Inventor
Alain Marc Lucien Bromann
Inventor
Vulaines sur Seine, FR
Overview
Patents· 18 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 turbines33%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants27%
F04DNon-positive-displacement pumps18%
Y02TClimate change mitigation technologies related to transportation11%
F02CGas-turbine plants5%
F02KJet-propulsion plants2%
F16CShafts2%
Y10TTechnical subjects covered by former us classification2%
PatentTitleYear
10,927,699Variable-pitch blade control ring for a turbomachine202110,648,359System for controlling variable-setting blades for a turbine engine202010,502,087Assembly for controlling variable pitch vanes in a turbine engine201910,385,721System for controlling variable pitch blades for a turbine engine201910,330,021System for controlling variable-pitch vanes for a turbine engine201910,100,842Cover of a turbomachine centrifugal compressor capable of being rigidly connected via the downstream side near to the upstream edge of same, and turbomachine comprising this cover201810,066,509Turbomachine part comprising a flange with a drainage device20189,926,944'Device for guiding variable pitch diffuser vanes of a turbine engine'20189,528,441'Aircraft turbofan comprising an intermediate ring with simplified downstream support'20169,212,564'Annular anti-wear shim for a turbomachine'20157,677,866'Device for adjusting the centring of a turbo-engine pivoting vane control synchronization ring'20107,458,771'Retaining of centering keys for rings under variable angle stator vanes in a gas turbine engine'20087,290,988'Device for blocking a ring for axially retaining a blade, associated rotor disk and retaining ring, and rotor and aircraft engine comprising them'20077,244,098'Device for adjusting the centering of a ring for synchronizing the control of pivoting vanes in a turbomachine'20077,214,030'Guide system for the outer pivot of a variable stator vane, for a turbojet stator'20077,112,040'Method of guiding a blade having a variable pitch angle'20066,200,091'High-pressure turbine stator ring for a turbine engine'20015,288,206'Turbo aero engine equipped with means facilitating adjustment of plays of the stator and between the stator and rotor'1994Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
1994–2018Patents assigned to SNECMA (10)· patent assignee history
1994–2001Based in Savigny le Temple, FR· patent location history
2006–2007Patents assigned to SNECMA MOTEURS (2)· patent assignee history
2006–2007Based in Neuilly sur Seine, FR· patent location history
2007–2019Based in Vulaines sur Seine, FR· patent location history
2018–2021Patents assigned to SAFRAN AIRCRAFT ENGINES (7)· patent assignee history
2018–2021Based in Moissy-Cramayel, FR· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| SNECMA | 10 | 1994–2018 |
| SAFRAN AIRCRAFT ENGINES | 7 | 2018–2021 |
| SNECMA MOTEURS | 2 | 2006–2007 |
Locations
| Location | Patents | Span |
|---|---|---|
| Vulaines sur Seine, FR | 9 | 2007–2019 |
| Moissy-Cramayel, FR | 5 | 2018–2021 |
| Neuilly sur Seine, FR | 2 | 2006–2007 |
| Savigny le Temple, FR | 2 | 1994–2001 |