US4308718A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Bleedoff of gas from diffusers in fluid flow machines
Assignee: Kongsberg Gruppen ASA
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Filing: 1978-12-27
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Granted: 1982-01-05
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Expires: 1998-12-27
Abstract
Abstract In a fluid flow machine comprising a compressor including a compressor diffuser and a turbine including an exhaust gas diffuser compressed air from boundary layers or vortex flows in the compressor diffuser is bled off and used as a driving medium for removing exhaust gas from boundary layers or vortex flows in the exhaust gas diffuser. Since the pressure of the exhaust gas to be removed from the exhaust gas diffuser is below the ambient pressure a suction has to be established to remove the desired gas from the boundary layers or vortex flows. This suction is established by an ejector or a pump which is driven by the energy of the compressed air bled from the compressor diffuser.
Inventors
- 👤 Jan Mowill
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 03:48
CPC Classifications
F; F01; F01D; F01D25/00; F01D25/30; F02; F02B; F02B39/00; F02C; F02C3/00; F02C3/32; F04; F04D; F04D27/00; F04D27/02; F04D27/0207; F04D27/0215; F04D29/00; F04D29/08; F04D29/16; F04D29/161; F04D29/162; F05; F05D; F05D2260/00; F05D2260/60; F05D2260/601; Y; Y10; Y10S; Y10S415/00; Y10S415/914
Claims Analysis
Total Claims: 2
Claim 1
Independent Claim
170 words
In a method of stabilizing the flow of a working medium in a gas turbine engine, having a compressor with a compressor diffuser and a turbine with an exhaust gas diffuser and wherein the turbine drives the compressor by a common shaft, by bleeding off a part of the working medium from a boundary layer, or vortex flow, in the engine, the improvement whereby the total efficiency of the machine is improved comprising bleeding off a part of the working medium from a first boundary layer, or vortex flow, from said compressor diffuser, bleeding off part of the working medium from a second boundary layer, or vortex flow, from said exhaust gas diffuser at lower pressure than said first boundary layer, coupling said bleedoffs by feeding said working fluid from said compressor diffuser to an air turbine to drive said air turbine thereby, driving an auxiliary pump or compressor by said air turbine, and connecting the suction line of said auxiliary pump or air turbine to said exhaust gas diffuser.
Claim 2
Dependent Claim
170 words
In a method of stabilizing the flow of a working medium in a gas turbine engine, having a compressor with a compressor diffuser and a turbine with an exhaust gas diffuser and wherein the turbine drives the compressor by a common shaft, by bleeding off a part of the working medium from a boundary layer, or vortex flow, in the engine, the improvement whereby the total efficiency of the machine is improved comprising bleeding off a part of the working medium from a first boundary layer, or vortex flow, from said compressor diffuser, bleeding off part of the working medium from a second boundary layer, or vortex flow, from said exhaust gas diffuser at lower pressure than said first boundary layer, coupling said bleedoffs by feeding said working fluid from said compressor diffuser to an air turbine to drive said air turbine thereby, driving an auxiliary pump or compressor by said air turbine, and connecting the suction line of said auxiliary pump or air turbine to said exhaust gas diffuser.
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) | 1985-01-04 | 1985-07-06 | 1986-01-05 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-01-04 | 1989-07-06 | 1990-01-05 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-01-04 | 1993-07-06 | 1994-01-05 | $7700.00 | Window Closed / Lapsed |