Patent US4232516A successfully refreshed from Google Patents.
US4232516A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Flow deflecting devices
Assignee: Rolls Royce PLC
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Filing: 1978-09-25
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Granted: 1980-11-11
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Expires: 1998-09-25
Abstract
Abstract A translating cowl thrust reverser for a ducted fan gas turbine engine has a fan cowl, the downstream portion of which is translatable axially to open an aperture in the cowl. The aperture has upstream and downstream side-walls and which are curved to deflect fan air flow through the aperture in a forward direction. An annular plate is positioned at the outlet from the aperture and projects into the turbulent flow region on the upstream side-wall to define with the side-wall a recess open to the flow which delays the separation of the flow from the side-wall. This increases the effective area of the outlet and the angle through which the flow is turned thus improving the thrust reverser efficiency to the point at which no cascades are needed in the aperture.
Inventors
- 👤 William J. Lewis
- 👤 Leslie R. Harper
- 👤 Malcolm J. Davis
- 👤 Richard G. Gardiner
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 16:23
CPC Classifications
F; F02; F02K; F02K1/00; F02K1/54; F02K1/64; F02K1/70; F02K1/72
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
184 words
A translating cowl thrust reverser for a ducted fan gas turbine engine comprising radially inner and outer walls defining a fan duct, means for translating a portion of the radially outer wall axially to open up in the radially outer wall an aperture which has an inlet communicating with the fan duct and an outlet communicating with atmosphere, means for simultaneously blocking the fan duct as the aperture is opened and for directing flow from the fan duct into the inlet of the aperture, the aperture having upstream and downstream side-walls which are shaped to give the flow through the aperture a forward component of velocity from the outlet thereof, and a substantially axially extending at least part-annular plate extending in a downstream direction from the upstream side-wall of the aperture only into a turbulent region of the flow and terminating upstream of the downstream extent of the upstream side-wall and defining with the upstream side-wall an annular recess open to the flow and in which, in operation, the flow causes a reduced pressure to delay the onset of separation from the upstream side-wall.
Claim 2
Dependent Claim
184 words
A translating cowl thrust reverser for a ducted fan gas turbine engine comprising radially inner and outer walls defining a fan duct, means for translating a portion of the radially outer wall axially to open up in the radially outer wall an aperture which has an inlet communicating with the fan duct and an outlet communicating with atmosphere, means for simultaneously blocking the fan duct as the aperture is opened and for directing flow from the fan duct into the inlet of the aperture, the aperture having upstream and downstream side-walls which are shaped to give the flow through the aperture a forward component of velocity from the outlet thereof, and a substantially axially extending at least part-annular plate extending in a downstream direction from the upstream side-wall of the aperture only into a turbulent region of the flow and terminating upstream of the downstream extent of the upstream side-wall and defining with the upstream side-wall an annular recess open to the flow and in which, in operation, the flow causes a reduced pressure to delay the onset of separation from the upstream side-wall.
Claim 3
Dependent Claim
45 words
A translating cowl thrust reverser as claimed in claim 1 and in which the plate is fixed adjacent to the upstream portion of the radially outer wall, and the downstream portion is provided with a slot for receiving the plate when the aperture is closed.
Claim 4
Dependent Claim
51 words
A translating cowl thrust reverser as claimed in claim 1 and in which means are provided to translate the plate into its operating position as the aperture is being opened, the plate being received in a slot in the upstream portion of the radially outer wall when the aperture is closed.
References Cited (Backward Citations)
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US3524458A
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DE2216220A1
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US4047381A
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US4098073A
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1983-11-11 | 1984-05-12 | 1984-11-11 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-11-11 | 1988-05-12 | 1988-11-11 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-11-11 | 1992-05-12 | 1992-11-11 | $7700.00 | Window Closed / Lapsed |