GB152872A - Explosion gas turbines - Google Patents

Explosion gas turbines

Info

Publication number
GB152872A
GB152872A GB2685719A GB2685719A GB152872A GB 152872 A GB152872 A GB 152872A GB 2685719 A GB2685719 A GB 2685719A GB 2685719 A GB2685719 A GB 2685719A GB 152872 A GB152872 A GB 152872A
Authority
GB
United Kingdom
Prior art keywords
turbine
water
regenerator
pipe
air
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
GB2685719A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to GB2685719A priority Critical patent/GB152872A/en
Publication of GB152872A publication Critical patent/GB152872A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium

Abstract

152,872. Davey, A. N. Nov. 1, 1919. Motor power plant; working-fluid supply; cooling parts.-In an internal-combustion turbine, the combustion chamber a, the nozzle j, and the turbine casing b are water-jacketed and the water therefrom is led to a regenerator c to which the exhaust gases pass by the pipe q leaving by the pipe r. Pipes l, n and p, o connect the water jackets together and to the regenerator. Steam raised in these sources may be used to drive a turbine or reciprocating engine actuating the compression pumps for the gas and air, or on the turbine blades, or otherwise. The valves e and d controlling the air and gas inlet ports g and the outlet port h respectively are actuated in the embodiment described by a motor i. The sparking-plug is indicated at k. The exit port h to the expanding nozzle j is shaped as shown in Fig. 2.
GB2685719A 1919-11-01 1919-11-01 Explosion gas turbines Expired GB152872A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2685719A GB152872A (en) 1919-11-01 1919-11-01 Explosion gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2685719A GB152872A (en) 1919-11-01 1919-11-01 Explosion gas turbines

Publications (1)

Publication Number Publication Date
GB152872A true GB152872A (en) 1920-10-28

Family

ID=10250333

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2685719A Expired GB152872A (en) 1919-11-01 1919-11-01 Explosion gas turbines

Country Status (1)

Country Link
GB (1) GB152872A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2563022A (en) * 1944-02-12 1951-08-07 Daniel And Florence Guggenheim Fuel feeding mechanism for detonating combustion apparatus
US2578596A (en) * 1946-09-11 1951-12-11 Russell W Rieck Compressor gas turbine combustion chamber with rotating and reciprocating valve therein

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2563022A (en) * 1944-02-12 1951-08-07 Daniel And Florence Guggenheim Fuel feeding mechanism for detonating combustion apparatus
US2578596A (en) * 1946-09-11 1951-12-11 Russell W Rieck Compressor gas turbine combustion chamber with rotating and reciprocating valve therein

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