SU109224A1 - Airplane landing gear with lever trolley - Google Patents

Airplane landing gear with lever trolley

Info

Publication number
SU109224A1
SU109224A1 SU565711A SU565711A SU109224A1 SU 109224 A1 SU109224 A1 SU 109224A1 SU 565711 A SU565711 A SU 565711A SU 565711 A SU565711 A SU 565711A SU 109224 A1 SU109224 A1 SU 109224A1
Authority
SU
USSR - Soviet Union
Prior art keywords
landing gear
lever
airplane landing
trolley
axles
Prior art date
Application number
SU565711A
Other languages
Russian (ru)
Inventor
Н.В. Кирпичев
Original Assignee
Н.В. Кирпичев
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 Н.В. Кирпичев filed Critical Н.В. Кирпичев
Priority to SU565711A priority Critical patent/SU109224A1/en
Application granted granted Critical
Publication of SU109224A1 publication Critical patent/SU109224A1/en

Links

Description

Предметом изобретени   вл етс  стойка шасси самолета с рычажноЛ тележкой, в которой рычаги передних и задних колес шарнирно сочленены с нижним концом стойки.The subject of the invention is the landing gear of an aircraft with a lever trolley in which the levers of the front and rear wheels are articulated with the lower end of the rack.

Известны стойки шасси само.четов с рычажной тележкой, выно.1ненные с aMopTHsaTOpaNSH, работающими на сжатие, что увеличивает вес конструкции.Known landing gear samo.chetov with lever trolley, 1nennye with aMopTHsaTOpaNSH, working in compression, which increases the weight of the structure.

В описываемой конструкции этот недостаток устранен тем, что в стойке в качестве силовото элемента нрименен работающий на расг жение воздущно-жидкостиой амортизатор , щток которого дл  нередачц амортизатору вертикальных нагрузок св зан посредством коромыс.та и подкосов с ос ми колес, шарнирио сочлененными рычажной системой с нижней частью амортизатора.In the described construction, this disadvantage is eliminated by the fact that in a rack as a strength element there is an air-liquid shock absorber working for the unraveling, the shafts of which for non-drag shock absorbers are connected to vertical loads by means of the yokes and axles of the wheel axles the lower part of the shock absorber.

На чертеже изображен в аксонометрической нроекции общий вид стойки с установкой ее на самолете .The drawing shows in axonometric projection a general view of the rack with its installation on the plane.

Звень  те.тежки / с колесами, ujapHHpHO присоединенными к центральному нижнему уз.1у цилиндра 2 амортизатора, разгружены от вертикальных нагрузок, которые передаютс  неносредственно от осей 5 колес, через нодкосы 4 и коромыс ,10 5 на щток 6 амортизатора, застав .л   его работать Tvo.TbKo на раст жение .,Link tetek / with wheels, ujapHHpHO attached to the center of the lower node 1 of the cylinder 2 shock absorber, unloaded from the vertical loads, which are transmitted directly from the axles of the 5 wheels, through knockers 4 and yokes 10 5 on the shock absorbers 6, hitting it work Tvo.TbKo for stretching.,

11 р е д м е г н з о б р с т е и п  11 p re d m e g n z o b r c e n

шасси само.1ета с рычажной те.тежкой, в которой рычаги передних и задних колес щарнирно соч.ченены с нижни% концом стойки шасси, о т л н ч а ю щ а   с   тем, что, с целью у.меньшенн  веса конструкции , в ней, в качестве си.ювого э-лемента , примепен работающий на раст жение воздушно-жидкостной амортизатор, шток которого, дл  передачи амортизатору вертикальных нагрузок, св зан через посредство коромыс.та и подкосов с ос ми колес, шарнирно соч.-|ененными. через носредство рычажной системы, с нижней частью цилиндра амортизатора . chassis samo.1eta with lever te.tezhkoy, in which the levers of the front and rear wheels are hingedly matched to the lower end of the landing gear, about the fact that, in order to reduce the weight of the structure, in it, as a blueprint, an air-liquid shock-absorber applied for stretching, the rod of which, for transferring vertical loads to the shock absorber, is connected to the axles of the wheels and axles with the axles of the wheels, it is an articulated stream. enenennymi. through the means of the lever system, with the lower part of the shock absorber cylinder.

SU565711A 1957-01-31 1957-01-31 Airplane landing gear with lever trolley SU109224A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU565711A SU109224A1 (en) 1957-01-31 1957-01-31 Airplane landing gear with lever trolley

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU565711A SU109224A1 (en) 1957-01-31 1957-01-31 Airplane landing gear with lever trolley

Publications (1)

Publication Number Publication Date
SU109224A1 true SU109224A1 (en) 1957-11-30

Family

ID=48382271

Family Applications (1)

Application Number Title Priority Date Filing Date
SU565711A SU109224A1 (en) 1957-01-31 1957-01-31 Airplane landing gear with lever trolley

Country Status (1)

Country Link
SU (1) SU109224A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2520266C1 (en) * 2010-06-16 2014-06-20 Мессье - Бюгатти - Довти Aircraft main landing gear with two bobs articulated with aircraft airframe

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2520266C1 (en) * 2010-06-16 2014-06-20 Мессье - Бюгатти - Довти Aircraft main landing gear with two bobs articulated with aircraft airframe

Similar Documents

Publication Publication Date Title
US2130914A (en) Shock strut
US1891188A (en) Airplane landing gear
SU109224A1 (en) Airplane landing gear with lever trolley
US4172570A (en) Landing gear in-flight vibration dampener
US2326210A (en) Aircraft landing gear
GB363811A (en) Improvements in and relating to resilient suspensions for motor road vehicles and the like
US2201438A (en) Independent wheel suspension
GB728401A (en) Improvements in or relating to shock absorbing device for the suspension of vehicles
US2466110A (en) Device for absorbing oscillations
RU2649111C1 (en) Aircraft landing gear
GB821185A (en) New or improved vehicle road wheel suspension
US1735852A (en) Landing gear for airplanes
US3091418A (en) Aircraft alighting gear
GB768379A (en) Improvements relating to the chassis and frames of caravans, trailers and the like
GB393445A (en) Improvements in or relating to aircraft landing gear
US1943887A (en) Shock absorbing strut for aeroplanes
US1840900A (en) Airplane landing gear
US1853312A (en) Aircraft landing gear
GB566570A (en) Improved torsional controlling means for independent front wheel suspensions of road vehicles
US2089263A (en) Stabilizer for vehicles
US1223705A (en) Shock-absorber for vehicles.
US1988093A (en) Landing gear
US1370693A (en) Airplane landing-gear
US1803039A (en) Aeroplane chassis
US1733365A (en) Vehicle spring