GB892885A - Support for bodies subject to differential expansion - Google Patents

Support for bodies subject to differential expansion

Info

Publication number
GB892885A
GB892885A GB3439158A GB3439158A GB892885A GB 892885 A GB892885 A GB 892885A GB 3439158 A GB3439158 A GB 3439158A GB 3439158 A GB3439158 A GB 3439158A GB 892885 A GB892885 A GB 892885A
Authority
GB
United Kingdom
Prior art keywords
support
welded
differential expansion
gas turbine
bodies subject
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
GB3439158A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB3439158A priority Critical patent/GB892885A/en
Publication of GB892885A publication Critical patent/GB892885A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/222—Fuel flow conduits, e.g. manifolds

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supports For Pipes And Cables (AREA)

Abstract

892,885. Gas turbine plant. MORRIS, V. S. Oct. 27, 1958, No. 34391/58. Class 110 (3). In a gas turbine, the fuel manifold is a circular length of tubing mounted on and surrounding the turbine outer casing. To permit unrestrained differential radial thermal dimension changes, the mountings securing the tube 1 to the casing 2 consist of a forked member 5, welded to 1, and slidable in the channels of an engaging block 6. The latter is bolted to the L-bracket 3, welded to 2. In an alternative form, the positions of members 5, 6 may be reversed.
GB3439158A 1958-10-27 1958-10-27 Support for bodies subject to differential expansion Expired GB892885A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3439158A GB892885A (en) 1958-10-27 1958-10-27 Support for bodies subject to differential expansion

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3439158A GB892885A (en) 1958-10-27 1958-10-27 Support for bodies subject to differential expansion

Publications (1)

Publication Number Publication Date
GB892885A true GB892885A (en) 1962-04-04

Family

ID=10365069

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3439158A Expired GB892885A (en) 1958-10-27 1958-10-27 Support for bodies subject to differential expansion

Country Status (1)

Country Link
GB (1) GB892885A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4696431A (en) * 1985-11-29 1987-09-29 United Technologies Corporation Augmentor liner support band having finger positioners

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4696431A (en) * 1985-11-29 1987-09-29 United Technologies Corporation Augmentor liner support band having finger positioners

Similar Documents

Publication Publication Date Title
GB1303962A (en)
GB836088A (en) Improvements in turbojet engine afterburners
FR2426158A1 (en) COMBINED GAS AND STEAM POWER PLANT WITH BACK PRESSURE TURBINE, ESPECIALLY FOR INDUSTRIAL APPLICATIONS
CH388022A (en) Combustion chamber for the simultaneous combustion of gaseous and non-gaseous fuels, especially for gas turbine systems
GB892885A (en) Support for bodies subject to differential expansion
FR1302273A (en) Chamber for the simultaneous combustion of gaseous and non-gaseous fuels, in particular for gas turbine installations
JPS5340120A (en) Air supply unit for thermal reactor
CA948421A (en) Fuel supply systems for gas turbine engines
GB855469A (en) Gas turbine engine afterburner
GB888109A (en) Improvements relating to gas turbine power plant
GB889308A (en) Improvements in or relating to shielding devices for members such as pipes
CA523686A (en) Means for conducting the flow of liquid fuel for feeding burners of gas turbine engines
CA607893A (en) Flame tubes for use in combustion systems of gas turbine engines
CA566028A (en) Fuel supply systems for gas turbine engines
CA579034A (en) Flame tubes for use in combustion systems of gas turbine engines
CA573550A (en) Gas turbine engine fuel systems
CA576083A (en) Igniters for gas turbine engines, combustion heaters, thermal de-icing plant and the like
AU201732B2 (en) Improvements in fuel supply systems for. gas turbine engines
CA539069A (en) Gas turbine engine fuel systems
AU234591B2 (en) Exhaust cone forthe jet pipe ofa gas turbine engine
CA565352A (en) Gas turbine engine fuel systems
CA566947A (en) Starting and fuel pumping means for gas turbine engines
GB791628A (en) Improvements in and relating to steam admission systems for turbines
AU751855A (en) Improvements in fuel supply systems for. gas turbine engines
CA564232A (en) Fuel systems for gas turbine engines