FIELD: transport.
SUBSTANCE: turbojet engine pod of aircraft contains front air intake section, middle section enveloping turbojet engine fan and rear section (1) which has inner structure (6) functioning as casing for rear pert of turbojet engine and forming together with outer structure (5) the path (7) for secondary flow circulation. Inner structure is provided with radial extension pieces (61, 62) which pass through path and by which it is connected with inner panel (51) of outer structure using stiffening element (110, 205-210) which is generally L-shaped. The stiffening element is also attached to outer panel (52) of outer structure.
EFFECT: prevention of connecting ribs turn.
9 cl, 10 dwg
| Title | Year | Author | Number |
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RU2480567C2 |
| AIRCRAFT ASSEMBLY WITH ENGINE MOVING NACELLE | 2008 |
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RU2472678C2 |
