P

Inventor

PAPPLE MICHAEL

CA32 patents
⚠️ This page may combine multiple inventors who share the name “PAPPLE MICHAEL”. Patents are grouped by organization below to help distinguish them — per-person disambiguation is on the roadmap.

PRATT & WHITNEY CANADA

31 patents
US6406260B1Jun 18, 2002

Heat transfer promotion structure for internally convectively cooled airfoils

PRATT & WHITNEY CANADA69 citations96
US6257831B1Jul 10, 2001

Cast airfoil structure with openings which do not require plugging

PRATT & WHITNEY CANADA71 citations96
US6508620B2Jan 21, 2003

Inner platform impingement cooling by supply air from outside

PRATT & WHITNEY CANADA90 citations95
US7520726B2Apr 21, 2009

HP turbine blade airfoil profile

PRATT & WHITNEY CANADA40 citations92
US7300250B2Nov 27, 2007

Cooled airfoil trailing edge tip exit

PRATT & WHITNEY CANADA31 citations92
US5711650AJan 27, 1998

Gas turbine airfoil cooling

PRATT & WHITNEY CANADA54 citations92
US10267521B2Apr 23, 2019

Combustor heat shield

PRATT & WHITNEY CANADA13 citations84
US9982890B2May 29, 2018

Combustor dome heat shield

PRATT & WHITNEY CANADA8 citations84
US9746184B2Aug 29, 2017

Combustor dome heat shield

PRATT & WHITNEY CANADA10 citations84
US9625152B2Apr 18, 2017

Combustor heat shield for a gas turbine engine

PRATT & WHITNEY CANADA12 citations84
US9557060B2Jan 31, 2017

Combustor heat shield

PRATT & WHITNEY CANADA8 citations84
US9376921B2Jun 28, 2016

Internally cooled gas turbine engine airfoil

PRATT & WHITNEY CANADA7 citations84
US9581029B2Feb 28, 2017

High pressure turbine blade cooling hole distribution

PRATT & WHITNEY CANADA8 citations83
US11015455B2May 25, 2021

Internally cooled turbine blade with creep reducing divider wall

PRATT & WHITNEY CANADA2 citations73
US9933161B1Apr 3, 2018

Combustor dome heat shield

PRATT & WHITNEY CANADA5 citations73
US9810071B2Nov 7, 2017

Internally cooled airfoil

PRATT & WHITNEY CANADA4 citations73
US9638046B2May 2, 2017

Airfoil with variable land width at trailing edge

PRATT & WHITNEY CANADA3 citations73
US9534786B2Jan 3, 2017

Combustor heat shield

PRATT & WHITNEY CANADA4 citations73
US9500093B2Nov 22, 2016

Internally cooled airfoil

PRATT & WHITNEY CANADA4 citations73
US10386072B2Aug 20, 2019

Internally cooled dilution hole bosses for gas turbine engine combustors

PRATT & WHITNEY CANADA2 citations72
US10247034B2Apr 2, 2019

Turbine vane rear insert scheme

PRATT & WHITNEY CANADA2 citations72
US10041675B2Aug 7, 2018

Multiple ventilated rails for sealing of combustor heat shields

PRATT & WHITNEY CANADA5 citations72
US11572790B1Feb 7, 2023

Turbine blade airfoil profile

PRATT & WHITNEY CANADA2 citations70
US10989409B2Apr 27, 2021

Combustor heat shield

PRATT & WHITNEY CANADA0 citations62
US8007237B2Aug 30, 2011

Cooled airfoil component

PRATT & WHITNEY CANADA5 citations62
US11085644B2Aug 10, 2021

Internally cooled dilution hole bosses for gas turbine engine combustors

PRATT & WHITNEY CANADA0 citations61
US11572789B1Feb 7, 2023

Turbine blade airfoil profile

PRATT & WHITNEY CANADA0 citations59
US10822987B1Nov 3, 2020

Turbine stator outer shroud cooling fins

PRATT & WHITNEY CANADA1 citations58
US10221695B2Mar 5, 2019

Internally cooled gas turbine engine airfoil

PRATT & WHITNEY CANADA0 citations52
US10174626B2Jan 8, 2019

Partially coated blade

PRATT & WHITNEY CANADA0 citations41
US10260751B2Apr 16, 2019

Single skin combustor with heat transfer enhancement

PRATT & WHITNEY CANADA0 citations40

BERGMAN RUSSELL J

1 patent