Inventor
Wesley D Brown
Inventor
Jupiter, FL, US
Overview
Patents· 28 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 turbines30%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants17%
F02CGas-turbine plants12%
Y10TTechnical subjects covered by former us classification11%
Y02TClimate change mitigation technologies related to transportation9%
F16CShafts5%
F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers5%
Y10STechnical subjects covered by former uspc cross-reference art collections [xracs] and digests5%
F04DNon-positive-displacement pumps2%
B22CFoundry moulding1%
PatentTitleYear
10,024,170Integrally bladed rotor with bore entry cooling holes20189,394,799'Air riding seal for a turbine'20168,794,907'Multiple staged compressor with last stage airfoil cooling'20148,475,112'Multiple staged compressor with last stage airfoil cooling'20138,382,439'Process of forming a high temperature turbine rotor blade'20138,336,206'Process of forming a high temperature turbine rotor blade'20128,307,661'Small gas turbine engine with multiple burn zones'20128,196,407'Small gas turbine engine with multiple burn zones'20128,070,450'High temperature turbine rotor blade'20118,052,391'High temperature turbine rotor blade'20118,015,705'Spar and shell blade with segmented shell'20118,007,242'High temperature turbine rotor blade'20117,997,057'Gas turbine engine with an air cooled bearing'20117,942,009'Gas turbine engine with an air cooled bearing'20117,874,804'Turbine blade with detached platform'20117,762,781'Composite blade and platform assembly'20107,758,314'Tungsten shell for a spar and shell turbine vane'20107,748,209'Small single use gas turbine engine with oil-less bearing arrangement'20107,670,116'Turbine vane with spar and shell construction'20107,568,343'Small gas turbine engine with multiple burn zones'20097,562,519'Gas turbine engine with an air cooled bearing'20097,080,971'Cooled turbine spar shell blade construction'20066,983,606'Integrated gas turbine compressor-rotary fuel injector'20066,413,044'Blade cooling in gas turbine'20025,403,156'Integral meter plate for turbine blade and method'19955,243,759'Method of casting to control the cooling air flow rate of the airfoil trailing edge'19934,872,810'Turbine rotor retention system'19894,820,122'Dirt removal means for air cooled blades'1989Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
1989–1995Patents assigned to UNITED TECHNOLOGIES CORP (4)· patent assignee history
1989–2018Based in Jupiter, FL, US· patent location history
2006–2018Patents assigned to FLORIDA TURBINE TECH INC (22)· patent assignee history
2011–2018Patents assigned to BROWN WESLEY D (8)· patent assignee history
2012Patents assigned to GARCIE ANGEL M (2)· patent assignee history
2012Patents assigned to HARRIS MARK M (2)· patent assignee history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| FLORIDA TURBINE TECH INC | 22 | 2006–2018 |
| BROWN WESLEY Dself | 8 | 2011–2018 |
| UNITED TECHNOLOGIES CORP | 4 | 1989–1995 |
| GARCIE ANGEL M | 2 | 2012 |
| HARRIS MARK M | 2 | 2012 |
Locations
| Location | Patents | Span |
|---|---|---|
| Jupiter, Florida, US | 28 | 1989–2018 |