Patent US3116578A successfully refreshed from Google Patents.
Patent US4217756A successfully refreshed from Google Patents.
US4217756A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Vortex mixers for reducing the noise emitted by jet engines
Assignee: Boeing Commercial Airplane Co
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Filing: 1977-12-27
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Granted: 1980-08-19
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Expires: 1997-12-27
Abstract
Abstract Apparatus for internally mixing fan exhaust with primary exhaust forward of the nozzle exit plane of a turbofan engine having an outer engine cowling, a splitter wall structure and a tail plug disposed in mid engine upstream of the nozzle exit plane is provided by a plurality of struts disposed radially between the engine tail plug and the outer engine cowling upstream of the nozzle exit plane and a plurality of vortex generating means disposed on the struts for generating vorticies across the entire engine exhaust area.
Inventors
- 👤 Jerome R. Laskody
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 08:09
CPC Classifications
F; F02; F02K; F02K1/00; F02K1/38; F02K1/386; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
172 words
In a turbofan engine having an annular fan fluid flow exhaust passageway located between an outer engine cowling and a splitter wall structure, said splitter wall structure terminating at a distance upstream of the nozzle exit plane of said engine, an annular primary fluid flow exhaust passageway located inside of said splitter wall structure, and a tail plug disposed in mid engine upstream of the nozzle exit plane and extending downstream past the end of said splitter wall structure, apparatus for internal mixing of fan exhaust flow with primary exhaust flow upstream of the nozzle exit plane of said engine and downstream of the end of said splitter wall structure, comprising: a plurality of struts disposed radially between the engine tail plug and the outer engine cowling upstream of the nozzle exit plane; and a plurality of vortex generating means disposed at radially spaced locations on each of said struts for generating vortices across the entire engine exhaust area to promote mixing of said fan and primary exhaust flows to reduce noise.
Claim 2
Dependent Claim
172 words
In a turbofan engine having an annular fan fluid flow exhaust passageway located between an outer engine cowling and a splitter wall structure, said splitter wall structure terminating at a distance upstream of the nozzle exit plane of said engine, an annular primary fluid flow exhaust passageway located inside of said splitter wall structure, and a tail plug disposed in mid engine upstream of the nozzle exit plane and extending downstream past the end of said splitter wall structure, apparatus for internal mixing of fan exhaust flow with primary exhaust flow upstream of the nozzle exit plane of said engine and downstream of the end of said splitter wall structure, comprising: a plurality of struts disposed radially between the engine tail plug and the outer engine cowling upstream of the nozzle exit plane; and a plurality of vortex generating means disposed at radially spaced locations on each of said struts for generating vortices across the entire engine exhaust area to promote mixing of said fan and primary exhaust flows to reduce noise.
Claim 3
Dependent Claim
31 words
Apparatus for internal mixing of fan exhaust with primary exhaust in a turbofan engine as defined in claim 1, wherein twelve struts are radially disposed symmetrically about the engine tail plug.
Claim 4
Dependent Claim
52 words
Apparatus for internal mixing of fan exhaust with primary exhaust in a turbofan engine as defined in claim 2, wherein said vortex generating means are disposed on each of two sides of said struts for generating a pair of counter-rotating vortices at each said radially spaced location along each of said struts.
Claim 5
Dependent Claim
31 words
Apparatus for internal mixing of fan exhaust with primary exhaust in a turbofan engine as defined in claim 1, wherein eight struts are radially disposed symmetrically about the engine tail plug.
Claim 6
Dependent Claim
64 words
Apparatus for internal mixing of fan exhaust with primary exhaust in a turbofan engine as defined in claim 4, wherein said vortex generating means are disposed on each of two sides of said struts for generating a pair of counter-rotating vortices at each said radially spaced location along each of said struts, one vortex of each pair disposed on each side of said strut.
Claim 7
Dependent Claim
54 words
Apparatus for internal mixing of fan exhaust with primary exhaust in a turbofan engine as defined in claim 2 or 4, wherein said vortex generating means are disposed on each of two sides of said struts for generating a pair of co-rotating vortices at each said radially spaced location along each of said struts.
Claim 8
Dependent Claim
38 words
Apparatus for internal mixing of fan exhaust with primary exhaust in a turbofan engine as claimed in claim 1, wherein said vortex generating means are positioned at a location spaced downstream from the end of said splitter structure.
Claim 9
Dependent Claim
42 words
Apparatus for internal mixing of fan exhaust with primary exhaust in a turbofan engine as claimed in claim 7, wherein said engine cowling has a conical shape of decreasing diameter for a distance downstream of the end of said splitter wall structure.
References Cited (Backward Citations)
US2443250A
Cited
US2880574A
Cited
US3100627A
Cited
US2935847A
Cited
US3655009A
Cited
US3647020A
Cited
US3776363A
Cited
US3737005A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1983-08-19 | 1984-02-18 | 1984-08-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-08-19 | 1988-02-18 | 1988-08-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-08-19 | 1992-02-18 | 1992-08-19 | $7700.00 | Window Closed / Lapsed |