FIELD: aircraft and aerospace engineering.
SUBSTANCE: proposed flight vehicle compartment comprises skin with vent hole, spring-loaded cover pivoted in said skin vent hole. Said cover also comprises vent hole to accommodate spring-loaded flap pivoted therein flush with cover surface. Compartment skin is furnished with limit stop restricting cover travel from compartment, while cover and flap incorporates limit stop to restrict, on the one hand, flap travel into compartment to allow cover to move together with flap into compartment, and, on the other hand, flap travel into ambient medium.
EFFECT: pressure control in flight vehicle compartment in ascent/descent, and simplified design.
12 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT COMPARTMENT | 2008 |
|
RU2374129C1 |
| LOAD-BEARING PANEL OF SPACECRAFT CASE (VERSIONS) | 2004 |
|
RU2283799C2 |
| LOAD-BEARING PANEL OF SPACECRAFT SOLAR BATTERY (VERSIONS) | 2004 |
|
RU2283798C2 |
| AFT BODY OF AIRCRAFT WITH ANNULAR LOCATION OF JET ENGINE NOZZLES ON ITS BOTTOM PROTECTION (VERSIONS) | 2013 |
|
RU2557125C2 |
| METHOD FOR DETERMINATION OF FLOW-RATE CHARACTERISTICS OF DRAINAGE DEVICES OF FLIGHT VEHICLE COMPARTMENT AND SYSTEM FOR ITS REALIZATION | 2003 |
|
RU2253095C2 |
| FLYING VEHICLE COMPARTMENT | 1999 |
|
RU2164883C1 |
| METHOD OF DETERMINATION OF FLOW RATE CHARACTERISTICS OF DRAINAGE FACILITIES OF FLYING VEHICLE CASE AND SYSTEM FOR REALIZATION OF THIS METHOD | 2003 |
|
RU2267108C2 |
| METHOD OF CONTROL OF AERODYNAMIC LOADS ACTING ON AIRCRAFT COMPARTMENTS AND DEVICE FOR REALIZATION OF THIS METHOD (VERSIONS) | 1999 |
|
RU2145563C1 |
| ROCKET-CARRIER ASCENT UNIT | 2007 |
|
RU2355607C1 |
| SHUT-OFF DEVICE FOR WELL TESTING | 2000 |
|
RU2187639C1 |
