Inventor
Victor Hugo Silva Correia
Inventor
Milton Mills, NH, US
Overview
Patents· 59 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 turbines29%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants23%
Y02TClimate change mitigation technologies related to transportation19%
F02CGas-turbine plants8%
B01DSeparation3%
F16JPistons2%
Y10TTechnical subjects covered by former us classification2%
B04CApparatus using free vortex flow, e.g. cyclones2%
F04DNon-positive-displacement pumps2%
F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers2%
PatentTitleYear
11,067,277Component assembly for a gas turbine engine202111,033,845Turbine engine and particle separators therefore202110,975,731Turbine engine, components, and methods of cooling same202110,822,974Turbine nozzle with CMC aft band202010,822,957Fillet optimization for turbine airfoil202010,815,806Engine component with insert202010,731,509Compliant seal component and associated method202010,704,425Assembly for a gas turbine engine202010,697,313Turbine engine component with an insert202010,590,781Turbine engine assembly with a component having a leading edge trough202010,570,760Turbine nozzle with CMC aft band202010,557,362Method and system for a pressure activated cap seal202010,487,677Turbine component having a seal slot and additive manufacturing process for making same201910,436,038Turbine engine with an airfoil having a tip shelf outlet201910,392,950Turbine band anti-chording flanges201910,392,967Compliant seal component and associated method201910,301,953Turbine nozzle with CMC aft Band201910,286,407Inertial separator201910,267,179Dirt extraction apparatus for a gas turbine engine201910,267,161Gas turbine engine with fillet film holes201910,245,539Virtual impactor filter assembly and method201910,227,876Fillet optimization for turbine airfoil201910,221,693Trench cooling of airfoil structures201910,167,725Engine component for a turbine engine201910,030,538Gas turbine engine with a vane having a cooling air turning nozzle20189,845,691Turbine nozzle outer band and airfoil cooling apparatus20179,810,079'Cyclonic dirt separating turbine accelerator'20179,810,086'Asymmetric radial spline seal for a gas turbine engine'20179,488,110'Device and method for preventing leakage of air between multiple turbine components'20168,790,084'Airfoil and method of fabricating the same'20148,591,189'Bifeed serpentine cooled blade'20138,296,945'Method for repairing a turbine nozzle segment'20128,281,604'Divergent turbine nozzle'20128,235,652'Turbine nozzle segment'20128,172,522'Method and system for supporting stator components'20128,092,163'Turbine stator mount'20128,079,807'Mounting apparatus for low-ductility turbine shroud'20117,857,587'Turbine blades and turbine blade cooling systems and methods'20107,121,793'Undercut flange turbine nozzle'20066,742,987'Cradle mounted turbine nozzle'20046,733,229'Insert metering plates for gas turbine nozzles'20046,413,042'Stationary flowpath components for gas turbine engines'20026,394,749'Apparatus and methods for relieving thermally induced stresses in inner and outer bands of thermally cooled turbine nozzle stages'20026,290,459'Stationary flowpath components for gas turbine engines'20016,231,307'Impingement cooled airfoil tip'20016,164,914'Cool tip blade'20006,135,715'Tip insulated airfoil'20005,823,741'Cooling joint connection for abutting segments in a gas turbine engine'19985,743,708'Turbine stator vane segments having combined air and steam cooling circuits'19985,713,722'Turbine nozzle and related casting method for optimal fillet wall thickness control'19985,662,160'Turbine nozzle and related casting method for optimal fillet wall thickness control'19975,634,766'Turbine stator vane segments having combined air and steam cooling circuits'19975,509,669'Gas-path leakage seal for a gas turbine'19965,480,281'Impingement cooling apparatus for turbine shrouds having ducts of increasing cross-sectional area in the direction of post-impingement cooling flow'19965,391,052'Impingement cooling and cooling medium retrieval system for turbine shrouds and methods of operation'19955,358,374'Turbine nozzle backflow inhibitor'19945,332,360'Stator vane having reinforced braze joint'19945,248,240'Turbine stator vane assembly'19935,176,496'Mounting arrangements for turbine nozzles'1993Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
1993–2021Patents assigned to GEN ELECTRIC (59)· patent assignee history
1993Based in Cincinnati, OH, US· patent location history
1994–1996Based in Scotia, NY, US· patent location history
1996–1998Based in New Lebanon, NY, US· patent location history
2000–2021Based in Milton Mills, NH, US· patent location history
2011–2012Patents assigned to SHAPIRO JASON DAVID (3)· patent assignee history
2012–2017Patents assigned to CORREIA VICTOR HUGO SILVA (8)· patent assignee history
2012Patents assigned to BROOMER MARK (3)· patent assignee history
2012–2014Patents assigned to MANNING ROBERT FRANCIS (3)· patent assignee history
2019Based in Lynn, MA, US· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| GEN ELECTRIC | 59 | 1993–2021 |
| CORREIA VICTOR HUGO SILVAself | 8 | 2012–2017 |
| BROOMER MARK | 3 | 2012 |
| MANNING ROBERT FRANCIS | 3 | 2012–2014 |
| SHAPIRO JASON DAVID | 3 | 2011–2012 |
Locations
| Location | Patents | Span |
|---|---|---|
| Milton Mills, NH, US | 43 | 2000–2021 |
| New Lebanon, New York, US | 5 | 1996–1998 |
| Scotia, New York, US | 4 | 1994–1996 |
| Lynn, Massachusetts, US | 3 | 2019 |
| Cincinnati, OH, US | 2 | 1993 |