FR1488824A - Installation of the nozzle body for hook-shaped fuel injection nozzles on the combustion chamber of gas turbine reactors - Google Patents

Installation of the nozzle body for hook-shaped fuel injection nozzles on the combustion chamber of gas turbine reactors

Info

Publication number
FR1488824A
FR1488824A FR72356A FR72356A FR1488824A FR 1488824 A FR1488824 A FR 1488824A FR 72356 A FR72356 A FR 72356A FR 72356 A FR72356 A FR 72356A FR 1488824 A FR1488824 A FR 1488824A
Authority
FR
France
Prior art keywords
hook
installation
combustion chamber
fuel injection
gas turbine
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
FR72356A
Other languages
French (fr)
Inventor
Christian Schmitz
Werner Bruder
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.)
Daimler Benz AG
Original Assignee
Daimler Benz AG
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 Daimler Benz AG filed Critical Daimler Benz AG
Priority to FR72356A priority Critical patent/FR1488824A/en
Application granted granted Critical
Publication of FR1488824A publication Critical patent/FR1488824A/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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR72356A 1966-08-08 1966-08-08 Installation of the nozzle body for hook-shaped fuel injection nozzles on the combustion chamber of gas turbine reactors Expired FR1488824A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR72356A FR1488824A (en) 1966-08-08 1966-08-08 Installation of the nozzle body for hook-shaped fuel injection nozzles on the combustion chamber of gas turbine reactors

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR72356A FR1488824A (en) 1966-08-08 1966-08-08 Installation of the nozzle body for hook-shaped fuel injection nozzles on the combustion chamber of gas turbine reactors

Publications (1)

Publication Number Publication Date
FR1488824A true FR1488824A (en) 1967-07-13

Family

ID=8615024

Family Applications (1)

Application Number Title Priority Date Filing Date
FR72356A Expired FR1488824A (en) 1966-08-08 1966-08-08 Installation of the nozzle body for hook-shaped fuel injection nozzles on the combustion chamber of gas turbine reactors

Country Status (1)

Country Link
FR (1) FR1488824A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2935777A1 (en) * 2008-09-09 2010-03-12 Snecma TURBOMACHINE COMBUSTION CHAMBER
CN110454237A (en) * 2019-08-28 2019-11-15 天津大学 A kind of supercritical carbon dioxide turbo-expander multistage carbocyclic ring labyrinth seal structure

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2935777A1 (en) * 2008-09-09 2010-03-12 Snecma TURBOMACHINE COMBUSTION CHAMBER
US8516830B2 (en) 2008-09-09 2013-08-27 Snecma Turbomachine combustion chamber
CN110454237A (en) * 2019-08-28 2019-11-15 天津大学 A kind of supercritical carbon dioxide turbo-expander multistage carbocyclic ring labyrinth seal structure

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