GB576042A - Improvements in or relating to heat engine power units - Google Patents

Improvements in or relating to heat engine power units

Info

Publication number
GB576042A
GB576042A GB2323/44A GB232344A GB576042A GB 576042 A GB576042 A GB 576042A GB 2323/44 A GB2323/44 A GB 2323/44A GB 232344 A GB232344 A GB 232344A GB 576042 A GB576042 A GB 576042A
Authority
GB
United Kingdom
Prior art keywords
turbine
pressure
supplied
air
compressor
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
GB2323/44A
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 GB2323/44A priority Critical patent/GB576042A/en
Publication of GB576042A publication Critical patent/GB576042A/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
    • F02C5/00—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • 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
    • F02C7/125—Cooling of plants by partial arc admission of the working fluid or by intermittent admission of working and cooling fluid
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Abstract

576,042. Generating combustion products under pressure. HALLOWELL, E. Feb. 8, 1944, No. 2323. [Class 51 (i)] [Also in Group XXVI] Gases generated in an oscillating column gas generator such as described in Specification 574,554, or other suitable I.C. engine, are led into a diverging duct 47 of about the same acoustic period as the duct 41 and thence to an impulse turbine 40. Compressed-air from a compressor 18 driven by the turbine 40 is heated in an economizer 12 and passed to a chamber 21 surrounding the ducts 41, 47. Here it is further heated and passes out to the rear of the turbine 40. The heated air passes through the turbine in the reverse direction during the low-pressure part of the acoustic cycle and mixes with the combustion products. The exhaust of the turbine 40 passes to a pressure-equalising chamber 10 and thence to a turbine 11 which exhausts to the economizer 12. The turbine drives a low-pressure compressor 14, in series with the compressor 18, and an electric generator 15. A cooler 17 is placed between the compressors 14, 18. The gas generator is supplied with compressed air through pipe 52. In starting, highly explosive fuel is supplied by a carburettor 25. When the air pressure rises, it acts upon a.piston 33 to open a valve 31 through which normal fuel is supplied. The valve 22 is closed during starting. Specification 574,552, [Group XXVI], is referred to in the Provisional Specification.
GB2323/44A 1944-02-08 1944-02-08 Improvements in or relating to heat engine power units Expired GB576042A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2323/44A GB576042A (en) 1944-02-08 1944-02-08 Improvements in or relating to heat engine power units

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2323/44A GB576042A (en) 1944-02-08 1944-02-08 Improvements in or relating to heat engine power units

Publications (1)

Publication Number Publication Date
GB576042A true GB576042A (en) 1946-03-15

Family

ID=9737525

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2323/44A Expired GB576042A (en) 1944-02-08 1944-02-08 Improvements in or relating to heat engine power units

Country Status (1)

Country Link
GB (1) GB576042A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1007118B (en) * 1951-03-16 1957-04-25 Snecma Gas turbine plant
GB2164139A (en) * 1984-08-29 1986-03-12 Toshiba Kk Pulse combustor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1007118B (en) * 1951-03-16 1957-04-25 Snecma Gas turbine plant
GB2164139A (en) * 1984-08-29 1986-03-12 Toshiba Kk Pulse combustor
US4619601A (en) * 1984-08-29 1986-10-28 Kabushiki Kaisha Toshiba Pulse combustor

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