SU343544A1 - CLEANING AIRCRAFT CHASSIS - Google Patents
CLEANING AIRCRAFT CHASSISInfo
- 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
Links
Landscapes
- Fluid-Damping Devices (AREA)
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.
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)
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 |
-
1970
- 1970-10-05 SU SU1479471/23A patent/SU343544A1/en active
Cited By (1)
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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