FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to seal of joint between aircraft fuselage and wing. Seal assy comprises elongated bellows to be secured to fuselage and wing front box. Said bellows feature flat, flexed or wavy (omega-shape) cross-section with two lengthwise lateral parts. One lateral part is secured to wing box whole another one is attached to fuselage by means of appropriate mounts. Said mounts make a lock seam for attachment of bellows to airframe mounts. Seal assy seals the clearance between fuselage and wing to maintain pressure in tight fuselage.
EFFECT: reliable seal for aircraft with detachable wing.
13 cl, 10 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SEALING ELEMENT | 2009 |
|
RU2518142C2 |
| MULTI-PURPOSE WELL CONNECTION UNIT WITH THE USE OF MECHANICAL RIGID ELEMENTS | 2014 |
|
RU2651659C1 |
| INTERSECTION OF MULTI-SHAFT WELL WITH USE OF MECHANICAL ELEMENTS OF STIFFENESS | 2014 |
|
RU2643248C1 |
| HYBRID AIRCRAFT | 1996 |
|
RU2160689C2 |
| PRESSURE BULKHEAD AND METHOD FOR DIVISION OF INTERIOR SPACE OF AIRCRAFT OR SPACECRAFT | 2008 |
|
RU2471672C2 |
| END AIRFOILS WITH RECESSES AND APPROPRIATE SYSTEMS AND METHODS | 2009 |
|
RU2492111C2 |
| WING LEADING EDGE FLAP UNIT | 1996 |
|
RU2181332C2 |
| APPARATUS AND METHODS FOR JOINING AIRCRAFT COMPOSITE STRUCTURES | 2014 |
|
RU2666593C2 |
| SEAL WITH INTEGRATED JOINT SURFACE | 2008 |
|
RU2463511C2 |
| MECHANICALLY DISTRIBUTED POWER PLANT AND METHOD OF AIRCRAFT OPERATION CONTROL | 2019 |
|
RU2743903C2 |
