US4302934A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Lobed mixer/inverter
Assignee: RTX Corp
•
Filing: 1979-11-01
•
Granted: 1981-12-01
•
Expires: 1999-11-01
Abstract
Abstract A fairing added to the upstream end of the lobe of conventional lobed mixers or inverters for a gas turbine engine redirects the boundary layer so as to improve engine performance.
Inventors
- 👤 Thomas A. Wynosky
- 👤 Donald C. Eiler
- 👤 Jerrold R. Blatt
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 13:43
CPC Classifications
F; F02; F02K; F02K1/00; F02K1/38; F02K1/386
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
142 words
A multi-lobed mixer for fan jet engine fabricated from a single generally cylindrically shaped member formed about an axially extending center line and having alternately circumferentially spaced radially inward and radially outward extending lobes on the aft end of said cylindrical member and forming chutes for directing fan and engine flow into mixing relationship, an annular depression formed intermediate the ends of said cylindrical member adjacent the flow entrance of said lobes, fairing means formed on the radially outward extending lobe bridging the depression and spanning the width of the attaching lobe and having its radial most extension portion extending substantially the same distance from said center line as the top portion of said radially outward extending lobe whereby a portion of the flow from the fan is directed substantially straight through over the top surface of said radially outward extending lobes.
Claim 2
Dependent Claim
142 words
A multi-lobed mixer for fan jet engine fabricated from a single generally cylindrically shaped member formed about an axially extending center line and having alternately circumferentially spaced radially inward and radially outward extending lobes on the aft end of said cylindrical member and forming chutes for directing fan and engine flow into mixing relationship, an annular depression formed intermediate the ends of said cylindrical member adjacent the flow entrance of said lobes, fairing means formed on the radially outward extending lobe bridging the depression and spanning the width of the attaching lobe and having its radial most extension portion extending substantially the same distance from said center line as the top portion of said radially outward extending lobe whereby a portion of the flow from the fan is directed substantially straight through over the top surface of said radially outward extending lobes.
Claim 3
Dependent Claim
19 words
A multi-lobed mixer as in claim 1 wherein said fairing means is mechanically fastened to the cylindrically shaped member.
Claim 4
Dependent Claim
147 words
In combination, an exhaust case for a gas turbine fan-jet engine, a lobed mixer having a generally cylindrically shaped hollow member concentrically mounted in said exhaust case and being spaced therefrom for defining an annular passage, said lobed mixer having a plurality of circumferentially spaced alternate radially inward and outward extending lobes on the end of said hollow member, the inward lobe forming a chute for directing the fan air radially inward and the outward lobe forming a chute for directing the jet exhaust from the turbine radially outward for encouraging mixing of the two streams, fairing means extending from a fore end of said hollow end to the radially outward extending lobe and spanning its width dimension and defining with said exhaust case a substantially straight through passage whereby the fan air adjacent the outward extending lobe passes straight over without migrating into the inward chute.
Claim 5
Dependent Claim
147 words
In combination, an exhaust case for a gas turbine fan-jet engine, a lobed mixer having a generally cylindrically shaped hollow member concentrically mounted in said exhaust case and being spaced therefrom for defining an annular passage, said lobed mixer having a plurality of circumferentially spaced alternate radially inward and outward extending lobes on the end of said hollow member, the inward lobe forming a chute for directing the fan air radially inward and the outward lobe forming a chute for directing the jet exhaust from the turbine radially outward for encouraging mixing of the two streams, fairing means extending from a fore end of said hollow end to the radially outward extending lobe and spanning its width dimension and defining with said exhaust case a substantially straight through passage whereby the fan air adjacent the outward extending lobe passes straight over without migrating into the inward chute.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1984-11-30 | 1985-06-01 | 1985-12-01 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-11-30 | 1989-06-01 | 1989-12-01 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-11-30 | 1993-06-01 | 1993-12-01 | $7700.00 | Window Closed / Lapsed |