FIELD: aeronautical engineering. SUBSTANCE: hydropneumatic shock absorber has housing where rod with piston is arranged. Mounted in rod under its piston is floating piston with cylindrical rod provided with profiled grooves. Shock absorber has pneumatic and hydraulic chambers and ratio of area of cylindrical rod to area of floating piston ranges from 0.25 to 0.5. EFFECT: enhanced efficiency of reduction of dynamic loads transmitted to flying vehicle during its motion over rough surface of runway at high loads. 3 dwg
Title | Year | Author | Number |
---|---|---|---|
TWO-CHAMBER SHOCK ABSORBER | 1994 |
|
RU2081031C1 |
0 |
|
SU266575A1 | |
0 |
|
SU525581A1 | |
TWO-CHAMBER SHOCK ABSORBER-JACK OF FLYING VEHICLE | 1995 |
|
RU2145294C1 |
0 |
|
SU245169A1 | |
HYDROPNEUMATIC DAMPER | 2001 |
|
RU2216665C2 |
FLYING VEHICLE LANDING GEAR SHOCK ABSORBER AND METHOD OF FILLING HYDRAULIC CHAMBER OF FLYING VEHICLE LANDING GEAR SHOCK ABSORBER | 1990 |
|
RU2057687C1 |
GAS-LIQUID SHOCK-ABSORBER FOR LANDING GEAR OF VEHICLE | 1983 |
|
RU1145602C |
HYDROPNEUMATIC SHOCK ABSORBER | 0 |
|
SU1357618A1 |
Authors
Dates
1995-09-20—Published
1992-08-12—Filed