FIELD: aircrafts.
SUBSTANCE: group of inventions relates to the suspension of power plants of short take-off and landing aircraft. Suspension and thrust angle control unit of the engine contains rods and dampers located in pylons. Unit further comprises a hydraulic cylinder with a stem and hydraulic locks for fixing the rod in extreme positions thereof. Rods with dampers form two vertical engine mount belts. Hydraulic cylinder body is hinged at its end on an additional rod with a damper, and the hydraulic cylinder rod is hinged on the engine.
EFFECT: simplified design of the rotation unit of the thrust vector of an aircraft engine is achieved, and the efficiency of controlling the angle of the thrust vector of the engine is increased.
8 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| COMPOUND HELICOPTER | 1994 |
|
RU2089456C1 |
| VTOL AIRCRAFT LIFT INCREASING DEVICE | 2013 |
|
RU2561886C2 |
| UNMANNED JET-HELICOPTER | 2018 |
|
RU2699513C1 |
| HYBRID JET PLANE-HELICOPTER | 2019 |
|
RU2706430C1 |
| HEAVY HIGH-SPEED ROTARY-WING AIRCRAFT | 2016 |
|
RU2608122C1 |
| MULTI-PURPOSE HIGH-SPEED HELICOPTER AIRCRAFT | 2017 |
|
RU2673317C1 |
| MULTI-PURPOSE DECK HELICOPTER AIRCRAFT | 2017 |
|
RU2652861C1 |
| MODULAR X-WING AIRCRAFT FOR ARCTIC ROCKET AVIATION COMPLEXES | 2020 |
|
RU2743311C1 |
| SURFACE-SUBMERGED SHIP WITH DECK AIR STRIKE COMPLEX | 2019 |
|
RU2721808C1 |
| MULTI-PURPOSE CRYOGENIC CONVERTIPLANE | 2009 |
|
RU2394723C1 |
