Inventor
PESYNA KENNETH M
US33 patents
⚠️ This page may combine multiple inventors who share the name “PESYNA KENNETH M”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
ROLLS ROYCE NAM TECH INC
25 patentsUS9677501B2Jun 13, 2017
Three stream, variable area fixed aperture nozzle with pneumatic actuation
ROLLS ROYCE NAM TECH INC42 citations96
US10677166B2Jun 9, 2020
Heat exchanger for a gas turbine engine propulsion system
ROLLS ROYCE NAM TECH INC25 citations94
US9845768B2Dec 19, 2017
Three stream, variable area, vectorable nozzle
ROLLS ROYCE NAM TECH INC43 citations94
US9587561B2Mar 7, 2017
Heat exchanger integrated with a gas turbine engine and adaptive flow control
ROLLS ROYCE NAM TECH INC21 citations93
US9517843B2Dec 13, 2016
Generator for flight vehicle
ROLLS ROYCE NAM TECH INC9 citations84
US9464594B2Oct 11, 2016
Compact actuation system for flow nozzle
ROLLS ROYCE NAM TECH INC5 citations84
US10513981B2Dec 24, 2019
Heat exchanger assembly for a gas turbine engine propulsion system
ROLLS ROYCE NAM TECH INC10 citations83
US10494116B2Dec 3, 2019
Heat shield for signature suppression system
ROLLS ROYCE NAM TECH INC12 citations80
US10378477B2Aug 13, 2019
Nozzle for jet engines
ROLLS ROYCE NAM TECH INC4 citations73
US9840967B2Dec 12, 2017
Ram air thermal management system
ROLLS ROYCE NAM TECH INC6 citations73
US10767559B2Sep 8, 2020
Adaptive-area inertial particle separators
ROLLS ROYCE NAM TECH INC3 citations71
US10371093B2Aug 6, 2019
Aircraft nozzle with a variable nozzle area of a second flow path
ROLLS ROYCE NAM TECH INC6 citations71
US12065965B1Aug 20, 2024
Rotating detonation augmentors with adjustable throats for gas turbine engines
ROLLS ROYCE NAM TECH INC3 citations68
US11339745B1May 24, 2022
Dual flowpath exhaust for fuel cooling in a hypersonic propulsion system
ROLLS ROYCE NAM TECH INC2 citations65
US10718229B2Jul 21, 2020
Infrared suppression system in a gas turbine engine
ROLLS ROYCE NAM TECH INC6 citations65
US10544755B2Jan 28, 2020
Variable infrared suppression system in a gas turbine engine
ROLLS ROYCE NAM TECH INC1 citations61
US12460601B2Nov 4, 2025
Plug nozzle and thrust reverser for high mach gas turbine engines
ROLLS ROYCE NAM TECH INC0 citations59
US12228096B1Feb 18, 2025
Plug nozzle and thrust reverser for high mach gas turbine engines
ROLLS ROYCE NAM TECH INC0 citations59
US10974840B2Apr 13, 2021
Heat shield for signature suppression system
ROLLS ROYCE NAM TECH INC0 citations59
US12421914B2Sep 23, 2025
Compact infrared suppressors with ring vanes for gas turbine engines
ROLLS ROYCE NAM TECH INC0 citations58
US12180910B1Dec 31, 2024
Compact infrared suppressors with ring vanes for gas turbine engines
ROLLS ROYCE NAM TECH INC0 citations58
US10730636B2Aug 4, 2020
Integrated aircraft cooling system
ROLLS ROYCE NAM TECH INC0 citations52
US12025074B1Jul 2, 2024
Plug nozzle for high mach gas turbine engines
ROLLS ROYCE NAM TECH INC0 citations48
US11891964B1Feb 6, 2024
Method of manufacture of plug nozzle with thrust reverser
ROLLS ROYCE NAM TECH INC0 citations48
US11339744B1May 24, 2022
Pressure equalization in a dual flow path exhaust of a hypersonic propulsion system
ROLLS ROYCE NAM TECH INC0 citations44