Inventor
Philippe Pierre Vincent Bouiller
Inventor
Samoreau, FR
Overview
Patents· 20 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
F01Dprimary
F01DNon-positive displacement machines or engines, e.g. steam turbines21%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants21%
F02CGas-turbine plants16%
F02KJet-propulsion plants11%
Y02TClimate change mitigation technologies related to transportation11%
F16CShafts5%
F04DNon-positive-displacement pumps3%
H02KDynamo-electric machines3%
B64DEquipment for fitting in or to aircraft2%
F16LPipes2%
PatentTitleYear
10,557,376Turbine engine unit for lubricating a bearing holder20209,765,645'Journal for a turbine engine comprising a ring for recovering a flow of lubricating oil with a plurality of lubricating oil discharge ports'20179,322,293'Turbojet venting pipe, method for mounting one such pipe and turbojet provided with one such pipe'20169,200,594'Gas turbine engine having fan blades of adjustable pitch with cyclic setting'20157,855,483'Turbomachine with integral generator/starter'20107,766,607'Device for ventilating turbine disks in a gas turbine engine'20107,619,331'Turbomachine with integral generator/starter'20097,555,894'Swivelling exhaust nozzle for an aircraft engine'20097,488,112'Assembly arrangement between a bearing inner race and a journal, race and journal suitable for such an arrangement, and turbomachine fitted therewith'20097,479,717'Turbomachine having a device for automatically detecting ferromagnetic particles in an oil enclosure'20097,390,167'Compressor with centripetal air takeoff'20087,372,175'Two-spool bypass turbojet with a rear electricity generator, and an air flow connection device and system'20087,224,082'Turbomachine including an integrated electricity generator'20077,097,415'Low-pressure turbine of a turbomachine'20067,040,082'Assistance and emergency drive for electrically-driven accessories'20066,276,126'Axisymmetric, directable and adjustable turbojet-engine exhaust nozzle'20016,179,225'Turbo jet engine exhaust nozzle with masked gas jet'20016,164,563'Converging exhaust nozzle fitted with translating cold flaps'20005,934,564'Variable geometry turbojet engine exhaust nozzle'19995,623,821'Turbojet equipped with a deicing system on the intake case'1997Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
1997–2017Patents assigned to SNECMA (17)· patent assignee history
1997–2017Based in Samoreau, FR· patent location history
2006Patents assigned to SNECMA MOTEURS (2)· patent assignee history
2009–2010Patents assigned to HISPANO SUIZA SA (2)· patent assignee history
2015–2016Patents assigned to BOUILLER PHILIPPE PIERRE VINCENT (2)· patent assignee history
2016Patents assigned to BRAULT MICHEL GILBERT ROLAND (1)· patent assignee history
2020Based in Moissy-Cramayel, FR· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| SNECMA | 17 | 1997–2017 |
| BOUILLER PHILIPPE PIERRE VINCENTself | 2 | 2015–2016 |
| HISPANO SUIZA SA | 2 | 2009–2010 |
| SNECMA MOTEURS | 2 | 2006 |
| BRAULT MICHEL GILBERT ROLAND | 1 | 2016 |
Locations
| Location | Patents | Span |
|---|---|---|
| Samoreau, FR | 19 | 1997–2017 |
| Moissy-Cramayel, FR | 1 | 2020 |