GB648647A - Improvements in or relating to heat engines utilising jet drives - Google Patents

Improvements in or relating to heat engines utilising jet drives

Info

Publication number
GB648647A
GB648647A GB19675/48A GB1967548A GB648647A GB 648647 A GB648647 A GB 648647A GB 19675/48 A GB19675/48 A GB 19675/48A GB 1967548 A GB1967548 A GB 1967548A GB 648647 A GB648647 A GB 648647A
Authority
GB
United Kingdom
Prior art keywords
drum
relating
jets
july
heat 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
GB19675/48A
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 GB648647A publication Critical patent/GB648647A/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
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • F02C3/16—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant
    • F02C3/165—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant the combustion chambers being formed at least partly in the turbine rotor or in an other rotating part of the plant the combustion chamber contributes to the driving force by creating reactive thrust

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Air Supply (AREA)

Abstract

648,647. Gas turbine plant. VADOLT TRUST. July 22, 1948, No. 19675. Convention date, July 24, 1947. [Class 110(iii)] Combustion cnambers 2 discharge through re-action jets 4 in a rotating drum 1. The drum drives a compressor which delivers air through a conduit 8 to the interior of a stationary drum. The air passes out through nozzles 5 and enters, with a supersonic relative velocity, passages 9 in the rotary drum 1 which lead to the combustion chambers. Fuel, which may be coal dust, is supplied to the burners with a pressure due to the rotation of the drum. The gases leaving the jets 4 are collected in a casing 6 and led to a normal turbine on the same shaft.
GB19675/48A 1947-07-24 1948-07-22 Improvements in or relating to heat engines utilising jet drives Expired GB648647A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
AT267495X 1947-07-24

Publications (1)

Publication Number Publication Date
GB648647A true GB648647A (en) 1951-01-10

Family

ID=3670453

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19675/48A Expired GB648647A (en) 1947-07-24 1948-07-22 Improvements in or relating to heat engines utilising jet drives

Country Status (2)

Country Link
CH (1) CH267495A (en)
GB (1) GB648647A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2240817A (en) * 1990-02-09 1991-08-14 Vni I Kt I Kompressornogo Mash Reaction-jet turbine
US5709076A (en) * 1992-09-14 1998-01-20 Lawlor; Shawn P. Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall
US6298653B1 (en) 1996-12-16 2001-10-09 Ramgen Power Systems, Inc. Ramjet engine for power generation
US6347507B1 (en) * 1992-09-14 2002-02-19 Ramgen Power Systems, Inc. Method and apparatus for power generation using rotating ramjets
US6446425B1 (en) 1998-06-17 2002-09-10 Ramgen Power Systems, Inc. Ramjet engine for power generation
WO2009009026A3 (en) * 2007-07-10 2009-02-26 Ziyad Qamhiyeh Rotary internal combustion engine
US8056529B2 (en) * 2007-07-10 2011-11-15 Qamhiyeh Ziyad A Rotary internal combustion engine for combusting low cetane fuels
WO2015118274A1 (en) * 2014-02-10 2015-08-13 Turbomeca System for the emergency starting of a turbomachine
US12066027B2 (en) 2022-08-11 2024-08-20 Next Gen Compression Llc Variable geometry supersonic compressor

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19546474C1 (en) * 1995-12-13 1997-04-17 Klein Hans Ulrich Dipl Ing Internal combustion engine with rotor housing having cylindrical chamber

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2240817A (en) * 1990-02-09 1991-08-14 Vni I Kt I Kompressornogo Mash Reaction-jet turbine
US6510683B1 (en) 1992-09-14 2003-01-28 Ramgen Power Systems, Inc. Apparatus for power generation with low drag rotor and ramjet assembly
US5709076A (en) * 1992-09-14 1998-01-20 Lawlor; Shawn P. Method and apparatus for power generation using rotating ramjet which compresses inlet air and expands exhaust gas against stationary peripheral wall
US6347507B1 (en) * 1992-09-14 2002-02-19 Ramgen Power Systems, Inc. Method and apparatus for power generation using rotating ramjets
US6298653B1 (en) 1996-12-16 2001-10-09 Ramgen Power Systems, Inc. Ramjet engine for power generation
US6334299B1 (en) 1996-12-16 2002-01-01 Ramgen Power Systems, Inc. Ramjet engine for power generation
US6434924B1 (en) 1996-12-16 2002-08-20 Ramgen Power Systems, Inc. Ramjet engine for power generation
US6446425B1 (en) 1998-06-17 2002-09-10 Ramgen Power Systems, Inc. Ramjet engine for power generation
WO2009009026A3 (en) * 2007-07-10 2009-02-26 Ziyad Qamhiyeh Rotary internal combustion engine
JP2010533259A (en) * 2007-07-10 2010-10-21 ジーヤッド クアムヒイェー Rotary internal combustion engine
US8056529B2 (en) * 2007-07-10 2011-11-15 Qamhiyeh Ziyad A Rotary internal combustion engine for combusting low cetane fuels
WO2015118274A1 (en) * 2014-02-10 2015-08-13 Turbomeca System for the emergency starting of a turbomachine
FR3017417A1 (en) * 2014-02-10 2015-08-14 Turbomeca PYROTECHNIC DEVICE FOR DRIVING A ROTATING MACHINE
US12066027B2 (en) 2022-08-11 2024-08-20 Next Gen Compression Llc Variable geometry supersonic compressor

Also Published As

Publication number Publication date
CH267495A (en) 1950-03-31

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