FIELD: transport.
SUBSTANCE: inventions relate to aircraft engineering, more specifically to aircraft engine mounting device, power plant and the aircraft with such power plant. Mounting device contains rigid structure forming torsional box and thrust load taking device which contains metal fixing element (34) hard mounted on the torsional box using fastening facilities (40). The fastening facilities (40) contain anchor pin (50) installed on longeron (17) and comprising the main part (54) located outside the torsional box. Herewith, the part (54) of the pin (50) passes through metal fixing element (34) which is pressed to longeron (17) using support cup washer (68) enveloping the main part (54) and being pressed by the screw (72) passing through it. The screw (72) is screwed into splined nut (78) installed in the hole (74) made inside the main part (54).
EFFECT: simplified maintenance of aircraft engine suspension assembly.
7 cl, 3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT ENGINE ATTACHMENT STRUT | 2006 |
|
RU2389657C2 |
| AIRCRAFT ENGINE STUB | 2006 |
|
RU2406658C2 |
| AIRCRAFT ENGINE ASSEMBLY UNIT | 2005 |
|
RU2381148C2 |
| AIRCRAFT POWER PLANT COMPRISING ENGINE AND ENGINE PYLON | 2006 |
|
RU2401222C2 |
| AIRCRAFT ENGINE ASSEMBLY | 2005 |
|
RU2381149C2 |
| AIRCRAFT POWER PLANT COMPRISING ENGINE AND ENGINE ATTACHMENT POST | 2006 |
|
RU2394730C2 |
| AIRCRAFT POWER PLANT WITH ENGINE AND ATTACHMENT STRUT | 2006 |
|
RU2420430C2 |
| AIRCRAFT POWER PLANT COMPRISING ENGINE AND ATTACHMENT OF SAID ENGINE | 2006 |
|
RU2424949C2 |
| NUT SYSTEM AND AIRCRAFT ENGINE STRUT WITH SAID SYSTEM | 2006 |
|
RU2428356C2 |
| AIRCRAFT TURBOJET ENGINE ATTACHMENT STRUT | 2006 |
|
RU2399558C2 |
