FR1221234A - Ensembles de canalisations - Google Patents

Ensembles de canalisations

Info

Publication number
FR1221234A
FR1221234A FR788437A FR788437A FR1221234A FR 1221234 A FR1221234 A FR 1221234A FR 788437 A FR788437 A FR 788437A FR 788437 A FR788437 A FR 788437A FR 1221234 A FR1221234 A FR 1221234A
Authority
FR
France
Prior art keywords
pipe sets
sets
pipe
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
FR788437A
Other languages
English (en)
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.)
Bristol Siddeley Engines Ltd
Original Assignee
De Havilland Engine 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 De Havilland Engine Co Ltd filed Critical De Havilland Engine Co Ltd
Application granted granted Critical
Publication of FR1221234A publication Critical patent/FR1221234A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
    • 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
    • F16L9/00—Rigid pipes
    • F16L9/18—Double-walled pipes; Multi-channel pipes or pipe assemblies
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Supports For Pipes And Cables (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR788437A 1958-03-05 1959-03-05 Ensembles de canalisations Expired FR1221234A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB7094/58A GB857345A (en) 1958-03-05 1958-03-05 Duct assemblies

Publications (1)

Publication Number Publication Date
FR1221234A true FR1221234A (fr) 1960-05-31

Family

ID=38461762

Family Applications (1)

Application Number Title Priority Date Filing Date
FR788437A Expired FR1221234A (fr) 1958-03-05 1959-03-05 Ensembles de canalisations

Country Status (5)

Country Link
US (1) US3053283A (fr)
CH (1) CH353940A (fr)
DE (1) DE1137276C2 (fr)
FR (1) FR1221234A (fr)
GB (1) GB857345A (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0202050A1 (fr) * 1985-04-29 1986-11-20 Avco Corporation Structure d'une paroi de chambre de combustion
EP0344877A1 (fr) * 1988-05-31 1989-12-06 General Electric Company Paroi thermique pour le carter d'une turbine à gaz
EP0397566A1 (fr) * 1989-05-11 1990-11-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Chemise de protection thermique pour canal de post-combustion ou de transition d'un turboréacteur
EP0576698A1 (fr) * 1992-06-29 1994-01-05 Asea Brown Boveri Ag Section de chambre de combustion refroidi par connexion

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3779282A (en) * 1971-11-08 1973-12-18 Boeing Co Annulus inverting valve
US4615359A (en) * 1982-08-30 1986-10-07 Affa Stephen N Shroud for aircraft duct
US4747543A (en) * 1987-04-14 1988-05-31 United Technologies Corporation Nozzle flap cooling liner
FR2622253B1 (fr) * 1987-10-21 1990-02-09 Snecma Canal de transition d'un ensemble d'ejection de turboreacteur
DE4104432C1 (fr) * 1991-02-14 1992-04-09 Erno Raumfahrttechnik Gmbh, 2800 Bremen, De
GB9127505D0 (en) * 1991-03-11 2013-12-25 Gen Electric Multi-hole film cooled afterburner combustor liner
DE4115403A1 (de) * 1991-05-10 1992-11-12 Mtu Muenchen Gmbh Duesenwand
US5669812A (en) * 1996-02-21 1997-09-23 Braden Manufacturing Exhaust gas diffuser interface
US7631481B2 (en) * 2004-12-01 2009-12-15 United Technologies Corporation Cooled duct for gas turbine engine
DE102008023052B4 (de) * 2008-05-09 2011-02-10 Eads Deutschland Gmbh Brennkammerwand bzw. Heißgaswand einer Brennkammer und Brennkammer mit einer Brennkammerwand
US20100116466A1 (en) * 2008-11-07 2010-05-13 Jerzy Hawranek Axial Heat Exchanger for Regulating the Temperature and Air Comfort in an Indoor Space
DE102009032045A1 (de) * 2009-07-07 2011-01-20 Elb-Form Gmbh Doppelwandiges Rohr, Verfahren zu seiner Herstellung und seine Verwendung
US9260191B2 (en) * 2011-08-26 2016-02-16 Hs Marston Aerospace Ltd. Heat exhanger apparatus including heat transfer surfaces
US9341377B2 (en) * 2012-12-06 2016-05-17 United Technologies Corporation Spherical collet for mounting a gas turbine engine liner
US20140238027A1 (en) * 2012-12-21 2014-08-28 United Technologies Corporation Thermally compliant dual wall liner for a gas turbine engine
BR112015016935B1 (pt) * 2013-01-15 2022-01-11 United Technologies Corporation Motor de turbina a gás, e, método para fornecer proteção contra fogo para uma unidade de potência auxiliar
GB201302125D0 (en) 2013-02-07 2013-03-20 Rolls Royce Plc A panel mounting arrangement
US20140223919A1 (en) * 2013-02-14 2014-08-14 United Technologies Corporation Flexible liner hanger
RU2529268C1 (ru) * 2013-04-11 2014-09-27 Открытое акционерное общество "Уфимское моторостроительное производственное объединение" ОАО "УМПО" Поворотное осесимметричное сопло турбореактивного двигателя
US9896970B2 (en) * 2014-11-14 2018-02-20 General Electric Company Method and system for sealing an annulus
EP3983646B1 (fr) * 2019-06-13 2023-09-06 Tata Steel Nederland Technology B.V. Segment de tube à double paroi et procédé de production dudit segment de tube

