GB698539A - Expansible connecting element - Google Patents

Expansible connecting element

Info

Publication number
GB698539A
GB698539A GB13965/52A GB1396552A GB698539A GB 698539 A GB698539 A GB 698539A GB 13965/52 A GB13965/52 A GB 13965/52A GB 1396552 A GB1396552 A GB 1396552A GB 698539 A GB698539 A GB 698539A
Authority
GB
United Kingdom
Prior art keywords
cylinders
connecting element
expansible connecting
expansible
xxviii
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
GB13965/52A
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.)
SVENSKA TURBINFAB AB
Original Assignee
SVENSKA TURBINFAB AB
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 SVENSKA TURBINFAB AB filed Critical SVENSKA TURBINFAB AB
Publication of GB698539A publication Critical patent/GB698539A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26—Double casings; Measures against temperature strain in casings
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/60—Assembly methods
    • F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
    • F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Arc Welding In General (AREA)

Abstract

698,539. Welding by pressure. SVENSKA TURBINFABRIKS AKTIEBOLAGET LJUNGSTROM. June 3, 1952 [Aug. 23, 1951], No. 13965/52. Class 83 (iv). [Also in Groups XXII and XXVIII] Two cylinders 1, 2 are connected by an expansion joint comprising a slotted ring 4 which is welded to the cylinders where shown. Electrodes may be placed outside surface 5 and inside the cylinder 1 near the place 6, a connecting piece bridging the gap. Beryllium bronze may be used.
GB13965/52A 1951-08-23 1952-06-03 Expansible connecting element Expired GB698539A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE698539X 1951-08-23

Publications (1)

Publication Number Publication Date
GB698539A true GB698539A (en) 1953-10-14

Family

ID=20315407

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13965/52A Expired GB698539A (en) 1951-08-23 1952-06-03 Expansible connecting element

Country Status (1)

Country Link
GB (1) GB698539A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2356000A1 (en) * 1976-06-21 1978-01-20 Gen Electric TURBOMACHINE COMBUSTION CHAMBER SUPPORT DEVICE
EP0073689A1 (en) * 1981-08-31 1983-03-09 Elliott Turbomachinery Company, Inc. Method and apparatus for controlling thermal growth
GB2117102A (en) * 1982-03-20 1983-10-05 Rolls Royce Improvements in or relating to mounting arrangements for combustion equipment
FR2538508A1 (en) * 1982-12-08 1984-06-29 Gen Electric COMBUSTION CHAMBER SHIRT AND METHOD OF MANUFACTURE
EP0116160A1 (en) * 1983-01-18 1984-08-22 BBC Brown Boveri AG Turbocharger having bearings at the ends of its shaft and an uncooled gas conduit
EP1249663A2 (en) * 2001-04-10 2002-10-16 FIATAVIO S.p.A. Gas turbine combustor, particularly for an aircraft engine

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2356000A1 (en) * 1976-06-21 1978-01-20 Gen Electric TURBOMACHINE COMBUSTION CHAMBER SUPPORT DEVICE
EP0073689A1 (en) * 1981-08-31 1983-03-09 Elliott Turbomachinery Company, Inc. Method and apparatus for controlling thermal growth
GB2117102A (en) * 1982-03-20 1983-10-05 Rolls Royce Improvements in or relating to mounting arrangements for combustion equipment
FR2538508A1 (en) * 1982-12-08 1984-06-29 Gen Electric COMBUSTION CHAMBER SHIRT AND METHOD OF MANUFACTURE
EP0116160A1 (en) * 1983-01-18 1984-08-22 BBC Brown Boveri AG Turbocharger having bearings at the ends of its shaft and an uncooled gas conduit
EP1249663A2 (en) * 2001-04-10 2002-10-16 FIATAVIO S.p.A. Gas turbine combustor, particularly for an aircraft engine
EP1249663A3 (en) * 2001-04-10 2002-11-20 FIATAVIO S.p.A. Gas turbine combustor, particularly for an aircraft engine
US6810672B2 (en) 2001-04-10 2004-11-02 Fiatavio S.P.A. Gas turbine combustor, particularly for an aircraft engine

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