FIELD: aerospace engineering; relieving pressure from cavity of flying vehicle to ensure dust and moisture protection. SUBSTANCE: device has cylinder-and-piston drive with return spring engageable with cover provided with elastic trapezoidal cross-section seal with projecting inclined flexible tab and stop engageable with rod of drive. According to first version, stop is made in form of outer race of bearing whose inner race is secured inside symmetric lugs of cover. According to second version, stop has inclined surface whose angle of inclination relative to plane normal to stroke of rod is half of angle of opening of cover. When pressure is present in actuating cylinder of drive, rod holds cover through in closed position and when pressure is relieved, cover opens under action of return spring. EFFECT: enhanced operational reliability; enhanced sealing of cover. 3 cl, 9 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR OPENING AND CLOSING WINDOWS OF FLYING VEHICLE | 2000 |
|
RU2198822C2 |
DEVICE FOR OPENING AND CLOSING AIRCRAFT WINDOWS | 2011 |
|
RU2480373C1 |
PROTECTIVE UNIT FOR FILLER NECK | 2001 |
|
RU2209749C1 |
DISTRIBUTING VALVE OF SHIP FIRE EXTINGUISHING SYSTEM | 2014 |
|
RU2594938C2 |
VENT-SAFETY VALVE | 1998 |
|
RU2142592C1 |
0 |
|
SU374216A1 | |
SUBASSEMBLY UNIT FOR DISCONNECTION OF FLIGHT VEHICLE PARTS | 1999 |
|
RU2150665C1 |
DOOR AIR DISTRIBUTION DEVICE AND ELECTROPNEUMATIC VALVE FOR AIR DISTRIBUTION DEVICE | 2004 |
|
RU2282702C2 |
DEVICE FOR FLOATING DEVICE SEPARATION INTO PRESSURE-TIGHT COMPARTMENTS | 2019 |
|
RU2705722C1 |
DEVICE FOR PROTECTION OF SPACECRAFT OPTICAL SURFACES | 2000 |
|
RU2188779C2 |
Authors
Dates
1999-07-10—Published
1998-03-27—Filed