Inventor profile of:

Michael Papple

City:

Verdun

Country:

Canada

Published Applications:

26

Last publication date:

2023-02-07

Top Assignees for applications by Michael Papple

The entities that hold a legal rights for patent applications filed by inventor Papple Michael:

Recent patent applications by Papple Michael

Michael Papple from Verdun, CA has applied for patents for these inventions. The list has both pending applications and granted patents:

#1 | 2023-02-07
US17454529
Mechanical engineering

Turbine blade airfoil profile

#2 | 2023-02-07
US17454524
Mechanical engineering

Turbine blade airfoil profile

#3 | 2020-10-22
US20200332669A1
Mechanical engineering

Turbine stator outer shroud cooling fins

#4 | 2020-10-15
US20200325781A1
Mechanical engineering

Internally cooled turbine blade with creep reducing divider wall

#5 | 2019-11-21
US20190353349A1
Mechanical engineering

Internally cooled dilution hole bosses for gas turbine engine combustors

#6 | 2019-07-11
US20190212008A1
Mechanical engineering

Combustor heat shield

#7 | 2018-03-15
US20180073736A1
Mechanical engineering

Combustor dome heat shield

#8 | 2017-03-30
US20170089581A1
Mechanical engineering

SINGLE SKIN COMBUSTOR HEAT TRANSFER AUGMENTERS

#9 | 2017-03-30
US20170089580A1
Mechanical engineering

Single skin combustor with heat transfer enhancement

#10 | 2017-03-02
US20170059162A1
Mechanical engineering

Internally cooled dilution hole bosses for gas turbine engine combustors

#11 | 2017-02-02
US20170030218A1
Mechanical engineering

Turbine vane rear insert scheme

#12 | 2016-10-13
US20160298846A1
Mechanical engineering

Combustor dome heat shield

#13 | 2016-10-13
US20160298841A1
Mechanical engineering

Combustor heat shield

#14 | 2016-09-22
US20160273366A1
Mechanical engineering

Internally cooled gas turbine engine airfoil

#15 | 2016-04-21
US20160108742A1
Mechanical engineering

Partially coated blade

#16 | 2016-03-24
US20160084091A1
Mechanical engineering

High pressure turbine blade cooling hole distribution

#17 | 2016-02-11
US20160040880A1
Mechanical engineering

Combustor heat shield

#18 | 2015-12-17
US20150362191A1
Mechanical engineering

Combustor heat shield

#19 | 2015-12-17
US20150361800A1
Mechanical engineering

Airfoil with variable land width at trailing edge

#20 | 2015-12-10
US20150354818A1
Mechanical engineering

Multiple ventilated rails for sealing of combustor heat shields

#21 | 2015-12-03
US20150345789A1
Mechanical engineering

Combustor heat shield for a gas turbine engine

#22 | 2015-05-21
US20150135720A1
Mechanical engineering

Combustor dome heat shield

#23 | 2015-04-02
US20150093252A1
Mechanical engineering

Internally cooled airfoil

#24 | 2015-03-26
US20150086381A1
Mechanical engineering

Internally cooled airfoil

#25 | 2014-03-27
US20140086756A1
Mechanical engineering

Internally cooled gas turbine engine airfoil

#26 | 2013-10-10
US20130266416A1
Mechanical engineering

Cooling system for a turbine vane

InventorID:

476403 ⎘