CH638016A5 - Turbo-jet engine with rotary combustion chambers - Google Patents

Turbo-jet engine with rotary combustion chambers Download PDF

Info

Publication number
CH638016A5
CH638016A5 CH874978A CH874978A CH638016A5 CH 638016 A5 CH638016 A5 CH 638016A5 CH 874978 A CH874978 A CH 874978A CH 874978 A CH874978 A CH 874978A CH 638016 A5 CH638016 A5 CH 638016A5
Authority
CH
Switzerland
Prior art keywords
rotor
combustion chambers
fins
turbo
jet engine
Prior art date
Application number
CH874978A
Other languages
English (en)
French (fr)
Inventor
Charles Provost
Original Assignee
Charles Provost
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 Charles Provost filed Critical Charles Provost
Publication of CH638016A5 publication Critical patent/CH638016A5/fr

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)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Supercharger (AREA)
CH874978A 1978-01-11 1978-08-17 Turbo-jet engine with rotary combustion chambers CH638016A5 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7801143A FR2414627A1 (fr) 1978-01-11 1978-01-11 Turbomoteur a reaction a chambres de combustion rotatives

Publications (1)

Publication Number Publication Date
CH638016A5 true CH638016A5 (en) 1983-08-31

Family

ID=9203512

Family Applications (1)

Application Number Title Priority Date Filing Date
CH874978A CH638016A5 (en) 1978-01-11 1978-08-17 Turbo-jet engine with rotary combustion chambers

Country Status (2)

Country Link
CH (1) CH638016A5 (ja)
FR (1) FR2414627A1 (ja)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0961872B1 (en) * 1997-10-22 2005-07-27 James T. Ray Micro-combustion chamber heat engine

Also Published As

Publication number Publication date
FR2414627B3 (ja) 1981-11-13
FR2414627A1 (fr) 1979-08-10

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Legal Events

Date Code Title Description
PL Patent ceased