US4155221A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Turbofan engine having variable geometry fan duct
Assignee: Boeing Co
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Filing: 1976-12-27
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Granted: 1979-05-22
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Expires: 1996-12-27
Abstract
Abstract This invention is an improved turbofan engine having a variable geometry fan duct which reduces stator source noise emitted from the engine. Attached to the inner wall of the fan casing near the fan stators is a pneumatically actuated annular membrane having two operating positions. In the cruise position, the membrane is forced radially inward to press against the radially outermost tips of the fan stators. In the second position, used during approach and takeoff, the membrane is drawn against a recessed portion in the fan casing, thereby creating an annular passageway between the stator tips and the casing. When the membrane is in this position, turbulent flow from the rotor blade tips which would normally impinge on the stators is directed through the annular passageway.
Inventors
- 👤 Louis G. Dhoore
- 👤 William H. Schultz
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 22:04
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/04; F02C7/045; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/141; F02K; F02K3/00; F02K3/02; F02K3/04; F02K3/075; F04; F04D; F04D27/00; F04D27/02; F04D27/0246; F04D29/00; F04D29/08; F04D29/16; F04D29/161; F04D29/164; F04D29/40; F04D29/52; F04D29/54; F04D29/541; F04D29/542; F04D29/66; F04D29/68; F04D29/681; F05; F05D; F05D2250/00; F05D2250/70; F05D2250/71; F05D2250/711; F05D2250/712; F05D2270/00; F05D2270/30; F05D2270/333; F05D2270/60; F05D2270/65; F05D2300/00; F05D2300/40; F05D2300/43; F05D2300/431
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
143 words
A gas turbine engine of the type commonly known as a turbofan comprising: a core engine; a centerbody enclosing said core engine and having an outer wall; a fan rotor located near the forward end of said core engine; a fan casing having an inner wall enclosing said rotor and forming an annular duct between said inner wall thereof and the outer wall of said centerbody for the passage of air through the engine; a row of fan stators located downstream of said rotor, attached to said centerbody, and extending radially outward therefrom, each of said stators having a radially outermost tip located radially inward of said inner wall and defining a gap therebetween; and, a flexible membrane circumferentially disposed about the inner wall of said fan casing radially outward said tips of said fan stators and having an inner and outer surface.
Claim 2
Dependent Claim
143 words
A gas turbine engine of the type commonly known as a turbofan comprising: a core engine; a centerbody enclosing said core engine and having an outer wall; a fan rotor located near the forward end of said core engine; a fan casing having an inner wall enclosing said rotor and forming an annular duct between said inner wall thereof and the outer wall of said centerbody for the passage of air through the engine; a row of fan stators located downstream of said rotor, attached to said centerbody, and extending radially outward therefrom, each of said stators having a radially outermost tip located radially inward of said inner wall and defining a gap therebetween; and, a flexible membrane circumferentially disposed about the inner wall of said fan casing radially outward said tips of said fan stators and having an inner and outer surface.
Claim 3
Dependent Claim
24 words
The engine of claim 1 wherein the inner wall of said fan casing has a contoured recess underlying said membrane for receiving said membrane.
Claim 4
Dependent Claim
25 words
The engine of claim 1 further comprising a cylindrical shroud concentrically surrounding said centerbody and attached to the radially outermost tips of said fan stators.
Claim 5
Dependent Claim
18 words
The engine of claim 1 wherein said membrane is circumferentially flexible but substantially inflexible in the axial direction.
Claim 6
Dependent Claim
35 words
The engine of claim 2 wherein said membrane has a first operating position lying contiguous to said contoured recess and a second operating position in contact with the radially outermost tips of said fan stators.
Claim 7
Dependent Claim
33 words
The engine of claim 3 wherein said membrane has a first operating position lying contiguous to said inner wall of said fan casing and a second operating position in contact with said shroud.
Claim 8
Dependent Claim
25 words
The engine of claim 1 further comprising fluid pressure means for varying the shape of said membrane and thereby varying the area of said duct.
Claim 9
Dependent Claim
27 words
The engine of claim 7 wherein said fluid pressure means comprises means for controllably creating a pressure differential between the inner and outer surfaces of said membrane.
Claim 10
Dependent Claim
24 words
The engine of claim 7 wherein said fluid pressure means comprises means for controllably exposing the inner surface of said membrane to atmospheric pressure.
References Cited (Backward Citations)
US3611724A
Cited
US3756026A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1982-05-21 | 1982-11-20 | 1983-05-22 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1986-05-21 | 1986-11-20 | 1987-05-22 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1990-05-21 | 1990-11-20 | 1991-05-22 | $7700.00 | Window Closed / Lapsed |