GB1447990A - Internal combustion engines - Google Patents

Internal combustion engines

Info

Publication number
GB1447990A
GB1447990A GB3134673A GB3134673A GB1447990A GB 1447990 A GB1447990 A GB 1447990A GB 3134673 A GB3134673 A GB 3134673A GB 3134673 A GB3134673 A GB 3134673A GB 1447990 A GB1447990 A GB 1447990A
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
spiral blade
supplied
internal combustion
combustion engines
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
GB3134673A
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.)
FORD RESEARCH DEV Ltd ERIC H
Original Assignee
FORD RESEARCH DEV Ltd ERIC H
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 FORD RESEARCH DEV Ltd ERIC H filed Critical FORD RESEARCH DEV Ltd ERIC H
Priority to GB3134673A priority Critical patent/GB1447990A/en
Publication of GB1447990A publication Critical patent/GB1447990A/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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

1447990 Gas turbine engines; screw compressors and turbines ERIC H FORD RESEARCH & DEVELOPMENT Ltd 2 Oct 1974 [2 July 1973] 31346/73 Headings F1C F1G and F1T An engine comprises a compressor rotor 4 formed with an open coiled spiral blade 14 delivering compressed gas into a combustion chamber 16 feeding an expansion rotor 2 having a similar spiral blade 12. Blades 14, 12 are of respectively decreasing and increasing pitch in the direction of flow. Fuel may be supplied via carburetter 18 or be injected at or adjacent combustion chamber 16. Air for starting may be supplied from a reservoir via port 26. Shaft 6 may drive a vehicle transmission.
GB3134673A 1973-07-02 1973-07-02 Internal combustion engines Expired GB1447990A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3134673A GB1447990A (en) 1973-07-02 1973-07-02 Internal combustion engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3134673A GB1447990A (en) 1973-07-02 1973-07-02 Internal combustion engines

Publications (1)

Publication Number Publication Date
GB1447990A true GB1447990A (en) 1976-09-02

Family

ID=10321759

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3134673A Expired GB1447990A (en) 1973-07-02 1973-07-02 Internal combustion engines

Country Status (1)

Country Link
GB (1) GB1447990A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2770258A1 (en) * 1997-10-23 1999-04-30 Ignacio Sierro Linear motor with compression reduction
GB2355768A (en) * 1999-11-01 2001-05-02 Kofi Abaka Jackson Turbine/compressor rotor with helical blade
GB2513440A (en) * 2013-02-10 2014-10-29 Zun Energy Ltd Combustion engine
EP1798473A3 (en) * 2005-12-16 2017-11-01 General Electric Company Axial flow positive displacement gas generator with combustion extending into an expansion section
WO2019104417A1 (en) * 2017-11-30 2019-06-06 Sung Rayne Gas turbine engines and compression systems therefor
CN114810339A (en) * 2022-05-17 2022-07-29 叶华 Ring cylinder engine with external transmission mechanism
CN116251451A (en) * 2022-12-29 2023-06-13 重庆大学 Gas condensate recovery device and method

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2770258A1 (en) * 1997-10-23 1999-04-30 Ignacio Sierro Linear motor with compression reduction
GB2355768A (en) * 1999-11-01 2001-05-02 Kofi Abaka Jackson Turbine/compressor rotor with helical blade
GB2355768B (en) * 1999-11-01 2004-03-17 Kofi Abaka Jackson Compressor or turbine rotor having spirally curved blades
EP1798473A3 (en) * 2005-12-16 2017-11-01 General Electric Company Axial flow positive displacement gas generator with combustion extending into an expansion section
GB2513440A (en) * 2013-02-10 2014-10-29 Zun Energy Ltd Combustion engine
GB2513440B (en) * 2013-02-10 2015-07-15 Zun Energy Ltd Combustion engine
WO2019104417A1 (en) * 2017-11-30 2019-06-06 Sung Rayne Gas turbine engines and compression systems therefor
US10598181B2 (en) 2017-11-30 2020-03-24 Rayne Sung Gas turbine engines and compression systems therefor
CN114810339A (en) * 2022-05-17 2022-07-29 叶华 Ring cylinder engine with external transmission mechanism
CN116251451A (en) * 2022-12-29 2023-06-13 重庆大学 Gas condensate recovery device and method

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee