FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering. Device for opening rotary flap opening in airframe of aircraft comprises remotely controlled multi-link mechanism of opening fold and lock locking flap, holding it in closed position. Flap opening mechanism comprises tension spring (4), a spring tensioning mechanism (5), double-arm rocker (6) fixed on glider structure (7) with possibility of rotation, and tie-rod (8), which is pivotally connected by one end (9) to first arm (10) of rocking arm (6), and second (11) – with rotary flap (1). Tension spring (4) is pivotally connected by first end (12) to second arm (13) of rocker (6), and by second (14) – to actuating element (15) of the tension mechanism of spring (5). Spring tensioning mechanism (5) is designed to hold stretched spring (5).
EFFECT: invention is aimed at reducing opening time of the opening flap, increasing durability and failure-free operation.
3 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
VEHICLE ROCKING DOOR SECURING DEVICE | 2022 |
|
RU2791947C1 |
VEHICLE ROCKING DOOR SECURING DEVICE | 2022 |
|
RU2791946C1 |
DOOR FOR AIRCRAFT (VERSIONS) AND DOOR UPPER HINGE MECHANISM | 2014 |
|
RU2548644C1 |
SYSTEM OF OPERATIONAL AND EMERGENCY EXIT | 2006 |
|
RU2301176C1 |
EMERGENCY EXIT OPENING SYSTEM | 2008 |
|
RU2376206C1 |
AIRCRAFT LANDING GEAR WELL FRONT FLAP DRIVE | 2010 |
|
RU2427502C1 |
AIRCRAFT CREW CABIN WINDOW LEAF | 2011 |
|
RU2475413C1 |
CABLE TENSIONER FOR CONTROL SYSTEM | 2000 |
|
RU2180640C2 |
DEVICE TO AIRCRAFT EMERGENCY POWER PLANT INITIATION | 2009 |
|
RU2396186C1 |
DEVICE FOR EMERGENCY OPENING OF ELECTRICALLY OPERATED DOOR OF LIFT CABIN | 2004 |
|
RU2263621C1 |
Authors
Dates
2020-01-29—Published
2019-05-24—Filed