IT8241540A0 - COMBUSTOR FOR TURBINE WITH IMPROVED COOLING OF THE WALLS. - Google Patents

COMBUSTOR FOR TURBINE WITH IMPROVED COOLING OF THE WALLS.

Info

Publication number
IT8241540A0
IT8241540A0 IT8241540A IT4154082A IT8241540A0 IT 8241540 A0 IT8241540 A0 IT 8241540A0 IT 8241540 A IT8241540 A IT 8241540A IT 4154082 A IT4154082 A IT 4154082A IT 8241540 A0 IT8241540 A0 IT 8241540A0
Authority
IT
Italy
Prior art keywords
combustor
turbine
walls
improved cooling
cooling
Prior art date
Application number
IT8241540A
Other languages
Italian (it)
Other versions
IT1158276B (en
IT8241540A1 (en
Inventor
Edward W Tobery
Stephen R Parker
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of IT8241540A0 publication Critical patent/IT8241540A0/en
Publication of IT8241540A1 publication Critical patent/IT8241540A1/en
Application granted granted Critical
Publication of IT1158276B publication Critical patent/IT1158276B/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
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
IT41540/82A 1981-03-27 1982-03-26 COMBUSTOR FOR IMPROVED COOLING TURBINES OF THE WALLS IT1158276B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US24812381A 1981-03-27 1981-03-27

Publications (3)

Publication Number Publication Date
IT8241540A0 true IT8241540A0 (en) 1982-03-26
IT8241540A1 IT8241540A1 (en) 1983-09-26
IT1158276B IT1158276B (en) 1987-02-18

Family

ID=22937770

Family Applications (1)

Application Number Title Priority Date Filing Date
IT41540/82A IT1158276B (en) 1981-03-27 1982-03-26 COMBUSTOR FOR IMPROVED COOLING TURBINES OF THE WALLS

Country Status (8)

Country Link
JP (1) JPS6055723B2 (en)
AR (1) AR227096A1 (en)
BE (1) BE892636A (en)
BR (1) BR8201368A (en)
CA (1) CA1185799A (en)
GB (1) GB2095816B (en)
IT (1) IT1158276B (en)
MX (1) MX156585A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN85107191A (en) * 1984-10-04 1986-09-24 西屋电气公司 Impact type cooling gas turbine firing chamber with interior air film cooling
DE19631616A1 (en) * 1996-08-05 1998-02-12 Asea Brown Boveri Liquid fuel combustion chamber
FR2826102B1 (en) * 2001-06-19 2004-01-02 Snecma Moteurs IMPROVEMENTS TO GAS TURBINE COMBUSTION CHAMBERS
US8276391B2 (en) * 2010-04-19 2012-10-02 General Electric Company Combustor liner cooling at transition duct interface and related method

Also Published As

Publication number Publication date
AR227096A1 (en) 1982-09-15
IT1158276B (en) 1987-02-18
IT8241540A1 (en) 1983-09-26
BE892636A (en) 1982-09-27
JPS6055723B2 (en) 1985-12-06
JPS57174622A (en) 1982-10-27
GB2095816B (en) 1984-12-12
BR8201368A (en) 1983-01-25
GB2095816A (en) 1982-10-06
CA1185799A (en) 1985-04-23
MX156585A (en) 1988-09-14

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19960126