FIELD: aeronautical engineering. SUBSTANCE: shock-absorber - hydraulically operated hoist includes liquid-spring gas shock-absorber with low- and high-pressure chambers. Hydraulically operated hoist is located between low- and high-pressure chambers; cylinder of this hoist is rigidly connected with cylinder of low-pressure chamber and rod is connected with piston provided with locking device for keeping the rod from motion when in inoperative position; it is rigidly connected with high-pressure chamber and may reciprocate over cylinder of hydraulically operated hoist; cavity of hydraulically operated hoist is separated from cavities of low- and high-pressure chambers by bottom of low-pressure chamber and crown of rod of high-pressure chamber. Shock-absorber - hydraulically operated hoist is additionally provided with device for excluding turn of rod of hydraulically operated hoist relative to its cylinder. EFFECT: enhanced efficiency of hoisting and dampening of main undercarriage leg of helicopter. 2 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
FLYING VEHICLE UNDERCARRIAGE LEG SHOCK ABSORBER | 2000 |
|
RU2183180C2 |
TWO-CHAMBER SHOCK ABSORBER-JACK OF FLYING VEHICLE | 1995 |
|
RU2145294C1 |
AIRCRAFT RETRACTABLE LANDING GEAR (VERSIONS) | 2013 |
|
RU2534836C1 |
FLYING VEHICLE LANDING GEAR SHOCK-ABSORBER | 1997 |
|
RU2188143C2 |
METHOD FOR MEASUREMENT OF FREE THRUST OF HELICOPTER MAIN ROTOR IN THE HOVER MODE | 1998 |
|
RU2157977C2 |
CLUSTER OF DETACHABLE EXTERNAL FUEL TANKS OF HELICOPTER | 1996 |
|
RU2112711C1 |
FLYING VEHICLE RETRACTABLE UNDERCARRIAGE LEG | 1996 |
|
RU2183179C2 |
FLYING VEHICLE LANDING GEAR SHOCK ABSORBER AND METHOD OF FILLING HYDRAULIC CHAMBER OF FLYING VEHICLE LANDING GEAR SHOCK ABSORBER | 1990 |
|
RU2057687C1 |
METHOD OF FLYING VEHICLE CLEARANCE CHANGE AT PARKING AND ACTUATING STRUT (VERSIONS) | 2016 |
|
RU2628002C1 |
METHOD OF TRANSPORTING Mi-8 HELICOPTER BY TRAILER AND EQUIPMENT FOR LOCATING AND LOCKING HELICOPTER FOR TRANSPORTATION | 2007 |
|
RU2347711C2 |
Authors
Dates
2000-08-20—Published
1998-02-12—Filed