Inventor
TOWNSEND PETER
CA37 patents
⚠️ This page may combine multiple inventors who share the name “TOWNSEND PETER”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.
PRATT & WHITNEY CANADA
28 patentsUS10378554B2Aug 13, 2019
Gas turbine engine with partial inlet vane
PRATT & WHITNEY CANADA30 citations94
US9726084B2Aug 8, 2017
Compressor bleed self-recirculating system
PRATT & WHITNEY CANADA23 citations94
US10837361B2Nov 17, 2020
Gas turbine engine inlet
PRATT & WHITNEY CANADA20 citations93
US10215194B2Feb 26, 2019
Mistuned fan
PRATT & WHITNEY CANADA20 citations93
US9303589B2Apr 5, 2016
Low hub-to-tip ratio fan for a turbofan gas turbine engine
PRATT & WHITNEY CANADA16 citations92
US11118601B2Sep 14, 2021
Gas turbine engine with partial inlet vane
PRATT & WHITNEY CANADA9 citations86
US10690146B2Jun 23, 2020
Turbofan nacelle assembly with flow disruptor
PRATT & WHITNEY CANADA18 citations86
US10107307B2Oct 23, 2018
Gas turbine engine rotor casing treatment
PRATT & WHITNEY CANADA7 citations84
US10865806B2Dec 15, 2020
Mistuned rotor for gas turbine engine
PRATT & WHITNEY CANADA10 citations83
US11041388B2Jun 22, 2021
Blade cutback distribution in rotor for noise reduction
PRATT & WHITNEY CANADA6 citations82
US10865807B2Dec 15, 2020
Mistuned fan
PRATT & WHITNEY CANADA6 citations82
US11033992B2Jun 15, 2021
Double row compressor stators
PRATT & WHITNEY CANADA5 citations73
US9810157B2Nov 7, 2017
Compressor shroud reverse bleed holes
PRATT & WHITNEY CANADA4 citations73
US10837459B2Nov 17, 2020
Mistuned fan for gas turbine engine
PRATT & WHITNEY CANADA2 citations72
US10408231B2Sep 10, 2019
Rotor with non-uniform blade tip clearance
PRATT & WHITNEY CANADA2 citations72
US10408223B2Sep 10, 2019
Low hub-to-tip ratio fan for a turbofan gas turbine engine
PRATT & WHITNEY CANADA1 citations72
US9803652B2Oct 31, 2017
Centrifugal compressor diffuser and method for controlling same
PRATT & WHITNEY CANADA6 citations71
US9879540B2Jan 30, 2018
Compressor stator with contoured endwall
PRATT & WHITNEY CANADA5 citations70
US10487847B2Nov 26, 2019
Gas turbine engine blade casing
PRATT & WHITNEY CANADA2 citations69
US9709070B2Jul 18, 2017
Low hub-to-tip ratio fan for a turbofan gas turbine engine
PRATT & WHITNEY CANADA2 citations64
US11338400B2May 24, 2022
Double row compressor stators
PRATT & WHITNEY CANADA0 citations62
US11136993B2Oct 5, 2021
Diffuser pipe with asymmetry
PRATT & WHITNEY CANADA0 citations62
US11421536B2Aug 23, 2022
Blade cutback distribution in rotor for noise reduction
PRATT & WHITNEY CANADA0 citations60
US11353038B2Jun 7, 2022
Compressor rotor for supersonic flutter and/or resonant stress mitigation
PRATT & WHITNEY CANADA0 citations60
US10670041B2Jun 2, 2020
Compressor rotor for supersonic flutter and/or resonant stress mitigation
PRATT & WHITNEY CANADA1 citations60
US10781705B2Sep 22, 2020
Inter-compressor flow divider profiling
PRATT & WHITNEY CANADA1 citations59
US10718216B2Jul 21, 2020
Airfoil for gas turbine engine
PRATT & WHITNEY CANADA1 citations57
US10724540B2Jul 28, 2020
Stator for a gas turbine engine fan
PRATT & WHITNEY CANADA0 citations37