Inventor

Brandon W. Spangler

Inventor
Vernon, CT, US

Overview

124→
Patents
2005–2021
Patent span
Mechanical engineering
Primary field (CPC F)

Patents· 124 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 turbines28%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants27%
Y02TClimate change mitigation technologies related to transportation19%
F02CGas-turbine plants5%
F23RGenerating combustion products of high pressure or high velocity, e.g. gas-turbine combustion chambers4%
B22CFoundry moulding4%
B22DCasting of metals1%
B23PMetal-working not otherwise provided for1%
F04DNon-positive-displacement pumps1%
B22FWorking metallic powder1%
PatentTitleYear
11,131,212Gas turbine engine cooling component202111,111,857Hourglass airfoil cooling configuration202111,047,241Gas turbine engine airfoil having serpentine fed platform cooling passage202110,975,705Gas turbine engine airfoil with wishbone baffle cooling scheme202110,975,710Cooling circuit for gas turbine engine component202110,968,782Rotatable vanes202110,934,857Shell and spar airfoil202110,871,074Blade/vane cooling passages202010,821,501Coated casting core and manufacture methods202010,822,971Cooling hole for a gas turbine engine component202010,822,963Axial flow cooling scheme with castable structural rib for a gas turbine engine202010,815,794Baffle for components of gas turbine engines202010,808,552Trip strip configuration for gaspath component in a gas turbine engine202010,787,912Spiral cavities for gas turbine engine components202010,787,913Airfoil cooling circuit202010,774,657Baffle assembly for gas turbine engine components202010,774,655Gas turbine engine component with flow separating rib202010,753,216Sliding baffle inserts202010,746,033Gas turbine engine component202010,731,476Low turn loss baffle flow diverter202010,697,309Platform cover plates for gas turbine engine components202010,690,346Washer for combustor assembly202010,670,273Cooling configurations for combustor attachment features202010,670,274Cooling configurations for combustor attachment features202010,669,861Airfoil cooling structure202010,662,783Variable heat transfer collector baffle202010,648,351Gas turbine engine cooling component202010,641,129Support rail truss for gas turbine engines202010,641,103Trailing edge configuration with cast slots and drilled filmholes202010,619,489Airfoil having end wall contoured pedestals202010,612,390Trailing edge pressure and flow regulator202010,590,785Beveled coverplate202010,577,947Baffle insert for a gas turbine engine component202010,544,682Expansion seals for airfoils202010,526,917Platform lip impingement features202010,519,781Airfoil turn caps in gas turbine engines201910,494,939Air shredder insert201910,487,668Gas turbine engine airfoil with wishbone baffle cooling scheme201910,480,329Airfoil turn caps in gas turbine engines201910,465,528Airfoil turn caps in gas turbine engines201910,465,542Gas turbine engine turbine vane baffle and serpentine cooling passage201910,458,264Seal arrangement for turbine engine component201910,458,291Cover plate for a component of a gas turbine engine201910,458,252Cooling passages for a gas path component of a gas turbine engine201910,422,233Baffle insert for a gas turbine engine component and component with baffle insert201910,415,428Dual cavity baffle201910,378,364Modified structural truss for airfoils201910,364,680Gas turbine engine component having platform trench201910,358,978Gas turbine engine component having shaped pedestals201910,352,172Manufacturing method for a dual wall component201910,337,334Gas turbine engine component with a baffle insert201910,329,932Baffle inserts201910,329,933Flapper seal apparatus and system201910,323,525Gas turbine engine component cooling with resupply of cooling passage201910,316,698Dirt shield201910,309,239Cooling hole for a gas turbine engine component201910,301,964Baffle with flow augmentation feature201910,294,799Partial tip flag201910,294,823Dirt evacuation devices201910,280,761Three dimensional airfoil micro-core cooling chamber201910,280,762Multi-chamber platform cooling structures201910,280,841Baffle insert for a gas turbine engine component and method of cooling201910,273,808Low loss airflow port201910,267,163Airfoil turn caps in gas turbine engines201910,240,470Baffle for gas turbine engine vane201910,227,927Supply duct for cooling air from gas turbine compressor201910,184,341Airfoil baffle with wedge region201910,166,599Coated casting cores and manufacture methods201910,082,033Gas turbine blade with platform