FIELD: transport.
SUBSTANCE: turbojet comprises front blower, intermediate housing with outer shell and hub arranged behind the blower and interconnected by radial arms, and outlet housing with outer shell on common axle. Proposed attachment comprises front fastener at intermediate housing, rear fastener with small links of rear fastener connected with outlet housing outer shell, two thrust transmission links attached to intermediate housing bush at its front. Plane formed by said two small links is inclined forward relative to outlet housing plane.
EFFECT: decreased local flexures of housing.
18 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| TURBOJET HINGED TO AIRCRAFT PYLON | 2008 |
|
RU2487056C2 |
| AIRCRAFT GAS TURBINE ENGINE MOUNT BAR | 2010 |
|
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| GAS TURBINE ENGINE CONTAINING SUSPENSION MEANS | 2019 |
|
RU2784242C2 |
| AIRCRAFT ENGINE WITH SUSPENSION APPLIANCES | 2005 |
|
RU2372256C2 |
| GAS TURBINE ENGINE MOUNTED ON PYLON OF AIRCRAFT FUSELAGE BY APPARATUS ENSURING SAFETY OF SUSPENSION | 2011 |
|
RU2583243C2 |
| ISOSTATIC SUSPENSION OF A TURBOJET BY REAR DOUBLE SUPPORT | 2014 |
|
RU2682206C2 |
| TURBOJET ENGINE FRONT SUSPENSION TO AIRCRAFT PYLON | 2006 |
|
RU2398715C2 |
| TURBOJET COLD FLOW CHANNEL SUSPENSION AT EXHAUST HOUSING, USING RODS AND RADIAL FORKS | 2012 |
|
RU2618142C2 |
| GAS TURBINE ENGINE SUSPENSION UNIT | 2019 |
|
RU2789803C2 |
| ATTACHMENT OF MULTISTAGE TURBOJET TO AIRCRAFT | 2009 |
|
RU2483004C2 |
