FR1228764A - Tuyère aérodynamique de réaction - Google Patents

Tuyère aérodynamique de réaction

Info

Publication number
FR1228764A
FR1228764A FR798766A FR798766A FR1228764A FR 1228764 A FR1228764 A FR 1228764A FR 798766 A FR798766 A FR 798766A FR 798766 A FR798766 A FR 798766A FR 1228764 A FR1228764 A FR 1228764A
Authority
FR
France
Prior art keywords
reaction nozzle
aerodynamic reaction
aerodynamic
nozzle
reaction
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
FR798766A
Other languages
English (en)
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.)
General Electric Co
Original Assignee
General Electric Co
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
Priority claimed from GB1245258A external-priority patent/GB884587A/en
Application filed by General Electric Co filed Critical General Electric Co
Priority to FR798766A priority Critical patent/FR1228764A/fr
Application granted granted Critical
Publication of FR1228764A publication Critical patent/FR1228764A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1238—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, the upstream series having its flaps hinged at their upstream ends on a fixed structure and the downstream series having its flaps hinged at their upstream ends on a substantially axially movable structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR798766A 1958-04-18 1959-06-29 Tuyère aérodynamique de réaction Expired FR1228764A (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR798766A FR1228764A (fr) 1958-04-18 1959-06-29 Tuyère aérodynamique de réaction

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1245258A GB884587A (en) 1958-04-18 1958-04-18 Improvements in jet propulsion nozzles
FR798766A FR1228764A (fr) 1958-04-18 1959-06-29 Tuyère aérodynamique de réaction

Publications (1)

Publication Number Publication Date
FR1228764A true FR1228764A (fr) 1960-09-02

Family

ID=26184150

Family Applications (1)

Application Number Title Priority Date Filing Date
FR798766A Expired FR1228764A (fr) 1958-04-18 1959-06-29 Tuyère aérodynamique de réaction

Country Status (1)

Country Link
FR (1) FR1228764A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116220921A (zh) * 2022-12-31 2023-06-06 中国航发沈阳发动机研究所 一种喷口控制回路执行机构动态特性评估指标生成方法

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN116220921A (zh) * 2022-12-31 2023-06-06 中国航发沈阳发动机研究所 一种喷口控制回路执行机构动态特性评估指标生成方法

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