FIELD: aircraft engines. SUBSTANCE: thrust reverser consists of two articulated semishells. Proposed thrust reverser and housing are connected by relatively penetrating inner connecting members and outer connecting members coupled according with housing semishells. Outer connecting members have support surface radially turned outside. Inner connecting members are provided with great number of tongues capable of covering support surface is closed position and releasing the support surface in open position. Such design of device precludes separation f spacers and chute without interfering with controlled (arbitrary) opening of reverser semishells without increasing weight of engine groups. EFFECT: enhanced reliability of operation. 12 cl, 10 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD AND DEVICE FOR CLOSING THRUST REVERSAL DOOR | 1997 |
|
RU2150596C1 |
| THRUST REVERSER WITH CASCADES AND OPTIMIZED- CONTROL WORKING CYLINDER | 1998 |
|
RU2150595C1 |
| TURBOJET ENGINE ONE-SHELL THRUST REVERSER | 1996 |
|
RU2145387C1 |
| THRUST REVERSER FOR TURBOJET ENGINE WITH DOORS CONNECTED TO FRONT PANEL FORMING INTAKE | 1996 |
|
RU2133861C1 |
| TURBOENGINE PROTECTION SHIELD | 1995 |
|
RU2122124C1 |
| THRUST REVERSER WITH DOORS AND OPTIMIZED INSTALLATION OF CONTROL JACK | 1997 |
|
RU2145388C1 |
| TURBOJET ENGINE THRUST REVERSER | 1992 |
|
RU2101534C1 |
| SINGLE-SIDED-ACCESS TURNING DEVICE COUPLING MOVABLE MEMBER WITH FIXED STRUCTURE | 1997 |
|
RU2156873C2 |
| DEVICE MEASURING AXIAL THRUST ON ROTATING SHAFT | 1998 |
|
RU2160435C2 |
| THRUST REVERSER OF TURBOJET ENGINE | 1992 |
|
RU2069782C1 |
