SU343544A1 - CLEANING AIRCRAFT CHASSIS - Google Patents

CLEANING AIRCRAFT CHASSIS

Info

Publication number
SU343544A1
SU343544A1 SU1479471/23A SU1479471A SU343544A1 SU 343544 A1 SU343544 A1 SU 343544A1 SU 1479471/23 A SU1479471/23 A SU 1479471/23A SU 1479471 A SU1479471 A SU 1479471A SU 343544 A1 SU343544 A1 SU 343544A1
Authority
SU
USSR - Soviet Union
Prior art keywords
lift
shock absorber
piston
landing gear
reduce
Prior art date
Application number
SU1479471/23A
Other languages
Russian (ru)
Inventor
В.Ф. Федоренко
Original Assignee
В.Ф. Федоренко
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 В.Ф. Федоренко filed Critical В.Ф. Федоренко
Priority to SU1479471/23A priority Critical patent/SU343544A1/en
Application granted granted Critical
Publication of SU343544A1 publication Critical patent/SU343544A1/en

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Abstract

1. Убирающееся шасси летательного аппарата, включающее балку, шарнирно связанную с амортизатором-подъемником, в корпусе амортизатора которого установлен поршень с полым штоком, на втором конце которого закреплен поршень подъемника, делящий корпус подъемника на подпоршневую и запоршневую рабочие полости, и шарнирные узлы крепления балки и амортизатора-подъемника к фюзеляжу, отличающееся тем, что, с целью уменьшения размеров ниши шасси, в нем шарнирные узлы крепления балки расположены на линии, перпендикулярной оси амортизатора-подъемника при максимально обжатом амортизаторе.2. Шасси летательного аппарата по п.1, отличающееся тем, что, с целью улучшения амортизационных характеристик, сокращения времени выпуска и повышения надежности работы шасси, в нем в корпусе подъемника закреплен полый плунжер с плавающим поршнем, образующий в полом штоке амортизатора дополнительную газовую камеру, а в подъемнике - компенсатор объема запоршневой полости.1. A retractable landing gear of an aircraft, including a beam pivotally connected to a shock absorber-lift, in the shock absorber case of which a piston with a hollow rod is mounted, on the second end of which a lift piston is fixed, dividing the lift case into a piston and piston and working cavities of the beam and a shock absorber-lift to the fuselage, characterized in that, in order to reduce the size of the landing gear niche, in it the hinge attachment points of the beam are located on a line perpendicular to the axis of the shock absorber-lift and at the maximum crimped amortizatore.2. Aircraft landing gear according to claim 1, characterized in that, in order to improve the damping characteristics, reduce the release time and increase the chassis reliability, a hollow plunger with a floating piston is fixed in the lift body, forming an additional gas chamber in the hollow stem of the shock absorber, in the lift - a compensator of the volume of the burrow cavity.

SU1479471/23A 1970-10-05 1970-10-05 CLEANING AIRCRAFT CHASSIS SU343544A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1479471/23A SU343544A1 (en) 1970-10-05 1970-10-05 CLEANING AIRCRAFT CHASSIS

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1479471/23A SU343544A1 (en) 1970-10-05 1970-10-05 CLEANING AIRCRAFT CHASSIS

Publications (1)

Publication Number Publication Date
SU343544A1 true SU343544A1 (en) 2005-03-10

Family

ID=60514790

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1479471/23A SU343544A1 (en) 1970-10-05 1970-10-05 CLEANING AIRCRAFT CHASSIS

Country Status (1)

Country Link
SU (1) SU343544A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2488523C2 (en) * 2008-12-05 2013-07-27 Мессье-Бюгатти-Довти Device to decrease aircraft undercarriage length

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2488523C2 (en) * 2008-12-05 2013-07-27 Мессье-Бюгатти-Довти Device to decrease aircraft undercarriage length

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