AT397512T

Hollow fan blade detail half, hollow fan blade for a gas turbine engine and corresponding manufacturing method

Abstract

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Term

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9 members in 5 offices

This recordMember, by publication datePriority claim

Priority claims1

Priority claims
DocumentOfficeKindDate
76534704United States of AmericaA

Members9

Family members, oldest first
DocumentOfficeKind
EP1557528A2European Patent Office (EPO)A2
US2005163618A1United States of AmericaA1
JP2005207424AJapanA
EP1557528A3European Patent Office (EPO)A3
US6994524B2United States of AmericaB2
EP1557528B1European Patent Office (EPO)B1
AT397512TThis recordAustriaT
DE602005007272D1GermanyD1
JP4125725B2JapanB2