GB588082A - Improvements relating to engines - Google Patents

Improvements relating to engines

Info

Publication number
GB588082A
GB588082A GB1083741A GB1083741A GB588082A GB 588082 A GB588082 A GB 588082A GB 1083741 A GB1083741 A GB 1083741A GB 1083741 A GB1083741 A GB 1083741A GB 588082 A GB588082 A GB 588082A
Authority
GB
United Kingdom
Prior art keywords
engines
improvements relating
annular
spherical
pipes
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
GB1083741A
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.)
Power Jets Ltd
Original Assignee
Power Jets Ltd
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 Power Jets Ltd filed Critical Power Jets Ltd
Priority to GB1083741A priority Critical patent/GB588082A/en
Publication of GB588082A publication Critical patent/GB588082A/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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants

Abstract

588,082. Gas turbines. POWER JETS, Ltd., WALKER, D. N., and PULLIN, C. G. Aug. 25, 1941, No. 10837. Drawings to Specification. [Class 110 (iii)] An annular series of axially arranged outlets from a centrifugal compressor is connected to associated combustion chambers by flexible pipes having annular corrugations and supported against extension by tension rods with spherical heads or by rigid pipes with joints made by synthetic rubber gaskets and held in place by joint rings having spherical surfaces.
GB1083741A 1941-08-25 1941-08-25 Improvements relating to engines Expired GB588082A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1083741A GB588082A (en) 1941-08-25 1941-08-25 Improvements relating to engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1083741A GB588082A (en) 1941-08-25 1941-08-25 Improvements relating to engines

Publications (1)

Publication Number Publication Date
GB588082A true GB588082A (en) 1947-05-14

Family

ID=9975233

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1083741A Expired GB588082A (en) 1941-08-25 1941-08-25 Improvements relating to engines

Country Status (1)

Country Link
GB (1) GB588082A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2494821A (en) * 1946-03-25 1950-01-17 Rolls Royce Means for supporting the nozzles of the combustion chambers of internal-combustion turbines
US2605611A (en) * 1948-08-16 1952-08-05 Solar Aircraft Co Thrust balance structure for rotary gas engines
US2670600A (en) * 1947-06-17 1954-03-02 Bristol Aeroplane Co Ltd Air distribution system for flame tubes of gas turbine engines
US2676459A (en) * 1947-06-12 1954-04-27 Bristol Aeroplane Co Ltd Gas turbine engine having a continuous outer stress bearing shell and means allowing access through the shell to the combustion space of the engine
US2722801A (en) * 1949-05-24 1955-11-08 Rolls Royce Exhaust ducting arrangements for gas-turbine engines

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2494821A (en) * 1946-03-25 1950-01-17 Rolls Royce Means for supporting the nozzles of the combustion chambers of internal-combustion turbines
US2676459A (en) * 1947-06-12 1954-04-27 Bristol Aeroplane Co Ltd Gas turbine engine having a continuous outer stress bearing shell and means allowing access through the shell to the combustion space of the engine
US2670600A (en) * 1947-06-17 1954-03-02 Bristol Aeroplane Co Ltd Air distribution system for flame tubes of gas turbine engines
US2605611A (en) * 1948-08-16 1952-08-05 Solar Aircraft Co Thrust balance structure for rotary gas engines
US2722801A (en) * 1949-05-24 1955-11-08 Rolls Royce Exhaust ducting arrangements for gas-turbine engines

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