CA741969A - Means for supporting the downstream end of a combustion chamber in a gas turbine engine - Google Patents

Means for supporting the downstream end of a combustion chamber in a gas turbine engine

Info

Publication number
CA741969A
CA741969A CA741969A CA741969DA CA741969A CA 741969 A CA741969 A CA 741969A CA 741969 A CA741969 A CA 741969A CA 741969D A CA741969D A CA 741969DA CA 741969 A CA741969 A CA 741969A
Authority
CA
Canada
Prior art keywords
supporting
combustion chamber
gas turbine
turbine engine
downstream end
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
CA741969A
Inventor
Ormerod Alan
S. Kay Arthur
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.)
ZF International UK Ltd
Original Assignee
Joseph Lucas Industries Ltd
Publication date
Application granted granted Critical
Publication of CA741969A publication Critical patent/CA741969A/en
Expired legal-status Critical Current

Links

CA741969A Means for supporting the downstream end of a combustion chamber in a gas turbine engine Expired CA741969A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA741969T

Publications (1)

Publication Number Publication Date
CA741969A true CA741969A (en) 1966-09-06

Family

ID=36171146

Family Applications (1)

Application Number Title Priority Date Filing Date
CA741969A Expired CA741969A (en) Means for supporting the downstream end of a combustion chamber in a gas turbine engine

Country Status (1)

Country Link
CA (1) CA741969A (en)

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