Turbojet engine suspension using a double rear support
US-2015377136-A1 · Dec 31, 2015 · US
US8950702B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-8950702-B2 |
| Application number | US-1623408-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jan 18, 2008 |
| Priority date | Jan 18, 2008 |
| Publication date | Feb 10, 2015 |
| Grant date | Feb 10, 2015 |
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A mounting arrangement for a gas turbine engine includes a pylon mount structure that has a fore mount portion and an aft mount portion. A first engine mount beam is integrally formed with the fore mount portion as a single-piece component, and a second engine mount beam is integrally formed with the aft mount portion as a single-piece component. The first engine mount beam is attachable to the engine case at a fore attachment interface, and the second engine mount beam is attached to the engine case at an aft attachment interface.
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What is claimed is: 1. A mounting arrangement for a gas turbine engine comprising: a pylon mount structure having a first mount portion and a second mount portion positioned aft of said first mount portion, said first and said second mount portions comprising separate components to be independently attached to a pylon; a first engine mount beam integrally formed with said first mount portion as a single-piece component, said first engine mount beam being attachable to an engine…
Operations & Transport · mapped topic
Operations & Transport · mapped topic
Cross-Sectional Technologies · mapped topic
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