FIELD: aerospace engineering.
SUBSTANCE: set of invention relates to aircraft engineering and covers the aircraft landing gear manipulation system and aircraft proper. Landing gear is hinged in landing gear room closed by doors. Aforesaid room incorporates control unit to activate various manipulation jobs, door control circuit and landing gear control circuit. Aforesaid unit and circuits are supplied from power supply in normal flight conditions, in stand-by and servicing conditions.
EFFECT: reduced weight and increased useful space.
12 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CONTROLLED POWER TRANSMISSION UNIT OF AIRCRAFT HYDRAULIC SYSTEM | 2023 |
|
RU2814642C1 |
| CONTROLLED POWER TRANSMISSION UNIT OF HYDRAULIC SYSTEM OF AIRCRAFT | 2023 |
|
RU2814901C1 |
| AIRCRAFT UNDERCARRIAGE SECTION FLAP CONTROL DEVICE | 2010 |
|
RU2527604C2 |
| AIRCRAFT CONTROL SYSTEM | 2011 |
|
RU2556474C2 |
| EMERGENCY RELEASE SYSTEM BY FREE FALL UNDER GRAVITY FOR NODES OF AIRCRAFT RETRACTABLE LANDING GEAR | 2014 |
|
RU2613677C2 |
| DEVICE FOR OPENING OF ROTARY FLAP OPENING IN AIRFRAME OF AIRCRAFT | 2019 |
|
RU2712465C1 |
| EMERGENCY DRIVE CHASSIS EXTENSION | 2022 |
|
RU2780009C1 |
| CONTROLLED POWER TRANSMISSION UNIT OF AIRCRAFT HYDRAULIC SYSTEM | 2023 |
|
RU2814840C1 |
| ELECTRICAL CONTROL SYSTEM FOR TURBOJET ENGINE THRUST REVERSER | 1997 |
|
RU2142569C1 |
| DEVICE FOR AIRCRAFT EMERGENCY POWER SUPPLY AND AIRCRAFT EQUIPPED WITH SUCH DEVICE | 2013 |
|
RU2631162C2 |