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US182370A (en) * 1876-09-19 Improvement in spark-arresters for stove-pipes
US566243A (en) * 1896-08-18 Max svagrovsky
US930012A (en) * 1907-10-18 1909-08-03 Matthaeus Woerner Construction of hollow bodies.
US976029A (en) * 1910-02-08 1910-11-15 Henry Birnbaum Sheet-metal pipe.
US2325616A (en) * 1942-11-30 1943-08-03 Landweber Louis Shroud ring
FR901719A (fr) * 1943-03-10 1945-08-03 Tuyaux en ciment d'amiante
US2475635A (en) * 1945-01-08 1949-07-12 Elmer C Parsons Multiple conduit
US2500501A (en) * 1946-09-12 1950-03-14 Kellogg M W Co Method of making heat exchangers
US2634759A (en) * 1949-07-27 1953-04-14 William Twickler & Sons Inc Insulated flue pipe
DE829835C (de) * 1950-02-21 1952-01-28 Rohrbau Mannesmann G M B H Rohrleitung
DE842734C (de) * 1950-10-18 1952-06-30 Rohrbau Mannesmann G M B H Rohrleitung fuer ueberhitzten Hochdruckdampf
CH308075A (de) * 1951-11-01 1955-06-30 Licentia Gmbh Rohrleitung für heisse Gase oder Dämpfe hohen Druckes, insbesondere für Luft- oder Gasturbinen.
US2717320A (en) * 1952-03-10 1955-09-06 Reliance Electric & Eng Co Heat exchanger
US2714395A (en) * 1952-05-24 1955-08-02 Epstein Saul Inner spacer for double wall vent pipe
US2706496A (en) * 1952-05-29 1955-04-19 Texas Co Concentric pipe insulator and spacer
US2785878A (en) * 1953-09-16 1957-03-19 Earl W Conrad Porous walled conduit for fluid cooling
US2795108A (en) * 1953-10-07 1957-06-11 Westinghouse Electric Corp Combustion apparatus
US2759491A (en) * 1953-10-27 1956-08-21 Nat Clay Pipe Res Corp Coaxial conduit construction

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0202050A1 (fr) * 1985-04-29 1986-11-20 Avco Corporation Structure d'une paroi de chambre de combustion
EP0344877A1 (fr) * 1988-05-31 1989-12-06 General Electric Company Paroi thermique pour le carter d'une turbine à gaz
EP0397566A1 (fr) * 1989-05-11 1990-11-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Chemise de protection thermique pour canal de post-combustion ou de transition d'un turboréacteur
FR2646880A1 (fr) * 1989-05-11 1990-11-16 Snecma Chemise de protection thermique pour canal de post-combustion ou de transition d'un turboreacteur
US5069034A (en) * 1989-05-11 1991-12-03 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Heat protective lining for an afterburner or transition duct of a turbojet engine
EP0576698A1 (fr) * 1992-06-29 1994-01-05 Asea Brown Boveri Ag Section de chambre de combustion refroidi par connexion

Also Published As

Publication number Publication date
GB857345A (en) 1960-12-29
US3053283A (en) 1962-09-11
CH353940A (fr) 1961-04-30
DE1137276C2 (de) 1963-04-11
DE1137276B (de) 1962-09-27

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