FR1458204A - Improvements to fixing devices for the thermal protection jacket of a reactor post-combustion chamber - Google Patents

Improvements to fixing devices for the thermal protection jacket of a reactor post-combustion chamber

Info

Publication number
FR1458204A
FR1458204A FR20525A FR20525A FR1458204A FR 1458204 A FR1458204 A FR 1458204A FR 20525 A FR20525 A FR 20525A FR 20525 A FR20525 A FR 20525A FR 1458204 A FR1458204 A FR 1458204A
Authority
FR
France
Prior art keywords
combustion chamber
fixing devices
thermal protection
protection jacket
reactor post
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
FR20525A
Other languages
French (fr)
Inventor
Andre Alphonse Mederic Camboul
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR20525A priority Critical patent/FR1458204A/en
Application granted granted Critical
Publication of FR1458204A publication Critical patent/FR1458204A/en
Priority to GB26047/66A priority patent/GB1118257A/en
Expired 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
FR20525A 1965-06-11 1965-06-11 Improvements to fixing devices for the thermal protection jacket of a reactor post-combustion chamber Expired FR1458204A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR20525A FR1458204A (en) 1965-06-11 1965-06-11 Improvements to fixing devices for the thermal protection jacket of a reactor post-combustion chamber
GB26047/66A GB1118257A (en) 1965-06-11 1966-06-10 Improvements in arrangements for fixing thermal protection jackets in jet engine reheat chambers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR20525A FR1458204A (en) 1965-06-11 1965-06-11 Improvements to fixing devices for the thermal protection jacket of a reactor post-combustion chamber

Publications (1)

Publication Number Publication Date
FR1458204A true FR1458204A (en) 1966-03-04

Family

ID=8581741

Family Applications (1)

Application Number Title Priority Date Filing Date
FR20525A Expired FR1458204A (en) 1965-06-11 1965-06-11 Improvements to fixing devices for the thermal protection jacket of a reactor post-combustion chamber

Country Status (1)

Country Link
FR (1) FR1458204A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0080404A1 (en) * 1981-11-19 1983-06-01 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Assembly of two joined rotationally symmetrical objects made of materials with differing co-efficients of dilatation
EP0397566A1 (en) * 1989-05-11 1990-11-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Heat insulation structure for an afterburner liner or turbine transition piece

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0080404A1 (en) * 1981-11-19 1983-06-01 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Assembly of two joined rotationally symmetrical objects made of materials with differing co-efficients of dilatation
US4452038A (en) * 1981-11-19 1984-06-05 S.N.E.C.M.A. System for attaching two rotating parts made of materials having different expansion coefficients
EP0397566A1 (en) * 1989-05-11 1990-11-14 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Heat insulation structure for an afterburner liner or turbine transition piece
FR2646880A1 (en) * 1989-05-11 1990-11-16 Snecma THERMAL PROTECTION SHIRT FOR POST-COMBUSTION CHANNEL OR TRANSITION OF TURBOREACTOR
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

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