190506

MM4A The patent is invalid due to non-payment of fees

Effective date: 20200727

NF4A Reinstatement of patent

Effective date: 20211124

PD4A Correction of name of patent owner
PC43 Official registration of the transfer of the exclusive right without contract for inventions

Effective date: 20220112