GB901044A - A gas turbine combustion chamber - Google Patents

A gas turbine combustion chamber

Info

Publication number
GB901044A
GB901044A GB1040959A GB1040959A GB901044A GB 901044 A GB901044 A GB 901044A GB 1040959 A GB1040959 A GB 1040959A GB 1040959 A GB1040959 A GB 1040959A GB 901044 A GB901044 A GB 901044A
Authority
GB
United Kingdom
Prior art keywords
segments
plates
combustion chamber
fins
radial
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
GB1040959A
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.)
ZD Y V I PLZEN
Zavody VI Lenina Plzen np
Original Assignee
ZD Y V I PLZEN
Zavody VI Lenina Plzen np
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 ZD Y V I PLZEN, Zavody VI Lenina Plzen np filed Critical ZD Y V I PLZEN
Publication of GB901044A publication Critical patent/GB901044A/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F23R3/002—Wall structures
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]

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)

Abstract

901,044. Generating combustion products under pressure. ZAVODY V.I. LENINA PLZEN NARODNI PODNIK. March 25, 1959 [March 25, 1958], No. 10409/59. Class 51(1). A gas-turbine combustion chamber has a combustion chamber lining of cylindrical or conical shape formed by a number of segments on which are mounted longitudinal cooling fins and supporting rings comprising plates, each welded to at least two fins, each plate being formed of two axially offset parts and an oblique connecting part. The thermal stresses in cooling fins 2 are relieved by radial slots 7. Adequate rigidity is provided by joining each fin to its adjacent fins by plates 3 and the gaps 6 between the plates 3 are disposed over the slots 7. Cooling air is admitted to the combustion zone through gaps 8 between the segments which may have a ceramic lining 9. The segments are mounted on pins sliding in sleeves, the pins being urged radially outwardly by springs. The pin in each suspension 4 has sufficient clearance in a hole at the bottom of the sleeve to allow for radial and circumferential displacement, whereas each suspension 5 allows only for radial displacement.
GB1040959A 1958-03-25 1959-03-25 A gas turbine combustion chamber Expired GB901044A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CS155758 1958-03-25

Publications (1)

Publication Number Publication Date
GB901044A true GB901044A (en) 1962-07-11

Family

ID=5350220

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1040959A Expired GB901044A (en) 1958-03-25 1959-03-25 A gas turbine combustion chamber

Country Status (3)

Country Link
CH (1) CH372507A (en)
FR (1) FR1228407A (en)
GB (1) GB901044A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2147405A (en) * 1983-09-28 1985-05-09 Rolls Royce Gas turbine engine combustion chamber mounting
EP0994304A3 (en) * 1998-10-15 2002-01-02 United Technologies Corporation Thermally compliant liner

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4748806A (en) * 1985-07-03 1988-06-07 United Technologies Corporation Attachment means

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2147405A (en) * 1983-09-28 1985-05-09 Rolls Royce Gas turbine engine combustion chamber mounting
EP0994304A3 (en) * 1998-10-15 2002-01-02 United Technologies Corporation Thermally compliant liner

Also Published As

Publication number Publication date
CH372507A (en) 1963-10-15
FR1228407A (en) 1960-08-29

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