SE0201735D0

Turbine for aircraft industry, has component placed in housing and partially beside rotor with respect to direction of gas flow to impede any fragments that may come loose from rotor from penetrating housing in radial direction

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DocumentOfficeKind
SE0201735D0This recordSwedenD0
SE0201735LSwedenL
WO03104630A1World Intellectual Property Organization (WIPO)A1
AU2003238992A1AustraliaA1
SE525050C2SwedenC2
EP1514018A1European Patent Office (EPO)A1
JP2005529276AJapanA
RU2004139051ARussian FederationA
US2006233636A1United States of AmericaA1
US7140834B2United States of AmericaB2
EP1514018B1European Patent Office (EPO)B1
AT358769TAustriaT
DE60312984D1GermanyD1
ES2283780T3SpainT3
DE60312984T2GermanyT2
RU2343293C2Russian FederationC2
JP4364794B2JapanB2