FR1033404A - Combined ignition device for gas turbo-engines - Google Patents

Combined ignition device for gas turbo-engines

Info

Publication number
FR1033404A
FR1033404A FR1033404DA FR1033404A FR 1033404 A FR1033404 A FR 1033404A FR 1033404D A FR1033404D A FR 1033404DA FR 1033404 A FR1033404 A FR 1033404A
Authority
FR
France
Prior art keywords
engines
ignition device
gas turbo
combined ignition
combined
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
Other languages
French (fr)
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.)
Canadian Patents and Development Ltd
Original Assignee
Canadian Patents and Development Ltd
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 Canadian Patents and Development Ltd filed Critical Canadian Patents and Development Ltd
Application granted granted Critical
Publication of FR1033404A publication Critical patent/FR1033404A/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • F23R3/48—Flame tube interconnectors, e.g. cross-over tubes
    • 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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/26—Starting; Ignition
    • F02C7/264—Ignition
    • F02C7/266—Electric
FR1033404D 1950-03-06 1951-03-05 Combined ignition device for gas turbo-engines Expired FR1033404A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB310034X 1950-03-06

Publications (1)

Publication Number Publication Date
FR1033404A true FR1033404A (en) 1953-07-10

Family

ID=10316462

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1033404D Expired FR1033404A (en) 1950-03-06 1951-03-05 Combined ignition device for gas turbo-engines

Country Status (4)

Country Link
CH (1) CH310034A (en)
DE (1) DE882775C (en)
FR (1) FR1033404A (en)
GB (1) GB691366A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2952126A (en) * 1955-05-10 1960-09-13 Midland Ross Corp Combustion unit for supplying hot gas for jet aircraft

Also Published As

Publication number Publication date
CH310034A (en) 1955-09-30
DE882775C (en) 1953-07-13
GB691366A (en) 1953-05-13

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