FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly to aircraft engine attachment strut. Aircraft engine attachment strut (4) represents box-type strut made by jointing upper spar (18), lower spar (20), two side panels (22) and transverse side ribs (24) jointing spars and panels (18, 20, 22). Strut comprises rear engine suspension assembly (8) including suspension rear assembly housing (54). Said rear engine suspension assembly (8) is provided with two lateral metal fasteners (26). Each said fastener comprises lengthwise section (28) in contact with inner side (44) of lateral panel (22) fixed on aforesaid inner side (44) and crosswise section (30) that includes attachment (38) of suspension rear assembly housing (38). Note here that said crosswise section (30) can pass through cutout (48) formed in side panel (22).
EFFECT: easier mounting of engine.
23 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT ENGINE STUB | 2006 |
|
RU2406658C2 |
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|
RU2424949C2 |
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|
RU2401222C2 |
| AIRCRAFT ENGINE ASSEMBLY UNIT | 2005 |
|
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|
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|
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|
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|
RU2391259C2 |
| AIRCRAFT ENGINE ASSEMBLY | 2005 |
|
RU2381149C2 |
| AIRCRAFT POWER PLANT | 2006 |
|
RU2401223C2 |
