Tandem thrust reverser with multi-bar linkage
US-2015121839-A1 · May 7, 2015 · US
Full ring sliding nacelle with thrust reverser
US9435293B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9435293-B2 |
| Application number | US-201414187027-A |
| Country | US |
| Kind code | B2 |
| Filing date | Feb 21, 2014 |
| Priority date | Feb 22, 2013 |
| Publication date | Sep 6, 2016 |
| Grant date | Sep 6, 2016 |
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- Title
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Abstract
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A gas turbine engine includes a first annular portion that is stationary and adapted for partially surrounding an engine core. The first annular portion includes a fore pylon connecting portion. The gas turbine engine also includes a rail coupled to the fore pylon and extending in the aft direction from the first annular portion. The gas turbine engine also includes a second annular portion, arranged aft of the first portion and coupled to the rail. The second annular portion is movable along an engine core centerline between a closed position and at least one open position. The second annular portion is configured to engage the first annular portion in the closed position, thereby providing access to the engine core. The gas turbine engine further comprises a thrust reverser arranged in the second annular portion.
First claim
Opening claim text (preview).
The invention claimed is: 1. A gas turbine engine comprising: a fore pylon; a first annular portion that is stationary and adapted for partially surrounding an engine core, the first annular portion including a fore pylon connecting portion; a rail coupled to the fore pylon and extending in an aft direction from the first annular portion; a second annular portion, aft of the first annular portion and coupled to the rail, the second annular portion being movable along an engi…
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Frequently asked questions
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- What does patent US9435293B2 cover?
- A gas turbine engine includes a first annular portion that is stationary and adapted for partially surrounding an engine core. The first annular portion includes a fore pylon connecting portion. The gas turbine engine also includes a rail coupled to the fore pylon and extending in the aft direction from the first annular portion. The gas turbine engine also includes a second annular portion, ar…
- Who is the assignee on this patent?
- United Technologies Corp
- What technology area does this patent fall under?
- Primary CPC classification F02K1/605. Mapped technology areas include Mechanical Engineering.
- When was this patent published?
- Publication date Tue Sep 06 2016 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
- What related patents are in patentsdb?
- We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).