GB671937A - Improvements in combustion apparatus - Google Patents

Improvements in combustion apparatus

Info

Publication number
GB671937A
GB671937A GB7823/49A GB782349A GB671937A GB 671937 A GB671937 A GB 671937A GB 7823/49 A GB7823/49 A GB 7823/49A GB 782349 A GB782349 A GB 782349A GB 671937 A GB671937 A GB 671937A
Authority
GB
United Kingdom
Prior art keywords
baffle
airjacketed
combustion chamber
tangential entries
combustion
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
GB7823/49A
Inventor
Ernest Frederick Winter
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
Priority to GB7823/49A priority Critical patent/GB671937A/en
Publication of GB671937A publication Critical patent/GB671937A/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
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)

Abstract

671,937. Generating combustion products under pressure. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. June 21, 1950 [March 22, 1949], No. 7823/49. Class 51 (i). [Also in Group XI] In a combustion chamber having an airjacketed flame tube in which is disposed a hollow baffle defining a primary combustion zone, a circular series of tangential entries is provided in the baffle extending along the length of the baffle so that the inner surface of the baffle is swept by a high-velocity air stream. The baffle comprises a conical portion 6 and a cylindrical portion 7, the tangential entries being in the form of scoops 8 and those in the two portions of the baffle are preferably oppositely handed. Atomized liquid fuel or pulverized solid fuel may be used. The combustion chamber described in the Provisional Specification is not essentially of the airjacketed type. Specifications 636,624 and 639,468 are referred to.
GB7823/49A 1949-03-22 1949-03-22 Improvements in combustion apparatus Expired GB671937A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB7823/49A GB671937A (en) 1949-03-22 1949-03-22 Improvements in combustion apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7823/49A GB671937A (en) 1949-03-22 1949-03-22 Improvements in combustion apparatus

Publications (1)

Publication Number Publication Date
GB671937A true GB671937A (en) 1952-05-14

Family

ID=9840438

Family Applications (1)

Application Number Title Priority Date Filing Date
GB7823/49A Expired GB671937A (en) 1949-03-22 1949-03-22 Improvements in combustion apparatus

Country Status (1)

Country Link
GB (1) GB671937A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930192A (en) * 1953-12-07 1960-03-29 Gen Electric Reverse vortex combustion chamber
US4429538A (en) 1980-03-05 1984-02-07 Hitachi, Ltd. Gas turbine combustor
WO2020120828A1 (en) * 2018-12-14 2020-06-18 Fortum Oyj Method for burning fuel, burner and boiler
CN117943978A (en) * 2024-03-21 2024-04-30 湖北三江博力智能装备有限公司 Movable arm of abrasive striking and sand blasting robot
CN117943978B (en) * 2024-03-21 2024-06-11 湖北三江博力智能装备有限公司 Movable arm of abrasive striking and sand blasting robot

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930192A (en) * 1953-12-07 1960-03-29 Gen Electric Reverse vortex combustion chamber
US4429538A (en) 1980-03-05 1984-02-07 Hitachi, Ltd. Gas turbine combustor
WO2020120828A1 (en) * 2018-12-14 2020-06-18 Fortum Oyj Method for burning fuel, burner and boiler
CN117943978A (en) * 2024-03-21 2024-04-30 湖北三江博力智能装备有限公司 Movable arm of abrasive striking and sand blasting robot
CN117943978B (en) * 2024-03-21 2024-06-11 湖北三江博力智能装备有限公司 Movable arm of abrasive striking and sand blasting robot

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