FIELD: aviation.
SUBSTANCE: invention is related to the field of aviation engineering, more precisely - to uncoupling of airplane lantern collapsible part. Uncoupling unit comprises facility for connection of lantern collapsible part frame to suspension beam, which is arranged with the possibility of installation on fuselage. Facility includes bolt and stop. Bolt has thread on one side from head for installation on lantern collapsible part, and on the other side pin is installed, which is arranged with the possibility of installation in transverse opening of beam. Stop is installed with the possibility of interaction with pin during displacement of suspension beam in longitudinal hole.
EFFECT: invention is aimed at reduction of pneumatic hydraulic cylinder force pulse losses for separation from suspension beam in case of emergency drop of lantern collapsible part.
4 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT HINGED CANOPY DRIVE AND TIME VALVE | 2008 |
|
RU2372249C1 |
| AIRCRAFT CANOPY OPENING-CLOSING CONTROL SYSTEM | 2004 |
|
RU2255878C1 |
| MULTI-PURPOSE HIGHLY MANOEUVRABLE SUPERSONIC AIRCRAFT, ITS AIRFRAME, EQUIPMENT AND SYSTEMS | 1996 |
|
RU2207968C2 |
| CANOPY DISPLACING AND LOCKING MECHANISM | 2012 |
|
RU2487818C1 |
| CYLINDER OF CANOPY CONTROL | 2012 |
|
RU2492366C1 |
| FLYING VEHICLE WITH PASSENGER EMERGENCY AND RESCUE MODULES | 2000 |
|
RU2172277C1 |
| PASSENGER AIRCRAFT WITH RESCUE MODULES AND COMBINED POWER PLANT | 2022 |
|
RU2781717C1 |
| AIRCRAFT CANOPY EMERGENCY OPENING CONTROL SYSTEM | 2022 |
|
RU2783689C1 |
| SUPERSONIC VERTICAL TAKEOFF AND LANDING PASSENGER AIRCRAFT | 2002 |
|
RU2225331C1 |
| AIRPLANE WITH SYSTEM OF GENERAL-AIRPLANE EQUIPMENT CONTROL | 2007 |
|
RU2359868C2 |
