FR2414627A1 - REACTION TURBOMOTOR WITH ROTARY COMBUSTION CHAMBERS - Google Patents

REACTION TURBOMOTOR WITH ROTARY COMBUSTION CHAMBERS

Info

Publication number
FR2414627A1
FR2414627A1 FR7801143A FR7801143A FR2414627A1 FR 2414627 A1 FR2414627 A1 FR 2414627A1 FR 7801143 A FR7801143 A FR 7801143A FR 7801143 A FR7801143 A FR 7801143A FR 2414627 A1 FR2414627 A1 FR 2414627A1
Authority
FR
France
Prior art keywords
combustion
combustion chambers
turbomotor
reaction
rotary combustion
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.)
Granted
Application number
FR7801143A
Other languages
French (fr)
Other versions
FR2414627B3 (en
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
Priority to FR7801143A priority Critical patent/FR2414627A1/en
Priority to CH874978A priority patent/CH638016A5/en
Publication of FR2414627A1 publication Critical patent/FR2414627A1/en
Application granted granted Critical
Publication of FR2414627B3 publication Critical patent/FR2414627B3/fr
Granted 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)
  • Supercharger (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

The turbine engine comprises a stator (1) fitted with blades (9) on the inside, and a rotor (2) fitted with external blades (16) and comprising two combustion chambers (3) fed by a centrifugal blower (17) connected to a carburettor. Electronic ignition brings about and sustains the combustion. Exhaust takes place laterally through ports (18) made in the rotor (2). A countercurrent exchanger on the exhaust of the combustion gases reheats the combustion-air/fuel mixture before it is taken up by the blower (17).
FR7801143A 1978-01-11 1978-01-11 REACTION TURBOMOTOR WITH ROTARY COMBUSTION CHAMBERS Granted FR2414627A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR7801143A FR2414627A1 (en) 1978-01-11 1978-01-11 REACTION TURBOMOTOR WITH ROTARY COMBUSTION CHAMBERS
CH874978A CH638016A5 (en) 1978-01-11 1978-08-17 Turbo-jet engine with rotary combustion chambers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7801143A FR2414627A1 (en) 1978-01-11 1978-01-11 REACTION TURBOMOTOR WITH ROTARY COMBUSTION CHAMBERS

Publications (2)

Publication Number Publication Date
FR2414627A1 true FR2414627A1 (en) 1979-08-10
FR2414627B3 FR2414627B3 (en) 1981-11-13

Family

ID=9203512

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7801143A Granted FR2414627A1 (en) 1978-01-11 1978-01-11 REACTION TURBOMOTOR WITH ROTARY COMBUSTION CHAMBERS

Country Status (2)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0961872A2 (en) * 1997-10-22 1999-12-08 James T. Ray Micro-combustion chamber heat engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0961872A2 (en) * 1997-10-22 1999-12-08 James T. Ray Micro-combustion chamber heat engine
EP0961872A4 (en) * 1997-10-22 2003-07-09 James T Ray Micro-combustion chamber heat engine

Also Published As

Publication number Publication date
FR2414627B3 (en) 1981-11-13
CH638016A5 (en) 1983-08-31

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Legal Events

Date Code Title Description
ST Notification of lapse