FR1047521A - Vaporization tube device, in particular for aircraft turbo-engines - Google Patents

Vaporization tube device, in particular for aircraft turbo-engines

Info

Publication number
FR1047521A
FR1047521A FR1047521DA FR1047521A FR 1047521 A FR1047521 A FR 1047521A FR 1047521D A FR1047521D A FR 1047521DA FR 1047521 A FR1047521 A FR 1047521A
Authority
FR
France
Prior art keywords
engines
tube device
vaporization tube
aircraft turbo
turbo
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 FR1047521A publication Critical patent/FR1047521A/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
    • F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
    • F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1047521D 1951-01-06 1952-01-04 Vaporization tube device, in particular for aircraft turbo-engines Expired FR1047521A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US1047521XA 1951-01-06 1951-01-06

Publications (1)

Publication Number Publication Date
FR1047521A true FR1047521A (en) 1953-12-15

Family

ID=22302174

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1047521D Expired FR1047521A (en) 1951-01-06 1952-01-04 Vaporization tube device, in particular for aircraft turbo-engines

Country Status (1)

Country Link
FR (1) FR1047521A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112082176A (en) * 2020-09-14 2020-12-15 清华大学 Combustion chamber structure of micro turbojet engine
CN114484501A (en) * 2022-02-16 2022-05-13 浙江意动科技股份有限公司 Evaporation tube type combustion chamber
CN112082176B (en) * 2020-09-14 2024-06-04 清华大学 Combustion chamber of miniature turbojet engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN112082176A (en) * 2020-09-14 2020-12-15 清华大学 Combustion chamber structure of micro turbojet engine
CN112082176B (en) * 2020-09-14 2024-06-04 清华大学 Combustion chamber of miniature turbojet engine
CN114484501A (en) * 2022-02-16 2022-05-13 浙江意动科技股份有限公司 Evaporation tube type combustion chamber

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