FIELD: engineering of equipment for use with aircrafts.
SUBSTANCE: in accordance to rescuing method, when aircraft is in dangerous situation, active values of pitch and bank angles are measured, as well as speed and changing direction of banking and pitching angles, and parachute is extended by means of rocket with gunpowder charge. Value of height, speed and descent acceleration are registered. Command for changing direction is transferred to control organs of rocket, to move rocket vertically upwards. At the same it is determined if current height value is critical or less than critical, and current values of pitching and banking angles do not exceed maximal allowed values.
EFFECT: expanded functional capabilities related to rescuing the aircraft.
2 cl
| Title | Year | Author | Number |
|---|---|---|---|
| HELICOPTER RESCUE DEVICE | 2001 |
|
RU2228884C2 |
| FLYING VEHICLE RECOVERY FACILITY | 2001 |
|
RU2191140C1 |
| METHOD OF SHORT TAKEOFF OF FLYING VEHICLE | 2004 |
|
RU2255028C1 |
| ACTIVE ON-BOARD FLIGHT-SAFETY SYSTEM | 2001 |
|
RU2223542C2 |
| METHOD OF CHECK AND CONTROL OF FUNCTIONAL AND PHYSIOLOGICAL CONDITION OF PILOT IN FLIGHT AND DEVICE FOR REALIZATION OF THIS METHOD | 2000 |
|
RU2170953C1 |
| METHOD OF RESPIRATORY SUPPORT OF OPERATOR DURING WORK | 2001 |
|
RU2210394C2 |
| AIR MISSILE LAUNCH SYSTEM | 2006 |
|
RU2324130C1 |
| METHOD FOR DETERMINATION OF LOCATION OF VEHICLE SUFFERING DISASTER AND SUPPORT OF VEHICLE OPERATOR | 2004 |
|
RU2240587C1 |
| TRAINING TECHNIQUES FOR PERSONS OF DANGEROUS OCCUPATIONS | 2006 |
|
RU2325935C2 |
| COOLING UNIT | 2003 |
|
RU2236989C1 |
