Vincent Pomme
Inventor
Stats
- 7 US patents issued
- 8 US Applications filed
- most recent filing
This is official USPTO record data
Details
- 7 US Patents Issued
- 8 US Applications Filed
- 44 Total Citation Count
- Nov 6, 2015 Most Recent Filing
- Apr 25, 1996 Earliest Filing
Work History
| Patent Owner | Applications Filed | Year |
|---|---|---|
| Valeo Climatisation | 3
1 1 | 1996
1998 2000 |
| AIRBUS HELICOPTERS | 2
2 1 | 2013
2014 2015 |
Inventor Addresses
| Address | Duration |
|---|---|
| Les Pennes Mirabeau, FR | Dec 26, 13 - Oct 18, 16 |
| Montigny Le Bretonneux, FR | Dec 02, 97 - Dec 02, 97 |
| Montigny le Bretonneux, FR | Mar 03, 98 - Jul 30, 02 |
| Virtolles, FR | Aug 14, 18 - Aug 14, 18 |
| Vitrolles, FR | Dec 18, 14 - Apr 18, 17 |
Technology Profile
| Technology | Matters | |
|---|---|---|
| B60H: | ARRANGEMENTS OR ADAPTATIONS OF HEATING, COOLING, VENTILATING, OR OTHER AIR-TREATING DEVICES SPECIALLY FOR PASSENGER OR GOODS SPACES OF VEHICLES | 2 |
| B64D: | EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS | 2 |
| F02C: | GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS | 1 |
Patents / Publication
| Patents / Publication # | Year of Publication / Issued | Title | Citations |
|---|---|---|---|
| 10047675 | 2018 | Power plant having a two-stage cooler device for cooling the admission air for a turboshaft engine | 0 |
| 9623723 | 2017 | System for heating the cabin of an aircraft provided with an annular heat exchanger around the exhaust nozzle | 6 |
| 9469407 | 2016 | Fluid temperature control installation for rotorcraft, associating a system for cooling a power plant with a system for heating a cabin | 0 |
| 2016/0131,032 | 2016 | POWER PLANT HAVING A TWO-STAGE COOLER DEVICE FOR COOLING THE ADMISSION AIR FOR A TURBOSHAFT ENGINE | 4 |
| 2014/0367,476 | 2014 | SYSTEM FOR HEATING THE CABIN OF AN AIRCRAFT PROVIDED WITH AN ANNULAR HEAT EXCHANGER AROUND THE EXHAUSE NOZZLE | 1 |
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