GB1479408A - Gas turbine engine - Google Patents

Gas turbine engine

Info

Publication number
GB1479408A
GB1479408A GB10567/75A GB1056775A GB1479408A GB 1479408 A GB1479408 A GB 1479408A GB 10567/75 A GB10567/75 A GB 10567/75A GB 1056775 A GB1056775 A GB 1056775A GB 1479408 A GB1479408 A GB 1479408A
Authority
GB
United Kingdom
Prior art keywords
rotor
compressor
gas turbine
feb
turbine engine
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
GB10567/75A
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
Publication of GB1479408A publication Critical patent/GB1479408A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

1479408 Gas turbine engines H LE MEUR 14 Feb 1975 [25 Feb 1974] 10567/75 Heading F1G A gas turbine engine of the intermittent combustion type comprises a rotor 4 having blades 5 and rotating in a stator casing 8 having one or more combustion chambers 3 with cam-operated inlet and outlet valves 12, the inlet being supplied with compressed air from an axial or radial flow compressor 1 and the exhaust gas from the combustion chambers 3 being further utilized to drive a bladed rotor 17 fast with the shaft 7 common with rotor 4 and compressor 1. A fuel injector (14), Fig. 2, (not shown), and spark-plug (15) are also provided for each combustion chamber. Opposite hand labyrinth seals 6 are provided on rotor 4, and are fed compressor air via ducts 16. An accelerator butterfly valve 11 controls a bleed duct in the compressor delivery duct 2.
GB10567/75A 1974-02-25 1975-02-14 Gas turbine engine Expired GB1479408A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7407173A FR2210718B2 (en) 1974-02-25 1974-02-25

Publications (1)

Publication Number Publication Date
GB1479408A true GB1479408A (en) 1977-07-13

Family

ID=9135728

Family Applications (1)

Application Number Title Priority Date Filing Date
GB10567/75A Expired GB1479408A (en) 1974-02-25 1975-02-14 Gas turbine engine

Country Status (3)

Country Link
FR (1) FR2210718B2 (en)
GB (1) GB1479408A (en)
OA (1) OA04964A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2305471A (en) * 1995-09-23 1997-04-09 James Linton Intermittant-combustion turbine engine
GB2325706A (en) * 1997-05-28 1998-12-02 Thomas Anthony Hollings Intermittant combustion jet engine
US20120285416A1 (en) * 2003-03-21 2012-11-15 Jung-Kuang Chou Rotary engine

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2455677A1 (en) * 1979-05-03 1980-11-28 Meur Henri Le EXPLOSION TURBINE AND GAS DISTRIBUTION SYSTEMS BY ROTATING DISCS OR SLIDING DRAWERS

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2305471A (en) * 1995-09-23 1997-04-09 James Linton Intermittant-combustion turbine engine
GB2325706A (en) * 1997-05-28 1998-12-02 Thomas Anthony Hollings Intermittant combustion jet engine
US20120285416A1 (en) * 2003-03-21 2012-11-15 Jung-Kuang Chou Rotary engine

Also Published As

Publication number Publication date
OA04964A (en) 1980-10-31
FR2210718B2 (en) 1978-04-14
FR2210718A2 (en) 1974-07-12

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Legal Events

Date Code Title Description
CSNS Application of which complete specification have been accepted and published, but patent is not sealed