Inventor · disambiguated record
Zhengxiang Pu
Also filed as: PU ZHENGXIANG
5 granted patents·2 pending applications·70 citations·filing 2006–2015
79Inventor score
Top patents by PatentIndex Score
7 records- 0192US9840930B2Internal cooling system with insert forming nearwall cooling channels in midchord cooling cavities of a gas turbine airfoilSIEMENS AG·Filed 2014·Granted Dec 12, 2017·25 cites·14 claims
- 0285US7686575B2Inner ring with independent thermal expansion for mounting gas turbine flow path componentsSIEMENS ENERGY INC·Filed 2006·Granted Mar 30, 2010·30 cites·7 claims
- 0383US9863256B2Internal cooling system with insert forming nearwall cooling channels in an aft cooling cavity of an airfoil usable in a gas turbine engineSIEMENS AG·Filed 2014·Granted Jan 9, 2018·9 cites·12 claims
- 0478US9109608B2Compressor airfoil tip clearance optimization systemLITTLE DAVID A·Filed 2011·Granted Aug 18, 2015·5 cites·14 claims
- 0552US10697306B2Gas turbine airfoil including integrated leading edge and tip cooling fluid passage and core structure used for forming such an airfoilSIEMENS AG·Filed 2014·Granted Jun 30, 2020·1 cites·5 claims
- 0634US2009014964A1Angled honeycomb seal between turbine rotors and turbine stators in a turbine engineSIEMENS POWER GENERATION INC·Filed 2007·Application pending·0 cites
- 0734US2018045059A1Internal cooling system with insert forming nearwall cooling channels in an aft cooling cavity of a gas turbine airfoil including heat dissipating ribsSIEMENS AG·Filed 2015·Application pending·0 cites
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