FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering and can be used in aft bodies of aircrafts. The aft body of the aircraft with the annular location of jet engine nozzles on the bottom protection with a heat-resistant reflector of a backflow of jet engine jets in the form of a rotation body includes a drain hole with a direct-acting pneumatic valve with a shutoff sensitive element in the form of a heat-resistant reflector of the backflow of the jet engine jets.
EFFECT: invention allows increasing the structural strength and improving the operating reliability of the aircraft aft body.
3 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF FIRE PREVENTION IN TAIL COMPARTMENTS OF LAUNCH VEHICLES AND FIRE PREVENTION SYSTEM IN THESE COMPARTMENTS | 2003 |
|
RU2247687C1 |
| ROCKET-CARRIER ASCENT UNIT | 2007 |
|
RU2355607C1 |
| SYSTEM OF SPACECRAFT THERMAL PROTECTION | 2007 |
|
RU2360849C2 |
| METHOD OF CONTROL OF AERODYNAMIC LOADS ACTING OF FLYING VEHICLE CASE AND DEVICE FOR REALIZATION OF THIS METHOD (VERSIONS) | 1999 |
|
RU2145564C1 |
| AEROSPACE AIRCRAFT | 2010 |
|
RU2436715C2 |
| AQUA AEROSPACE VEHICLE | 2012 |
|
RU2626418C2 |
| METHOD OF CONTROL OF AERODYNAMIC LOADS ACTING ON AIRCRAFT COMPARTMENTS AND DEVICE FOR REALIZATION OF THIS METHOD (VERSIONS) | 1999 |
|
RU2145563C1 |
| DEVICE AND METHOD FOR CONTROL OF SPACE VEHICLE LANDING | 1994 |
|
RU2097286C1 |
| ACCELERATION ENGINE INSTALLATION | 2002 |
|
RU2211358C1 |
| METHOD OF DETERMINATION OF FLOW RATE CHARACTERISTICS OF DRAINAGE FACILITIES OF FLYING VEHICLE CASE AND SYSTEM FOR REALIZATION OF THIS METHOD | 2003 |
|
RU2267108C2 |
