GB736267A - Improvements in thermal insulator covers for conduits - Google Patents

Improvements in thermal insulator covers for conduits

Info

Publication number
GB736267A
GB736267A GB25416/53A GB2541653A GB736267A GB 736267 A GB736267 A GB 736267A GB 25416/53 A GB25416/53 A GB 25416/53A GB 2541653 A GB2541653 A GB 2541653A GB 736267 A GB736267 A GB 736267A
Authority
GB
United Kingdom
Prior art keywords
cover
conduits
edge
thermal insulator
laced
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
GB25416/53A
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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 Motors Liquidation Co filed Critical Motors Liquidation Co
Publication of GB736267A publication Critical patent/GB736267A/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
    • F02C7/24—Heat or noise insulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L59/00—Thermal insulation in general
    • F16L59/02—Shape or form of insulating materials, with or without coverings integral with the insulating materials
    • F16L59/026—Mattresses, mats, blankets or the like

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Exhaust Silencers (AREA)

Abstract

736,267. Heat insulation. GENERAL MOTORS CORPORATION. Sept. 15, 1953 [Oct. 1, 1952], No. 25416/53. Class 64 (2). A pad 44 of asbestos felt is contained in a skin 46 of nickel-chrome-iron alloy foil to form a cover for a gas turbine exhaust duct 12 and the longitudinal edges are laced together by wires 36, 38 engaging hooks 40 secured to edgeseams of the cover. The join may be covered by a flap 60 spot welded at 62 near one edge of the cover and laced loosely to hooks 70 near the other edge.
GB25416/53A 1952-10-01 1953-09-15 Improvements in thermal insulator covers for conduits Expired GB736267A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US736267XA 1952-10-01 1952-10-01

Publications (1)

Publication Number Publication Date
GB736267A true GB736267A (en) 1955-09-07

Family

ID=22114822

Family Applications (1)

Application Number Title Priority Date Filing Date
GB25416/53A Expired GB736267A (en) 1952-10-01 1953-09-15 Improvements in thermal insulator covers for conduits

Country Status (1)

Country Link
GB (1) GB736267A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0199319A1 (en) * 1985-04-20 1986-10-29 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Device for supporting construction parts exposed to high temperatures at thermally insulated casings
DE4035137A1 (en) * 1990-11-06 1992-05-07 Viessmann Hans DEVICE FOR FIXING HEAT INSULATION MATS
WO1993000506A1 (en) * 1991-06-25 1993-01-07 Isolfeu Ag Thermal machine insulation
US5262217A (en) * 1989-05-04 1993-11-16 Hunter Douglas International N.V. Core arrangement in mineral wool sandwich panel
FR2844303A1 (en) * 2002-09-10 2004-03-12 Airbus France Tubular acoustic attenuation piece for aircraft jet engine air intake, comprises at least two shells with cellular core assembled only by external fish plate strips, with each connection edge being edge face of corresponding shell

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0199319A1 (en) * 1985-04-20 1986-10-29 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Device for supporting construction parts exposed to high temperatures at thermally insulated casings
US5262217A (en) * 1989-05-04 1993-11-16 Hunter Douglas International N.V. Core arrangement in mineral wool sandwich panel
DE4035137A1 (en) * 1990-11-06 1992-05-07 Viessmann Hans DEVICE FOR FIXING HEAT INSULATION MATS
GB2251026A (en) * 1990-11-06 1992-06-24 Hans Viessmann Fixing heat insulating jackets to containers
WO1993000506A1 (en) * 1991-06-25 1993-01-07 Isolfeu Ag Thermal machine insulation
US5336542A (en) * 1991-06-25 1994-08-09 Isolfeu Ag Insulation of thermal machines
FR2844303A1 (en) * 2002-09-10 2004-03-12 Airbus France Tubular acoustic attenuation piece for aircraft jet engine air intake, comprises at least two shells with cellular core assembled only by external fish plate strips, with each connection edge being edge face of corresponding shell
EP1398472A1 (en) * 2002-09-10 2004-03-17 AIRBUS France Tubular acoustic attenuation piece for the air inlet of an aircraft engine
US6761245B2 (en) 2002-09-10 2004-07-13 Airbus France Tubular acoustic attenuation piece for an aircraft jet engine air intake

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