FR1104809A - Perfectionnements apportés aux dispositifs de combustion avec vaporisation - Google Patents

Perfectionnements apportés aux dispositifs de combustion avec vaporisation

Info

Publication number
FR1104809A
FR1104809A FR1104809DA FR1104809A FR 1104809 A FR1104809 A FR 1104809A FR 1104809D A FR1104809D A FR 1104809DA FR 1104809 A FR1104809 A FR 1104809A
Authority
FR
France
Prior art keywords
vaporization
improvements made
combustion devices
combustion
devices
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
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research 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 Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Application granted granted Critical
Publication of FR1104809A publication Critical patent/FR1104809A/fr
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)
FR1104809D 1953-04-22 1954-04-22 Perfectionnements apportés aux dispositifs de combustion avec vaporisation Expired FR1104809A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1104809X 1953-04-22

Publications (1)

Publication Number Publication Date
FR1104809A true FR1104809A (fr) 1955-11-24

Family

ID=10874348

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1104809D Expired FR1104809A (fr) 1953-04-22 1954-04-22 Perfectionnements apportés aux dispositifs de combustion avec vaporisation

Country Status (1)

Country Link
FR (1) FR1104809A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020239702A1 (fr) * 2019-05-28 2020-12-03 Safran Helicopter Engines Canne de prévaporisation, ensemble de combustion muni de celle-ci et turbomachine munie de celui-ci

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020239702A1 (fr) * 2019-05-28 2020-12-03 Safran Helicopter Engines Canne de prévaporisation, ensemble de combustion muni de celle-ci et turbomachine munie de celui-ci
FR3096761A1 (fr) * 2019-05-28 2020-12-04 Safran Helicopter Engines Canne de prévaporisation, ensemble de combustion muni de celle-ci et turbomachine munie de celui-ci
CN113924445A (zh) * 2019-05-28 2022-01-11 赛峰直升机发动机公司 预蒸发管、设置有预蒸发管的燃烧组件以及设置有燃烧组件的涡轮机
CN113924445B (zh) * 2019-05-28 2023-11-21 赛峰直升机发动机公司 预蒸发管、设置有预蒸发管的燃烧组件以及设置有燃烧组件的涡轮机
US11867401B2 (en) 2019-05-28 2024-01-09 Safran Helicopter Engines Pre-vaporizing pipe, combustion assembly provided therewith and turbomachine provided therewith

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