Patent US3011349A successfully refreshed from Google Patents.
Patent US4275564A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4275564A Expired / Lapsed US ⏱️ 0.0 years remaining

Combustion chamber for gas turbine engines

Assignee: MOTOREN-UND TURBINEN-UNION MUENCEN GmbH
•
Filing: 1979-04-10
•
Granted: 1981-06-30
•
Expires: 1999-04-10
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract Combustion chambers for gas turbine engines and, more particularly, an annular combustion chamber. The combustion chamber comprises a flame tube having a back wall through which several vaporizers project into the flame tube or combustion zone. Each vaporizer has a pipe section extending within the flame tube, fuel supply and also supply ports in communication with the pipe section, and at least one outlet port for supplying a vaporous fuel-air mixture from the pipe section to the flame tube. Outlet ports of adjacent vaporizers are arranged spaced-apart from and facing one another, whereby a zone of maximum turbulence is formed between the outlet ports.

Inventors

  • 👤 Guenter Kappler
  • 👤 Adolf Fehler

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 21:52
CPC Classifications
F; F23; F23R; F23R3/00; F23R3/28; F23R3/30; F23R3/32; F23R3/02; F23R3/16; F23R3/18; F23R3/20

Claims Analysis

Total Claims: 12
Claim 1
Independent Claim 128 words
A gas turbine engine, comprising: a combustion chamber including a flame tube having a back wall; a plurality of vaporizers projecting through said back wall and into said flame tube, each said vaporizer having at least one pipe section extending within said flame tube, fuel supply and air supply ports in communication with said pipe section, and at least one outlet port for supplying a vaporous fuel-air mixture from said pipe section to said flame tube, wherein first and second said outlet ports of respective, adjacent first and second said vaporizers are arranged spaced-apart from and directly facing one another, said first and second outlet ports having respective center axes which are coaligned, whereby a zone of maximum turbulence is formed between said first and second outlet ports.
Claim 2
Dependent Claim 128 words
A gas turbine engine, comprising: a combustion chamber including a flame tube having a back wall; a plurality of vaporizers projecting through said back wall and into said flame tube, each said vaporizer having at least one pipe section extending within said flame tube, fuel supply and air supply ports in communication with said pipe section, and at least one outlet port for supplying a vaporous fuel-air mixture from said pipe section to said flame tube, wherein first and second said outlet ports of respective, adjacent first and second said vaporizers are arranged spaced-apart from and directly facing one another, said first and second outlet ports having respective center axes which are coaligned, whereby a zone of maximum turbulence is formed between said first and second outlet ports.
Claim 3
Dependent Claim 37 words
The apparatus of claim 1, wherein a flame occurs between each of said first and second outlet ports and said zone of maximum turbulence, fuel in said vaporous fuel-air mixture being conditioned by heat from said flame.
Claim 4
Dependent Claim 38 words
The apparatus of claim 1, wherein each said outlet port defines an opening having a center, all said outlet port opening centers lying in a common plane intersecting at right angles a longitudinal centerline of said combustion chamber.
Claim 5
Dependent Claim 18 words
The apparatus of claim 1, further comprising a cooling air shroud external to each said vaporizer pipe section.
Claim 6
Dependent Claim 32 words
The apparatus of claim 1, wherein each said vaporizer comprises a separate fuel injection nozzle extending into said pipe section, said fuel supply port comprising an opening in said fuel injection nozzle.
Claim 7
Dependent Claim 55 words
The apparatus of claim 5, wherein each said vaporizer includes two said outlet ports, and said fuel injection nozzle terminates at said nozzle opening upstream of said outlet ports, further comprising central flow dividing means located within said vaporizer downstream of said nozzle opening for dividing said vaporous fuel-air mixture between said two outlet ports.
Claim 8
Dependent Claim 15 words
The apparatus of claim 6, wherein said two outlet ports face in approximately mutually-opposing directions.
Claim 9
Dependent Claim 36 words
The apparatus of claim 7, wherein said vaporizer includes a cross-tube section approximately perpendicular to and in communication with said pipe section, and said two outlet ports comprise openings in respective ends of said cross-tube section.
Claim 10
Dependent Claim 25 words
The apparatus of claim 8, wherein said central flow dividing means comprises an interiorly-extending bulge in said cross-tube, said bulge located adjacent said nozzle opening.
Claim 11
Independent Claim 64 words
The apparatus of one of claims 1 to 5, wherein said flame tube has a reaction zone and a plurality of opposingly-located air supply holes in said flame tube downstream of said reaction zone, whereby air may be supplied through said holes to radially shield said reaction zone downstream of reaction eddies within said zone and to supplement air supplied to said reaction zone.
Claim 12
Independent Claim 79 words
The apparatus of one of claims 1 to 9, wherein said flame tube comprises an annulus defined by inner and outer flame tube walls, said flame tube having a reaction zone and a plurality of opposingly-located air-supply holes in said inner and outer walls downstream of said reaction zone, whereby air may be supplied through said holes to radially shield said reaction zone downstream of reaction eddies within said zone and to supplement air supplied to said reaction zone.

References Cited (Backward Citations)

US2628475A Cited
US2635426A Cited
US2548087A Cited
US2612023A Cited
US2693676A Cited
US2782597A Cited
DE1079895B Cited
US2959006A Cited
US3961475A Cited
US3968644A Cited
US4073137A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1984-06-29 1984-12-29 1985-06-30 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1988-06-29 1988-12-29 1989-06-30 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1992-06-29 1992-12-29 1993-06-30 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag