CA453432A - Combustion chamber drain arrangement - Google Patents

Combustion chamber drain arrangement

Info

Publication number
CA453432A
CA453432A CA453432A CA453432DA CA453432A CA 453432 A CA453432 A CA 453432A CA 453432 A CA453432 A CA 453432A CA 453432D A CA453432D A CA 453432DA CA 453432 A CA453432 A CA 453432A
Authority
CA
Canada
Prior art keywords
combustion chamber
chamber drain
drain arrangement
arrangement
combustion
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
CA453432A
Other languages
French (fr)
Inventor
W. Kuyper William
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.)
General Electric Canada Co
Original Assignee
Canadian General Electric Co Ltd
Publication date
Application granted granted Critical
Publication of CA453432A publication Critical patent/CA453432A/en
Expired legal-status Critical Current

Links

CA453432A Combustion chamber drain arrangement Expired CA453432A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CA453432T

Publications (1)

Publication Number Publication Date
CA453432A true CA453432A (en) 1948-12-21

Family

ID=35571163

Family Applications (1)

Application Number Title Priority Date Filing Date
CA453432A Expired CA453432A (en) Combustion chamber drain arrangement

Country Status (1)

Country Link
CA (1) CA453432A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5285636A (en) * 1992-10-28 1994-02-15 General Electric Company Diagnostic drain mast for a gas turbine engine
FR2936274A1 (en) * 2008-09-25 2010-03-26 Ea Tech Fluid e.g. lubricant, collecting device for e.g. gas turbine engine of aircraft, has visual control unit for controlling maximum level of stored fluid, and permitting visualization of maximum height reached by fluid within tank

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5285636A (en) * 1992-10-28 1994-02-15 General Electric Company Diagnostic drain mast for a gas turbine engine
FR2936274A1 (en) * 2008-09-25 2010-03-26 Ea Tech Fluid e.g. lubricant, collecting device for e.g. gas turbine engine of aircraft, has visual control unit for controlling maximum level of stored fluid, and permitting visualization of maximum height reached by fluid within tank

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