Patent US4197700A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4197700A Expired / Lapsed US ⏱️ 0.0 years remaining

Gas turbine power system with fuel injection and combustion catalyst

Assignee: Individual
•
Filing: 1976-10-13
•
Granted: 1980-04-15
•
Expires: 1996-10-13
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract An expansion turbine is used to develop power, wherein combustion of fuel is carried out within the turbine. Increments of fuel are added to two or more points in the presence of a catalyst whereby temperature of the gas or equipment is controlled at substantially isothermal conditions.

Inventors

  • 👤 Charles E. Jahnig

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-08 04:38
CPC Classifications
F; F02; F02C; F02C6/00; F02C6/003

Claims Analysis

Total Claims: 17
Claim 1
Independent Claim 32 words
In a method of producing power in a gas turbine, the improvement which comprises injecting and combusting a fuel with air in the presence of a combustion catalyst in said gas turbine.
Claim 2
Dependent Claim 32 words
In a method of producing power in a gas turbine, the improvement which comprises injecting and combusting a fuel with air in the presence of a combustion catalyst in said gas turbine.
Claim 3
Dependent Claim 43 words
In a system for producing power including a gas turbine, the improvement which comprises providing combustion means for injecting and firing a fuel into said turbine and means for providing a catalyst in said gas turbine to improve the combustion of said fuel.
Claim 4
Dependent Claim 43 words
In a system for producing power including a gas turbine, the improvement which comprises providing combustion means for injecting and firing a fuel into said turbine and means for providing a catalyst in said gas turbine to improve the combustion of said fuel.
Claim 5
Dependent Claim 44 words
In a method of producing power in a gas turbine, the improvement which comprises injecting and combusting a fuel with air in the presence of a combustion catalyst in said gas turbine to thereby maintain the expansion of said gas at substantially isothermal conditions.
Claim 6
Dependent Claim 44 words
In a method of producing power in a gas turbine, the improvement which comprises injecting and combusting a fuel with air in the presence of a combustion catalyst in said gas turbine to thereby maintain the expansion of said gas at substantially isothermal conditions.
Claim 7
Dependent Claim 26 words
A method according to claim 3 wherein said combustion is carried out by injecting said fuel in increments at two or more points in said turbine.
Claim 8
Dependent Claim 36 words
A method according to claim 3 wherein the fuel injected into said turbine is a liquid fuel and contains at least about 2% water to thereby aid in the atomization of said fuel in said turbine.
Claim 9
Dependent Claim 24 words
A method according to claim 3 wherein the temperature is greater than about 1000° F. and the pressure is greater than about 10 atmospheres.
Claim 10
Dependent Claim 18 words
A method according to claim 3 wherein said air is compressed prior to feeding it to said turbine.
Claim 11
Dependent Claim 22 words
A method according to claim 7 wherein said compressed air is indirectly heat exchanged with the exhaust gas from said gas turbine.
Claim 12
Dependent Claim 55 words
In a system for producing power including a gas turbine, the improvement which comprises providing combustion means for injecting and firing a fuel into said turbine to thereby maintain the expansion of the gas at substantially isothermal conditions and means for providing a catalyst in said gas turbine to improve the combustion of said fuel.
Claim 13
Dependent Claim 55 words
In a system for producing power including a gas turbine, the improvement which comprises providing combustion means for injecting and firing a fuel into said turbine to thereby maintain the expansion of the gas at substantially isothermal conditions and means for providing a catalyst in said gas turbine to improve the combustion of said fuel.
Claim 14
Dependent Claim 25 words
A power system according to claim 9 wherein said combustion means includes fuel injection means for injecting fuel in increments at two or more points.
Claim 15
Dependent Claim 32 words
A power system according to claim 9 including a combustion means for injecting and firing fuel in said air to thereby heat said air prior to passing it into said gas turbine.
Claim 16
Dependent Claim 22 words
A power system according to claim 9 including a compression means for compressing air to be fed to the said gas turbine.
Claim 17
Dependent Claim 25 words
A power system according to claim 12 including indirect heat exchange means for heating said compressed air with the exhaust gas from said gas turbine.

References Cited (Backward Citations)

US2243467A Cited
US2305785A Cited
US2407166A Cited
CH288547A Cited
US2656677A Cited
US3928961A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1983-04-15 1983-10-15 1984-04-15 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1987-04-15 1987-10-15 1988-04-15 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1991-04-15 1991-10-15 1992-04-15 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag