AU444257B2 - Prevention of hot corrosion in gas turbine engines - Google Patents

Prevention of hot corrosion in gas turbine engines

Info

Publication number
AU444257B2
AU444257B2 AU65391/69A AU6539169A AU444257B2 AU 444257 B2 AU444257 B2 AU 444257B2 AU 65391/69 A AU65391/69 A AU 65391/69A AU 6539169 A AU6539169 A AU 6539169A AU 444257 B2 AU444257 B2 AU 444257B2
Authority
AU
Australia
Prior art keywords
prevention
gas turbine
turbine engines
hot corrosion
corrosion
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
AU65391/69A
Other versions
AU6539169A (en
Inventor
SAMUEL BORNSTEIN and MICHAEL ANTHGF DECRESCENTE NORMAN
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
Application granted granted Critical
Publication of AU444257B2 publication Critical patent/AU444257B2/en
Publication of AU6539169A publication Critical patent/AU6539169A/en
Expired legal-status Critical Current

Links

AU65391/69A 1969-01-07 1969-12-17 Prevention of hot corrosion in gas turbine engines Expired AU444257B2 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
USUS789,578 1969-01-07

Publications (2)

Publication Number Publication Date
AU444257B2 true AU444257B2 (en) 1971-06-24
AU6539169A AU6539169A (en) 1971-06-24

Family

ID=

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