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Inventor profile of:

Paul STONE

City:

Guelph

Country:

Canada

Published Applications:

36

Last publication date:

2025-07-17

Top Assignees for applications by Paul STONE

The entities that hold a legal rights for patent applications filed by inventor STONE Paul:

Recent patent applications by STONE Paul

Paul STONE from Guelph, CA has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2025-07-17
US20250230757A1
Mechanical engineering

TEST ROTOR BLADE FOR AN AIRCRAFT ENGINE BLADE-OFF TEST

 #2 | 2025-02-27
US20250067195A1
Mechanical engineering

Test rotor blade for an aircraft engine blade-off test

 #3 | 2024-12-24
US18238319
Mechanical engineering

Test rotor blade for an aircraft engine blade-off test

 #4 | 2024-03-26
US17971211
Mechanical engineering

Method and integrally bladed rotor for blade off testing

 #5 | 2023-12-07
US20230392503A1
Mechanical engineering

Airfoil ribs for rotor blades

 #6 | 2023-11-02
US20230349297A1
Mechanical engineering

METHOD OF MANUFACTURING A MISTUNED ROTOR

 #7 | 2023-02-09
US20230043965A1
Mechanical engineering

Integrated bladed rotor

 #8 | 2021-09-09
US20210277826A1
Mechanical engineering

Fan blade anti-icing concept

 #9 | 2021-04-29
US20210123383A1
Mechanical engineering

Fan blade anti-icing concept

 #10 | 2021-04-22
US20210115795A1
Mechanical engineering

Method for fan blade heating using coanda effect

 #11 | 2020-12-17
US20200392968A1
Mechanical engineering

Compressor rotor for supersonic flutter and/or resonant stress mitigation

 #12 | 2020-06-25
US20200200013A1
Mechanical engineering

Gas turbine engine rotor balancing

 #13 | 2020-01-16
US20200018176A1
Mechanical engineering

Compressor rotor with coated blades

 #14 | 2019-05-16
US20190145431A1
Mechanical engineering

Mistuned fan

 #15 | 2019-04-11
US20190107123A1
Mechanical engineering

Mistuned fan for gas turbine engine

 #16 | 2019-03-21
US20190085868A1
Mechanical engineering

Mistuned compressor rotor with hub scoops

 #17 | 2019-03-21
US20190085708A1
Mechanical engineering

Compressor rotor with coated blades

 #18 | 2019-03-21
US20190085704A1
Mechanical engineering

Mistuned rotor for gas turbine engine

 #19 | 2019-03-14
US20190078589A1
Mechanical engineering

Rotor with non-uniform blade tip clearance

 #20 | 2018-05-17
US20180135415A1
Mechanical engineering

Stress reduction dimples for circular holes

 #21 | 2017-08-24
US20170241432A1
Mechanical engineering

Compressor rotor for supersonic flutter and/or resonant stress mitigation

 #22 | 2017-08-03
US20170218767A1
Mechanical engineering

Method of balancing a gas turbine engine rotor

 #23 | 2017-06-22
US20170175776A1
Mechanical engineering

Mistuned fan

 #24 | 2017-03-16
US20170074104A1
Mechanical engineering

Gas turbine engine rotor balancing

 #25 | 2016-05-05
US20160123150A1
Mechanical engineering

Method of balancing a gas turbine engine rotor

 #26 | 2013-08-15
US20130209260A1
Mechanical engineering

Gas turbine engine rotor balancing

 #27 | 2013-05-02
US20130108456A1
Mechanical engineering

Blade for a gas turbine engine

 #28 | 2012-08-23
US20120210579A1
Mechanical engineering

Blade preloading method

 #29 | 2010-07-29
US20100189564A1
Mechanical engineering

Blade preloading system

 #30 | 2010-07-22
US20100183444A1
Mechanical engineering

Fan blade preloading arrangement and method

 #31 | 2009-10-01
US20090246032A1
Performing operations; transporting

Method of machining airfoil root fillets

 #32 | 2009-06-25
US20090162190A1
Mechanical engineering

Centrifugal impeller with internal heating

 #33 | 2005-11-17
US20050254958A1
Mechanical engineering

Natural frequency tuning of gas turbine engine blades

 #34 | 2005-11-17
US20050254953A1
Mechanical engineering

Blade fixing relief mismatch

 #35 | 2005-11-17
US20050254952A1
Mechanical engineering

Bladed disk fixing undercut

 #36 | 2005-08-30
US10193916
-

Low cycle fatigue life (LCF) impeller design concept
InventorID:

221555 ⎘