US4086761A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Stator bypass system for turbofan engine
Assignee: Boeing Co
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Filing: 1976-04-26
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Granted: 1978-05-02
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Expires: 1996-04-26
Abstract
Abstract A nacelle for use with a turbofan engine for reducing both rotor and stator source noise emitting from the engine. The nacelle contains a ducted system which when in operation bypasses a portion of the flow in the fan duct around the fan stators causing unloading of the rotor, diffusion of the flow between the rotor and the stators, a reduction in the viscous flow at the rotor tips, and a substantial elimination of the rotor tip flow. Flow enters the duct system through openings in the interior walls of the nacelle located between the rotor and fan stators but downstream of the rotor at least a certain predetermined minimum distance. Flow through the system is controlled by doors or other means and it is normally operated only during approach and take-off, thus minimizing cruise penalty on engine performance.
Inventors
- 👤 Larry Allen Schaut
- 👤 Richard Alan Zimbrick
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 12:16
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/04; F02C7/045; F04; F04D; F04D27/00; F04D27/02; F04D27/0207; F04D27/0215; F04D27/023; F04D29/00; F04D29/40; F04D29/52; F04D29/54; F04D29/541; F04D29/545; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 15
Claim 1
Independent Claim
127 words
A nacelle for a gas turbine engine of the type known as a turbofan having a fan stage including a rotor having a plurality of blades and a set of stators spaced apart and downstream of said rotor, said nacelle having an inner wall which forms an annular fan duct for the passage of air through the engine, said nacelle comprising: means for ducting a portion of said air out of said fan duct, through said nacelle and into the atmosphere, said means having an entrance in said inner wall located upstream of said fan stators but downstream of said rotor a distance greater than one-fourth of the chord of the radially outermost rotor blade tips; and, means for controlling the airflow through said means for ducting.
Claim 2
Dependent Claim
127 words
A nacelle for a gas turbine engine of the type known as a turbofan having a fan stage including a rotor having a plurality of blades and a set of stators spaced apart and downstream of said rotor, said nacelle having an inner wall which forms an annular fan duct for the passage of air through the engine, said nacelle comprising: means for ducting a portion of said air out of said fan duct, through said nacelle and into the atmosphere, said means having an entrance in said inner wall located upstream of said fan stators but downstream of said rotor a distance greater than one-fourth of the chord of the radially outermost rotor blade tips; and, means for controlling the airflow through said means for ducting.
Claim 3
Dependent Claim
32 words
The nacelle of claim 1 wherein said means for controlling comprises: a ring slidably mounted in said nacelle near said entrance; and, means attached to said ring for moving said ring axially.
Claim 4
Dependent Claim
48 words
The nacelle of claim 1 wherein said means for ducting includes a substantially cylindrical section having an inner wall which forms a portion of said fan duct, and an outer wall, and further having a plurality of passageways extending between said inner and outer walls of said section.
Claim 5
Dependent Claim
35 words
The nacelle of claim 3 wherein said means for controlling comprises: a ring rotably mounted in said nacelle, concentrically surrounding said section and having a plurality of mating passageways; and, means for rotating said ring.
Claim 6
Dependent Claim
34 words
The nacelle of claim 3 wherein said means for controlling comprises: a ring slidably mounted in said nacelle and concentrically surrounding said section; and, means attached to said ring for axially sliding said ring.
Claim 7
Dependent Claim
35 words
The nacelle of claim 1 wherein said means for ducting includes a bypass collector located within said nacelle and covering said entrance, and a bypass passageway providing communication between said bypass collector and the atmosphere.
Claim 8
Dependent Claim
29 words
The nacelle of claim 6 wherein said means for controlling comprises: a door attached to the nacelle for sealing said entrance; and means for opening and closing said door.
Claim 9
Dependent Claim
23 words
The nacelle of claim 7 wherein said door is pivotally mounted at its forward edge and opens radially outward from the fan duct.
Claim 10
Dependent Claim
24 words
The nacelle of claim 7 wherein said door is pivotally mounted at its aft edge and opens toward the interior of the fan duct.
Claim 11
Dependent Claim
39 words
The nacelle of claim 1 wherein said means for controlling comprises: an arcuate channel section slidably mounted in said nacelle; and, means attached to said channel section for axially moving the section between an open and a closed position.
Claim 12
Dependent Claim
91 words
The nacelle of claim 1 wherein said means for controlling comprises: a door pivotally mounted to the outer surface of the nacelle, having a closed position in which it covers the downstream end of said ducting means and an open position in which the door is spaced apart from the outer nacelle surface and forms a channel in which ambient air passing over the outer nacelle surface is mixed with said portion of air exhausting from said ducting means; and, means attached to said door for opening and closing said door.
Claim 13
Dependent Claim
18 words
The nacelle of claim 1 wherein said means for ducting comprises a plurality of turning vanes mounted therein.
Claim 14
Dependent Claim
30 words
The nacelle of claim 1 wherein said means for ducting comprises a second entrance in said inner wall located downstream from the aforesaid entrance, but upstream of said fan stators.
Claim 15
Dependent Claim
29 words
The nacelle of claim 13 wherein said means for controlling comprises: a pair of doors for closing said openings; and, pneumatically actuated means for opening and closing said doors.
References Cited (Backward Citations)
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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) | 1981-05-01 | 1981-10-31 | 1982-05-02 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1985-05-01 | 1985-10-31 | 1986-05-02 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1989-05-01 | 1989-10-31 | 1990-05-02 | $7700.00 | Window Closed / Lapsed |