GB717581A - Improvements in and relating to gas turbine power plants - Google Patents

Improvements in and relating to gas turbine power plants

Info

Publication number
GB717581A
GB717581A GB1507751A GB1507751A GB717581A GB 717581 A GB717581 A GB 717581A GB 1507751 A GB1507751 A GB 1507751A GB 1507751 A GB1507751 A GB 1507751A GB 717581 A GB717581 A GB 717581A
Authority
GB
United Kingdom
Prior art keywords
outer casing
casing
gas turbine
connects
casting
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
GB1507751A
Inventor
Paul Kolb
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.)
CA Parsons and Co Ltd
Original Assignee
CA Parsons and Co 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 CA Parsons and Co Ltd filed Critical CA Parsons and Co Ltd
Priority to GB1507751A priority Critical patent/GB717581A/en
Publication of GB717581A publication Critical patent/GB717581A/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

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

717,581. Gas turbine plant. PARSONS & CO., Ltd., C. A. May 28, 1952 [June 25, 1951], No. 15077/51. Class 110(3) [Also in Group XII] A gas turbine plant comprising an annular combustion chamber, the outer casing of which connects the compressor casing to the turbine casing, has the outer wall of the flame tube sub-divided into segments, a number of which are fixed to the outer casing and the remainder to detachable cover plates which cover openings in the outer casing. The shaft 2 which connects the compressor 1 and-turbine 3 is mounted in bearings 5 housed in a casting 6 which also forms the inner casing of the combustion chamber. A separate casting 9 which forms the outer casing not only connects but supports and holds together the turbine and compressor casings. The casting 6 is protected against heat by an annular sheet 11 enclosing a lagged space 12. The flame tube consists of eighteen segments 14, twelve of which are attached to the outer casing 9 and six to the cover plates 15. A burner 16, supplied with liquid or solid fuel through pipes 17, 18, is also subdivided into eighteen parts.
GB1507751A 1951-06-25 1951-06-25 Improvements in and relating to gas turbine power plants Expired GB717581A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1507751A GB717581A (en) 1951-06-25 1951-06-25 Improvements in and relating to gas turbine power plants

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1507751A GB717581A (en) 1951-06-25 1951-06-25 Improvements in and relating to gas turbine power plants

Publications (1)

Publication Number Publication Date
GB717581A true GB717581A (en) 1954-10-27

Family

ID=10052605

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1507751A Expired GB717581A (en) 1951-06-25 1951-06-25 Improvements in and relating to gas turbine power plants

Country Status (1)

Country Link
GB (1) GB717581A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2892181A1 (en) * 2005-10-18 2007-04-20 Snecma Sa Combustion chamber module for aircraft jet engines comprises combustion chamber, front end of whose external wall is attached to annular bracket with radial bars which fit into groove in wall of frame

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2892181A1 (en) * 2005-10-18 2007-04-20 Snecma Sa Combustion chamber module for aircraft jet engines comprises combustion chamber, front end of whose external wall is attached to annular bracket with radial bars which fit into groove in wall of frame
EP1777460A1 (en) * 2005-10-18 2007-04-25 Snecma Fastening of a combustion chamber inside its housing
US7752851B2 (en) 2005-10-18 2010-07-13 Snecma Fastening a combustion chamber inside its casing

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