GB1371097A - Engines - Google Patents

Engines

Info

Publication number
GB1371097A
GB1371097A GB4764470A GB4764470A GB1371097A GB 1371097 A GB1371097 A GB 1371097A GB 4764470 A GB4764470 A GB 4764470A GB 4764470 A GB4764470 A GB 4764470A GB 1371097 A GB1371097 A GB 1371097A
Authority
GB
United Kingdom
Prior art keywords
turbine
combustion chamber
combustion
compressor
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
GB4764470A
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.)
Budd C A
Original Assignee
Budd C A
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 Budd C A filed Critical Budd C A
Priority to GB4764470A priority Critical patent/GB1371097A/en
Publication of GB1371097A publication Critical patent/GB1371097A/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
    • F02C5/12—Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Abstract

1371097 Gas turbine engines; jet propulstion units C A BUDD 16 Oct 1971 [7 Oct 1970] 47644/70 Headings FIG and F1J The invention relates to an engine comprising an air compressor from which pressurized air passes to a combustion chamber, gases passing from the chamber to a utilisation device such as a gas turbine, the combustion chamber having non- return air inlet means. In Fig.1, the engine comprises compressor 62, combustion equipment 63 and a turbine 64 connected to drive the compressor through shaft 69. The combustion equipment comprises a flame tube 63 having a non- return inlet valve 77, also fuel injection means 67 and an igniter 68. The combustion chamber communicates by way of a duct 66 with a reservoir 81 from which the gases pass to inlet nozzle 82 of the turbine. A number of concentric baffles are disposed in the reservoir. Slugs of combustion gas and air pass in succession from the combustion chamber. The air compressor and the turbine may be dispensed with, the unit operating as a pulsating jet propulsion unit
GB4764470A 1971-10-06 1971-10-06 Engines Expired GB1371097A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB4764470A GB1371097A (en) 1971-10-06 1971-10-06 Engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4764470A GB1371097A (en) 1971-10-06 1971-10-06 Engines

Publications (1)

Publication Number Publication Date
GB1371097A true GB1371097A (en) 1974-10-23

Family

ID=10445753

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4764470A Expired GB1371097A (en) 1971-10-06 1971-10-06 Engines

Country Status (1)

Country Link
GB (1) GB1371097A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100365256C (en) * 2005-12-26 2008-01-30 王菲 Pulsating flow gas turbine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN100365256C (en) * 2005-12-26 2008-01-30 王菲 Pulsating flow gas turbine

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Legal Events

Date Code Title Description
PS Patent sealed
435 Patent endorsed 'licences of right' on the date specified (sect. 35/1949)
PCNP Patent ceased through non-payment of renewal fee