FIELD: aeronautical engineering; construction of flying vehicle landing gear. device includes load-bearing bead fitted inside rod and engageable with thrust end of intermediate bottom. Intermediate bottom is provided with stops embracing the load-bearing bead, thus locking the intermediate bottom longitudinal displacement relative to rod. Besides that, load-bearing bead is provided with mounting slots for respective stops. EFFECT: reduced mass of shock-absorber and labor consumption. 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FLYING VEHICLE UNDERCARRIAGE LEG SHOCK ABSORBER | 2000 |
|
RU2183180C2 |
| FLYING VEHICLE LANDING GEAR SHOCK-ABSORBER | 1997 |
|
RU2188143C2 |
| FLYING VEHICLE RETRACTABLE UNDERCARRIAGE LEG | 1996 |
|
RU2183179C2 |
| FLYING VEHICLE LANDING WHEEL TURN CONTROL MECHANICAL | 1999 |
|
RU2167786C1 |
| TWO-CHAMBER SHOCK ABSORBER-JACK OF FLYING VEHICLE | 1995 |
|
RU2145294C1 |
| RETRACTABLE LANDING GEAR FOR FLYING VEHICLE | 2003 |
|
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| HYDRAULIC HOIST | 2005 |
|
RU2297382C2 |
| OIL-WELL CENTRIFUGAL SECTIONAL PUMP | 2001 |
|
RU2197643C2 |
| FLYING VEHICLE LANDING GEAR SHOCK-ABSORBER | 1991 |
|
RU2051073C1 |
| HYDRAULIC DAMPER | 1997 |
|
RU2135856C1 |
