BE520732A - - Google Patents

Info

Publication number
BE520732A
BE520732A BE520732DA BE520732A BE 520732 A BE520732 A BE 520732A BE 520732D A BE520732D A BE 520732DA BE 520732 A BE520732 A BE 520732A
Authority
BE
Belgium
Prior art keywords
compressor
fuel system
valve
fuel
orifice
Prior art date
Application number
Other languages
English (en)
French (fr)
Publication of BE520732A publication Critical patent/BE520732A/fr

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
BE520732D BE520732A (sv)

Publications (1)

Publication Number Publication Date
BE520732A true BE520732A (sv)

Family

ID=156515

Family Applications (1)

Application Number Title Priority Date Filing Date
BE520732D BE520732A (sv)

Country Status (1)

Country Link
BE (1) BE520732A (sv)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2947141A (en) * 1954-01-04 1960-08-02 Bendix Aviat Corp Fuel feed and power control system for gas turbine engines

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2947141A (en) * 1954-01-04 1960-08-02 Bendix Aviat Corp Fuel feed and power control system for gas turbine engines

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