FR85730E - Improvements to jet thruster combustion devices, particularly applicable to post-combustion - Google Patents

Improvements to jet thruster combustion devices, particularly applicable to post-combustion

Info

Publication number
FR85730E
FR85730E FR974179A FR974179A FR85730E FR 85730 E FR85730 E FR 85730E FR 974179 A FR974179 A FR 974179A FR 974179 A FR974179 A FR 974179A FR 85730 E FR85730 E FR 85730E
Authority
FR
France
Prior art keywords
combustion
post
particularly applicable
jet thruster
devices
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
FR974179A
Other languages
French (fr)
Inventor
Rene Leon Constant
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR974179A priority Critical patent/FR85730E/en
Priority to DE1965S0052612 priority patent/DE1950033U/en
Priority to GB2006465A priority patent/GB1092643A/en
Application granted granted Critical
Publication of FR85730E publication Critical patent/FR85730E/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/20—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants incorporating fuel injection means

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Spray-Type Burners (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
FR974179A 1964-05-12 1964-05-12 Improvements to jet thruster combustion devices, particularly applicable to post-combustion Expired FR85730E (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR974179A FR85730E (en) 1964-05-12 1964-05-12 Improvements to jet thruster combustion devices, particularly applicable to post-combustion
DE1965S0052612 DE1950033U (en) 1964-05-12 1965-05-10 COMBUSTION DEVICE ON REFLECTIVE ENGINES, IN PARTICULAR FOR POST-COMBUSTION
GB2006465A GB1092643A (en) 1964-05-12 1965-05-12 Improvements to combustion devices for gas turbine jet propulsion engines, applicable more particularly to reheat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR974179A FR85730E (en) 1964-05-12 1964-05-12 Improvements to jet thruster combustion devices, particularly applicable to post-combustion

Publications (1)

Publication Number Publication Date
FR85730E true FR85730E (en) 1965-10-01

Family

ID=8829836

Family Applications (1)

Application Number Title Priority Date Filing Date
FR974179A Expired FR85730E (en) 1964-05-12 1964-05-12 Improvements to jet thruster combustion devices, particularly applicable to post-combustion

Country Status (3)

Country Link
DE (1) DE1950033U (en)
FR (1) FR85730E (en)
GB (1) GB1092643A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2586792A1 (en) * 1985-09-03 1987-03-06 Snecma CONNECTING DEVICE BETWEEN A BURNER RING OR FLAME RING IN COMPOSITE MATERIAL AND A POST-COMBUSTION CHAMBER CHANNEL OF A TURBOJETACTOR
US10578021B2 (en) * 2015-06-26 2020-03-03 Delavan Inc Combustion systems

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2873408B1 (en) * 2004-07-23 2008-10-17 Snecma Moteurs Sa TURBOREACTOR WITH A PROTECTION SCREEN OF THE FUEL RAMP OF A BURNER RING, THE BURNER RING AND THE PROTECTION SCREEN

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2586792A1 (en) * 1985-09-03 1987-03-06 Snecma CONNECTING DEVICE BETWEEN A BURNER RING OR FLAME RING IN COMPOSITE MATERIAL AND A POST-COMBUSTION CHAMBER CHANNEL OF A TURBOJETACTOR
EP0234137A1 (en) * 1985-09-03 1987-09-02 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Attaching means for a flame holder, or annular burner, of composite material for a turbo jet
US10578021B2 (en) * 2015-06-26 2020-03-03 Delavan Inc Combustion systems

Also Published As

Publication number Publication date
GB1092643A (en) 1967-11-29
DE1950033U (en) 1966-11-17

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