FR2038152A1 - High temperature wall structure - Google Patents

High temperature wall structure

Info

Publication number
FR2038152A1
FR2038152A1 FR7011364A FR7011364A FR2038152A1 FR 2038152 A1 FR2038152 A1 FR 2038152A1 FR 7011364 A FR7011364 A FR 7011364A FR 7011364 A FR7011364 A FR 7011364A FR 2038152 A1 FR2038152 A1 FR 2038152A1
Authority
FR
France
Prior art keywords
wall structure
pref
high temperature
channels
temperature wall
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.)
Withdrawn
Application number
FR7011364A
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of FR2038152A1 publication Critical patent/FR2038152A1/fr
Withdrawn legal-status Critical Current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
    • F23R3/005—Combined with pressure or heat exchangers
    • 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
    • F01D25/08—Cooling; Heating; Heat-insulation
    • 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; Infra-red radiation suppressors
    • 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
FR7011364A 1969-04-02 1970-03-26 High temperature wall structure Withdrawn FR2038152A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US81260769A 1969-04-02 1969-04-02

Publications (1)

Publication Number Publication Date
FR2038152A1 true FR2038152A1 (en) 1971-01-08

Family

ID=25210105

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7011364A Withdrawn FR2038152A1 (en) 1969-04-02 1970-03-26 High temperature wall structure

Country Status (6)

Country Link
AU (1) AU1230370A (fr)
BE (1) BE748069A (fr)
DE (1) DE2012947A1 (fr)
FR (1) FR2038152A1 (fr)
IL (1) IL33995A0 (fr)
NL (1) NL7004576A (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2478259A1 (fr) * 1980-03-17 1981-09-18 Snecma Element metallique allege etanche de construction mecanique
EP0273073A1 (fr) * 1986-12-30 1988-07-06 Stirling Engine Associates Echangeur thermique
FR2640321A1 (fr) * 1988-12-14 1990-06-15 Gen Electric Dispositif de controle de la deformation thermique d'une tuyere d'echappement
EP0801210A2 (fr) * 1996-04-10 1997-10-15 General Electric Company Refroidissement pour paroi de chambre de combustion de turbine à gaz
EP0816010A2 (fr) * 1996-06-24 1998-01-07 General Electric Company Procédé de fabrication des composants de turbine à paroi double à partir des ensembles préconsolidés

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4033381A (en) * 1975-06-27 1977-07-05 General Connectors Corporation Hot air duct
DE3003347A1 (de) * 1979-12-20 1981-06-25 BBC AG Brown, Boveri & Cie., Baden, Aargau Gekuehlte wand
US11619387B2 (en) * 2015-07-28 2023-04-04 Rolls-Royce Corporation Liner for a combustor of a gas turbine engine with metallic corrugated member

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2478259A1 (fr) * 1980-03-17 1981-09-18 Snecma Element metallique allege etanche de construction mecanique
EP0036356A1 (fr) * 1980-03-17 1981-09-23 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Elément métallique allégé étanche de construction mécanique
EP0273073A1 (fr) * 1986-12-30 1988-07-06 Stirling Engine Associates Echangeur thermique
FR2640321A1 (fr) * 1988-12-14 1990-06-15 Gen Electric Dispositif de controle de la deformation thermique d'une tuyere d'echappement
EP0801210A2 (fr) * 1996-04-10 1997-10-15 General Electric Company Refroidissement pour paroi de chambre de combustion de turbine à gaz
EP0801210A3 (fr) * 1996-04-10 1998-12-23 General Electric Company Refroidissement pour paroi de chambre de combustion de turbine à gaz
EP0816010A2 (fr) * 1996-06-24 1998-01-07 General Electric Company Procédé de fabrication des composants de turbine à paroi double à partir des ensembles préconsolidés
EP0816010A3 (fr) * 1996-06-24 1998-12-23 General Electric Company Procédé de fabrication des composants de turbine à paroi double à partir des ensembles préconsolidés
US5933699A (en) * 1996-06-24 1999-08-03 General Electric Company Method of making double-walled turbine components from pre-consolidated assemblies

Also Published As

Publication number Publication date
NL7004576A (fr) 1970-10-06
DE2012947A1 (de) 1970-11-05
IL33995A0 (en) 1970-05-21
AU1230370A (en) 1971-09-16
BE748069A (fr) 1970-08-31

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Legal Events

Date Code Title Description
ST Notification of lapse