Bil; Eric Stephan

Patent Applications and Registrations

Patent applications and USPTO patent grants for Bil; Eric Stephan.The latest application filed is for "bleeding of air via the diffuser of a centrifugal compressor of a turbine engine".

Company Profile

0.11.6

Bil; Eric Stephan - Chartrettes FR
Bil; Eric Stephan - Combs la Ville FR

*profile and listings may contain filings by different individuals or companies with the same name. Review application materials to confirm ownership/assignment.

Patent Activity

Patent	Date
Gas turbine high pressure compressor fluid return and reinjection including an annular air bleeding manifold Grant 8,959,926 - Bil , et al. February 24, 2	2015-02-24
Bleeding of air via the diffuser of a centrifugal compressor of a turbine engine Grant 8,800,291 - Bil , et al. August 12, 2	2014-08-12
Bleeding Of Air Via The Diffuser Of A Centrifugal Compressor Of A Turbine Engine App 20110314828 - BIL; Eric Stephan ; et al.	2011-12-29
Air Manifold In A Turbomachine App 20110072829 - Bil; Eric Stephan ; et al.	2011-03-31
Bleed system for a low-pressure compressor of a turbomachine Grant 7,785,066 - Bil , et al. August 31, 2	2010-08-31
Compressor comprising a plurality of cells reconstituting an annular volume of separation of flows in a turbine engine Grant 7,618,232 - Bil , et al. November 17, 2	2009-11-17
Rotor blade for a compressor or a gas turbine Grant 7,399,163 - Bil , et al. July 15, 2	2008-07-15
Bleed System For A Low-pressure Compressor Of A Turbomachine App 20080063515 - BIL; Eric Stephan ; et al.	2008-03-13
Rotor blade for a compressor or a gas turbine App 20070292271 - Bil; Eric Stephan ; et al.	2007-12-20
Gas turbine or compressor blade App 20070243067 - Bil; Eric Stephan ; et al.	2007-10-18
Compressor Comprising A Plurality Of Cells Reconstituting An Annular Volume Of Separation Of Flows In A Turbine Engine App 20070039310 - Bil; Eric Stephan ; et al.	2007-02-22
System for ventilating a pair of juxtaposed vane platforms Grant 6,457,935 - Antunes , et al. October 1, 2	2002-10-01
Cooled turbine blade Grant 6,328,531 - Bariaud , et al. December 11, 2	2001-12-11
Method of reducing the gap between a liner and a turbine distributor of a turbojet engine Grant 6,163,959 - Arraitz , et al. December 26, 2	2000-12-26
Seal of stacked thin slabs that slide within reception slots Grant 5,997,247 - Arraitz , et al. December 7, 1	1999-12-07

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