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Robert Briggs
Robert Briggs
Aero-Thermal Engineering Manager, GE Aviation
Verified email at ge.com - Homepage
Title
Cited by
Cited by
Year
The effect of internal crossflow on the adiabatic effectiveness of compound angle film cooling holes
JW McClintic, SR Klavetter, JR Winka, JB Anderson, DG Bogard, JE Dees, ...
Journal of Turbomachinery 137 (7), 071006, 2015
682015
The effect of rib turbulators on film cooling effectiveness of round compound angle holes fed by an internal cross-flow
SR Klavetter, JW McClintic, DG Bogard, JE Dees, GM Laskowski, ...
Journal of Turbomachinery 138 (12), 121006, 2016
422016
Engine components with impingement cooling features
CW Stover, JM Rausch, S Atsuchi, GS Brainch, RD Briggs, RS Bunker, ...
US Patent 10,690,055, 2020
222020
Effects of crossflow in an internal-cooling channel on film cooling of a flat plate through compound-angle holes
ZT Stratton, TIP Shih, GM Laskowski, B Barr, R Briggs
Turbo Expo: Power for Land, Sea, and Air 56727, V05BT12A022, 2015
182015
Dust holes
KR Feldmann, RS Bunker, RD Briggs, JR Allen
US Patent App. 14/718,120, 2016
172016
Airfoil for a turbine engine
DG Konitzer, SR Bunker, RD Briggs
US Patent App. 15/138,624, 2017
142017
Turbine blade
ML Krumanaker, WN Dooley, SR Brassfield, DB Helmer, JC Bailey, ...
US Patent 10,174,620, 2019
132019
Engine component assembly
RS Bunker, RF Bergholz, JR Allen, RD Briggs, BA Pritchard Jr, ...
US Patent App. 14/989,290, 2017
132017
Near-hole thermal field measurements for round compound angle film cooling holes fed by cross-flow
JW McClintic, EK Wilkes, DG Bogard, JE Dees, GM Laskowski, R Briggs
Turbo Expo: Power for Land, Sea, and Air 56727, V05BT12A050, 2015
122015
Engine component assembly
RF Bergholz, JR Allen, RD Briggs, KR Feldmann, CW Stover, ZD Webster, ...
US Patent 11,280,215, 2022
112022
The effect of internal cross-flow on the adiabatic effectiveness of compound angle film cooling holes
JW McClintic, SR Klavetter, JB Anderson, JR Winka, DG Bogard, JE Dees, ...
Turbo Expo: Power for Land, Sea, and Air 45721, V05BT13A035, 2014
112014
Fastback turbulator structure and turbine nozzle incorporating same
RD Briggs, SM Pearson, JC Schilling
US Patent 8,408,872, 2013
112013
The Effect of Rib Turbulators on Film Cooling Effectiveness of Round Compound Angle Holes Fed by an Internal Cross-Flow
SR Klavetter, JW McClintic, DG Bogard, JE Dees, GM Laskowski, ...
Turbo Expo: Power for Land, Sea, and Air 56727, V05BT12A049, 2015
102015
Airfoil for a turbine engine
RS Bunker, RF Bergholz, RD Briggs, KR Feldmann
US Patent App. 14/882,551, 2016
92016
Fastback turbulator
RS Bunker, RD Briggs, SM Pearson
US Patent 10,563,514, 2020
82020
Windward cooled turbine nozzle
JC Schilling, RD Briggs, RE McRae Jr
US Patent 8,206,101, 2012
72012
Airfoil having impingement openings
RS Bunker, RD Briggs, TD Stone
US Patent 10,352,177, 2019
62019
Method and system for gas temperature measurement
G Wang, NV Nirmalan, RS Bunker, TG Wetzel, RM Zacharias, SD Wehe, ...
US Patent 9,528,880, 2016
62016
Method and system for gas temperature measurement
G Wang, NV Nirmalan, TG Wetzel, RS Bunker, RM Zacharias, SD Wehe, ...
US Patent 9,335,215, 2016
62016
Airfoil for a gas turbine engine
RS Bunker, RD Briggs, JR Allen, KR Feldmann
US Patent 10,450,874, 2019
42019
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