FIELD: engines and pumps.
SUBSTANCE: nacelle (5) cowl for jet turbine engine is equipped with fixed (6) part and moving (7) part. The said cowl parts are located one above the other. Note that the moving part is performed with the possibility of movement along the fixed part from the closed position, in which moving part is running as extension of the fixed part, into open position, in which moving part partially covers the fixed part.
EFFECT: prevention of sudden nacelle cowl opening during the flight.
10 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TURBOJET NACELLE WITH SLIDING FRONT COWL | 2009 |
|
RU2505458C2 |
| TURBOJET NACELLE | 2009 |
|
RU2500588C2 |
| TURBOJET NACELLE | 2010 |
|
RU2524321C2 |
| TURBOJET NACELLE MOVING COWL DRIVE AND CONTROL SYSTEM | 2009 |
|
RU2494016C2 |
| DEVICE TO CONTROL DRIVES OF TURBOJET NACELLE COWLING SERVICING | 2008 |
|
RU2466910C2 |
| TURBOJET ENGINE NACELLE REINFORCING STRUCTURE | 2011 |
|
RU2569725C2 |
| POWER CYLINDER FOR OPENING OF COWLING OF NACELLE OF AIRCRAFT ENGINE, AND NACELLE EQUIPPED WITH SUCH CYLINDER | 2008 |
|
RU2471090C2 |
| TURBOJET ENGINE CAR EQUIPPED WITH MECHANICAL SYSTEM OF THRUST REVERSER BLOCKING | 2008 |
|
RU2493396C2 |
| DETACHABLE AIR INTAKE FOR TURBOJET NACELLE | 2007 |
|
RU2451804C2 |
| TURBOJET NACELLE REAR ASSEMBLY | 2008 |
|
RU2457984C2 |
