US4183539A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Seal heat shield
Assignee: Rolls Royce Corp
•
Filing: 1978-11-13
•
Granted: 1980-01-15
•
Expires: 1998-11-13
Abstract
Abstract A regenerator seal structure for a rotary regenerator of a gas turbine engine includes a rim bypass seal located on the hot surface of the matrix of the rotating regenerator including a semi-circular platform with a leaf spring on one surface thereof that is engageable with an engine block support platform to seal between the engine block and one surface of the platform with a free end thereof connected to an inboard edge of the platform and being secured thereto by a hinge member and wherein the platform includes a face seal element with its inboard edge located on the outer diameter of the platform at a point isolated from infrared radiation emissions from a combustor located within the engine housing; the platform including a substantial, radially extending semi-circular flat-plate heat exchanger segment thereon that is exposed to hot gas on one side and to cool gas on the opposite side and inboard of low heat conductivity attachment faces on the seal element to reduce conduction of heat from the inboard edge of the platform to the wear surface of the face seal element.
Inventors
- 👤 James M. French
- 👤 Samuel R. Thrasher
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 08:57
CPC Classifications
F; F28; F28D; F28D19/00; F28D19/04; F28D19/047
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
209 words
In a rotary regenerator seal assembly with a hot side inlet and outlet sealed by a rim bypass seal and for use in a gas turbine with a rotary regenerator disc and combustor the improvement comprising: an arcuate platform with an inboard edge, a leaf spring seal having one end thereon fixed to said inboard edge of the platform, means including said platform and said leaf spring seal defining therebetween a low temperature air plenum separated by said leaf spring from high temperature gas at the regenerator hot side outlet, a wear face seal element supported on the outer diameter of said platform and including a wear surface thereon held by said leaf spring seal in spring biased sealing relation with the hot side of the disc, said arcuate platform including an extension offset inboard of said seal element to define a flat plate heat exchange segment for cooling said platform thereby to reduce conductive heat transfer through the platform from the inboard end thereof to the wear face seal element, said platform extension having an axial extent that shields the wear face seal element from infrared radiation produced at the combustor thereby to prevent excessive temperature build-up in the wear face seal element during gas turbine engine operations.
Claim 2
Dependent Claim
209 words
In a rotary regenerator seal assembly with a hot side inlet and outlet sealed by a rim bypass seal and for use in a gas turbine with a rotary regenerator disc and combustor the improvement comprising: an arcuate platform with an inboard edge, a leaf spring seal having one end thereon fixed to said inboard edge of the platform, means including said platform and said leaf spring seal defining therebetween a low temperature air plenum separated by said leaf spring from high temperature gas at the regenerator hot side outlet, a wear face seal element supported on the outer diameter of said platform and including a wear surface thereon held by said leaf spring seal in spring biased sealing relation with the hot side of the disc, said arcuate platform including an extension offset inboard of said seal element to define a flat plate heat exchange segment for cooling said platform thereby to reduce conductive heat transfer through the platform from the inboard end thereof to the wear face seal element, said platform extension having an axial extent that shields the wear face seal element from infrared radiation produced at the combustor thereby to prevent excessive temperature build-up in the wear face seal element during gas turbine engine operations.
Claim 3
Dependent Claim
256 words
In a rotary regenerator seal assembly with a hot side inlet and outlet sealed by a rim bypass seal and for use in a gas turbine with a rotary regenerator disc and combustor the improvement comprising: an arcuate platform with an inboard edge, a leaf spring seal having one end thereon fixed to said inboard edge of the platform, means including said platform and said leaf spring seal defining therebetween a low temperature air plenum separated by said leaf spring from high temperature gas at the regenerator hot side outlet, a wear face seal element supported on the outer diameter of said platform and including a wear surface thereon held by said leaf spring seal in spring biased sealing relation with the hot side of the disc, said arcuate platform including an extension offset inboard of said seal element to define a flat plate heat exchange segment for cooling said platform thereby to reduce conductive heat transfer through the platform from the inboard end thereof to the wear face seal element, said platform extension having an axial extent that shields the wear face seal element from infrared radiation produced at the combustor thereby to prevent excessive temperature buildup in the wear face seal element during gas turbine engine operations, said wear face seal element being located on the outer one-half of the diameter of said arcuate platform and having side edges connected thereto and to said platform through a limited extent to maintain a clean surface on said extension for transfer of heat from said platform.
Claim 4
Dependent Claim
256 words
In a rotary regenerator seal assembly with a hot side inlet and outlet sealed by a rim bypass seal and for use in a gas turbine with a rotary regenerator disc and combustor the improvement comprising: an arcuate platform with an inboard edge, a leaf spring seal having one end thereon fixed to said inboard edge of the platform, means including said platform and said leaf spring seal defining therebetween a low temperature air plenum separated by said leaf spring from high temperature gas at the regenerator hot side outlet, a wear face seal element supported on the outer diameter of said platform and including a wear surface thereon held by said leaf spring seal in spring biased sealing relation with the hot side of the disc, said arcuate platform including an extension offset inboard of said seal element to define a flat plate heat exchange segment for cooling said platform thereby to reduce conductive heat transfer through the platform from the inboard end thereof to the wear face seal element, said platform extension having an axial extent that shields the wear face seal element from infrared radiation produced at the combustor thereby to prevent excessive temperature buildup in the wear face seal element during gas turbine engine operations, said wear face seal element being located on the outer one-half of the diameter of said arcuate platform and having side edges connected thereto and to said platform through a limited extent to maintain a clean surface on said extension for transfer of heat from said platform.
References Cited (Backward Citations)
US3743008A
Cited
US3856077A
Cited
US3913926A
Cited
US3954135A
Cited
US4056141A
Cited
US4071076A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1983-01-14 | 1983-07-16 | 1984-01-15 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-01-14 | 1987-07-16 | 1988-01-15 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-01-14 | 1991-07-16 | 1992-01-15 | $7700.00 | Window Closed / Lapsed |