AU1566A - Chemical process - Google Patents

Chemical process

Info

Publication number
AU1566A
AU1566A AU15/66A AU1566A AU1566A AU 1566 A AU1566 A AU 1566A AU 15/66 A AU15/66 A AU 15/66A AU 1566 A AU1566 A AU 1566A AU 1566 A AU1566 A AU 1566A
Authority
AU
Australia
Prior art keywords
chemical process
chemical
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
AU15/66A
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 filed Critical
Publication of AU1566A publication Critical patent/AU1566A/en
Expired legal-status Critical Current

Links

AU15/66A 1965-01-05 1966-01-04 Chemical process Expired AU1566A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
USUS423,588 1965-01-05

Publications (1)

Publication Number Publication Date
AU1566A true AU1566A (en) 1967-07-06

Family

ID=

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4012172A (en) * 1975-09-10 1977-03-15 Avco Corporation Low noise blades for axial flow compressors
US4077741A (en) * 1975-05-19 1978-03-07 Westland Aircraft Limited Helicopter rotor blades
US4712980A (en) * 1985-05-09 1987-12-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Fairing for turbo-jet engine fan leading edge

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4077741A (en) * 1975-05-19 1978-03-07 Westland Aircraft Limited Helicopter rotor blades
US4012172A (en) * 1975-09-10 1977-03-15 Avco Corporation Low noise blades for axial flow compressors
US4712980A (en) * 1985-05-09 1987-12-15 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Fairing for turbo-jet engine fan leading edge

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