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Inventor profile of:

Peter TOWNSEND

City:

Mississauga

Country:

Canada

Published Applications:

33

Last publication date:

2026-03-26

Top Assignees for applications by Peter TOWNSEND

The entities that hold a legal rights for patent applications filed by inventor TOWNSEND Peter:

Recent patent applications by TOWNSEND Peter

Peter TOWNSEND from Mississauga, CA has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2026-03-26
US20260085640A1
Mechanical engineering

DEVICES AND METHODS FOR GUIDING BLEED AIR IN A TURBOFAN ENGINE

 #2 | 2021-12-02
US20210372434A1
Mechanical engineering

GAS TURBINE ENGINE WITH PARTIAL INLET VANE

 #3 | 2021-09-23
US20210293149A1
Mechanical engineering

Blade cutback distribution in rotor for noise reduction

 #4 | 2021-08-26
US20210260706A1
Performing operations; transporting

Double row compressor stators

 #5 | 2020-12-17
US20200392968A1
Mechanical engineering

Compressor rotor for supersonic flutter and/or resonant stress mitigation

 #6 | 2020-10-08
US20200318649A1
Mechanical engineering

Diffuser pipe with asymmetry

 #7 | 2020-05-28
US20200165924A1
Mechanical engineering

Inter-compressor flow divider profiling

 #8 | 2020-04-09
US20200108473A1
Performing operations; transporting

Double row compressor stators

 #9 | 2019-05-16
US20190145431A1
Mechanical engineering

Mistuned fan

 #10 | 2019-04-11
US20190107119A1
Mechanical engineering

Gas turbine engine with partial inlet vane

 #11 | 2019-03-21
US20190085704A1
Mechanical engineering

Mistuned rotor for gas turbine engine

 #12 | 2019-03-14
US20190078589A1
Mechanical engineering

Rotor with non-uniform blade tip clearance

 #13 | 2019-03-07
US20190072034A1
Mechanical engineering

Gas turbine engine inlet

 #14 | 2018-07-05
US20180187697A1
Mechanical engineering

Turbofan nacelle assembly with flow disruptor

 #15 | 2018-06-07
US20180156235A1
Mechanical engineering

Stator for a gas turbine engine fan

 #16 | 2017-09-21
US20170268529A1
Mechanical engineering

Low hub-to-tip ratio fan for a turbofan gas turbine engine

 #17 | 2017-08-24
US20170241432A1
Mechanical engineering

Compressor rotor for supersonic flutter and/or resonant stress mitigation

 #18 | 2017-07-20
US20170204876A1
Mechanical engineering

Gas turbine engine blade casing

 #19 | 2017-06-22
US20170175776A1
Mechanical engineering

Mistuned fan

 #20 | 2016-10-20
US20160305285A1
Mechanical engineering

Gas turbine engine rotor casing treatment

 #21 | 2016-10-06
US20160290137A1
Mechanical engineering

Blade cutback distribution in rotor for noise reduction

 #22 | 2016-08-18
US20160238022A1
Mechanical engineering

Low hub-to-tip ratio fan for a turbofan gas turbine engine

 #23 | 2016-03-24
US20160084265A1
Mechanical engineering

Gas turbine engine with partial inlet vane

 #24 | 2016-03-24
US20160084162A1
Mechanical engineering

Gas turbine engine inlet

 #25 | 2015-08-13
US20150226232A1
Mechanical engineering

Centrifugal compressor diffuser and method for controlling same

 #26 | 2015-08-06
US20150219115A1
Mechanical engineering

Blade for axial compressor rotor

 #27 | 2014-12-04
US20140356159A1
Mechanical engineering

Low hub-to-tip ratio fan for a turbofan gas turbine engine

 #28 | 2014-09-25
US20140286746A1
Mechanical engineering

Compressor shroud reverse bleed holes

 #29 | 2014-09-18
US20140271158A1
Mechanical engineering

Compressor stator with contoured endwall

 #30 | 2014-09-18
US20140271108A1
Mechanical engineering

Compressor bleed self-recirculating system

 #31 | 2013-10-31
US20130287542A1
Mechanical engineering

Twisted variable inlet guide vane

 #32 | 2013-09-12
US20130236319A1
Mechanical engineering

Airfoil for gas turbine engine

 #33 | 2011-01-27
US20110016877A1
Mechanical engineering

Continuous slot in shroud
InventorID:

432599 ⎘