cooling201810,060,445Cooling hole patterned surfaces201810,053,996Sliding baffle inserts201810,054,055Serpentine platform cooling structures201810,047,629Multi-segment adjustable stator vane for a variable area vane arrangement201810,041,374Gas turbine engine component with platform cooling circuit201810,036,259Turbine blade having film cooling hole arrangement201810,012,106Enclosed baffle for a turbine engine component201810,012,092Low turn loss baffle flow diverter201810,006,295Gas turbine engine component having trip strips20189,988,913Using inserts to balance heat transfer and stress in high temperature alloys20189,988,934Gas turbine engines including channel-cooled hooks for retaining a part relative to an engine casing structure20189,982,543Partial cavity baffles for airfoils in gas turbine engines20189,957,813Gas turbine engine airfoil platform cooling passage and core20189,938,842Leakage air systems for turbomachines20189,845,686Overlapping herringbone filmhole patterned airfoil20179,845,693Overlapping herringbone filmhole patterned surfaces20179,810,084'Gas turbine engine turbine vane baffle and serpentine cooling passage'20179,803,489'Low loss baffled serpentine turns'20179,790,801'Gas turbine engine component having suction side cutback opening'20179,771,814'Tolerance resistance coverplates'20179,726,023'Airfoil support and cooling scheme'20179,500,099'Cover plate for a component of a gas turbine engine'20169,482,103'Intermediate additively manufactured component'20169,422,816'Airfoil with hybrid drilled and cutback trailing edge'20169,415,438'Method for forming single crystal parts using additive manufacturing and remelt'20169,376,920'Gas turbine engine cooling hole with circular exit geometry'20169,375,782'Regenerating an additively manufactured component'20169,364,888'Regenerating an additively manufactured component to cure defects and alter microstructure'20169,366,144'Trailing edge cooling'20169,353,631'Gas turbine engine airfoil baffle'20169,328,617'Trailing edge or tip flag antiflow separation'20169,322,279'Airfoil cooling arrangement'20169,273,566'Turbine engine variable area vane'20169,138,804'Core for a casting process'20159,115,597'Gas turbine engine turbine vane airfoil profile'20159,115,590'Gas turbine engine airfoil cooling circuit'20159,109,453'Airfoil cooling arrangement'20159,021,816'Gas turbine engine turbine vane platform core'20158,807,945'Cooling system for turbine airfoil including ice-cream-cone-shaped pedestals'20148,707,712'Gas turbine engine turbine vane airfoil profile'20148,360,716'Nozzle segment with reduced weight flange'20138,282,354'Reduced weight blade for a gas turbine engine'20128,257,045'Platforms with curved side edges and gas turbine engine systems involving such platforms'20128,240,981'Turbine airfoil with platform cooling'20128,240,987'Gas turbine engine systems involving baffle assemblies'20128,206,114'Gas turbine engine systems involving turbine blade platforms with cooling holes'20128,092,179'Blade tip cooling groove'20127,845,906'Dual cut-back trailing edge for airfoils'20107,837,441'Impingement skin core cooling for gas turbine engine blade'20107,766,615'Local indented trailing edge heat transfer devices'20107,712,316'Turbine blade with reverse cooling air film hole direction'20107,306,024'Refractory metal core wall thickness control'20077,270,170'Investment casting core methods'20077,174,945'Refractory metal core wall thickness control'20076,929,054'Investment casting cores'2005

Career & activity timeline

Assembled from patent assignee/location history and declaration credentials.

2005–2021Patents assigned to UNITED TECHNOLOGIES CORP (121)· patent assignee history
2005–2007Based in Rocky Hill, CT, US· patent location history
2007–2021Based in Vernon, CT, US· patent location history
2012–2019Patents assigned to SPANGLER BRANDON W (22)· patent assignee history
2012Patents assigned to PAAUWE CORNEIL S (3)· patent assignee history
2013–2016Patents assigned to BERGMAN RUSSELL J (7)· patent assignee history
2016Based in East Hartford, CT, US· patent location history
2020–2021Patents assigned to RAYTHEON TECH CORP (24)· patent assignee history

Inventor activity

Assignee and location history derived from the patent record.

Assignees
AssigneePatentsSpan
UNITED TECHNOLOGIES CORP1212005–2021
RAYTHEON TECH CORP242020–2021
SPANGLER BRANDON Wself222012–2019
BERGMAN RUSSELL J72013–2016
PAAUWE CORNEIL S32012
Locations
LocationPatentsSpan
Vernon, CT, US1212007–2021
Rocky Hill, CT, US22005–2007
East Hartford, CT, US12016