FIELD: engines and pumps.
SUBSTANCE: sealant to be arranged between a shutter of the rear section of a nacelle and a jet turbine engine in the airborne vehicle assembly forming a jet stream includes a cylindrical section, jaws and a longitudinal rib. Jaws project radially from the generating line of the cylindrical section; the longitudinal rib projects radially inward the cylindrical section, and maximum ratio of the overall dimension of the sealant to the thickness of material is more than 10. Jaws are oriented relative to each other in the form of V letter, and the cylindrical section is provided on its external surface with a flat surface located diametrically opposite to the jaws.
EFFECT: invention allows increasing tightness and compressibility of the seal.
8 cl, 4 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TURBOJET ENGINE NACELLE COMPRISES A SECONDARY LOOP NOZZLE WITH ROTATABLE FLAPS | 2015 |
|
RU2688082C2 |
| SEAL WITH INTEGRATED JOINT SURFACE | 2008 |
|
RU2463511C2 |
| FIXATOR | 2008 |
|
RU2463424C2 |
| DOUBLE SEALER | 2008 |
|
RU2474740C2 |
| THRUST REVERSER ACTUATOR WITH ADJUSTABLE NOZZLE FOR TURBOJET ENGINE NACELLE AND NACELLE WITH SUCH DEVICE | 2011 |
|
RU2570791C2 |
| AIRCRAFT TURBOJET NACELLE | 2008 |
|
RU2489321C2 |
| THRUST REVERSER, NACELLE CONTAINING SUCH THRUST REVERSER, AND METHOD OF CHANGE OF NOZZLE CROSS-SECTION, IMPLEMENTED USING SUCH THRUST REVERSER | 2011 |
|
RU2571705C2 |
| FLAP REVERSER | 2011 |
|
RU2570740C2 |
| THRUST REVERSER | 2010 |
|
RU2538142C2 |
| LATCH | 2008 |
|
RU2456214C2 |
