SG106085A1 - Preferential multihole combustor liner - Google Patents

Preferential multihole combustor liner

Info

Publication number
SG106085A1
SG106085A1 SG200204908A SG200204908A SG106085A1 SG 106085 A1 SG106085 A1 SG 106085A1 SG 200204908 A SG200204908 A SG 200204908A SG 200204908 A SG200204908 A SG 200204908A SG 106085 A1 SG106085 A1 SG 106085A1
Authority
SG
Singapore
Prior art keywords
multihole
preferential
combustor liner
combustor
liner
Prior art date
Application number
SG200204908A
Other languages
English (en)
Inventor
Dale Brown Daniel
Farmer Gilbert
Edward Rutherford Myron
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of SG106085A1 publication Critical patent/SG106085A1/en

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
    • F23R3/06—Arrangement of apertures along the flame tube
    • 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)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gas Burners (AREA)
  • Spray-Type Burners (AREA)
SG200204908A 2001-08-21 2002-08-13 Preferential multihole combustor liner SG106085A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/934,182 US6513331B1 (en) 2001-08-21 2001-08-21 Preferential multihole combustor liner

Publications (1)

Publication Number Publication Date
SG106085A1 true SG106085A1 (en) 2004-09-30

Family

ID=25465105

Family Applications (1)

Application Number Title Priority Date Filing Date
SG200204908A SG106085A1 (en) 2001-08-21 2002-08-13 Preferential multihole combustor liner

Country Status (7)

Country Link
US (2) US6513331B1 (fr)
EP (1) EP1286117A1 (fr)
JP (1) JP4256128B2 (fr)
BR (1) BR0203357B1 (fr)
CA (2) CA2626439C (fr)
MX (1) MXPA02007988A (fr)
SG (1) SG106085A1 (fr)

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US11112115B2 (en) 2013-08-30 2021-09-07 Raytheon Technologies Corporation Contoured dilution passages for gas turbine engine combustor
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Also Published As

Publication number Publication date
CA2397455A1 (fr) 2003-02-21
MXPA02007988A (es) 2003-02-26
CA2626439C (fr) 2009-06-09
US6655149B2 (en) 2003-12-02
US20030167772A1 (en) 2003-09-11
BR0203357A (pt) 2003-05-27
JP2003114023A (ja) 2003-04-18
CA2397455C (fr) 2009-06-23
CA2626439A1 (fr) 2003-02-21
US6513331B1 (en) 2003-02-04
EP1286117A1 (fr) 2003-02-26
JP4256128B2 (ja) 2009-04-22
BR0203357B1 (pt) 2011-12-27

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