Jason D Liles

US Patent:

20210102474, Apr 8, 2021

Filed:

Oct 3, 2019

Appl. No.:

16/592001

Inventors:

- Farmington CT, US
Veronika Reynolds - Lawrence MA, US
Jason David Liles - Port Saint Lucie FL, US

Assignee:

United Technologies Corporation - Farmington CT

International Classification:

F01D 21/00
F01D 11/12

Abstract:

A replaceable rotor blade tip clearance measurement device for a gas turbine engine, includes a threaded section along an axis and an integral abradable tip with an internal lattice geometry that extends from the threaded section along the axis.

US Patent:

20170145827, May 25, 2017

Filed:

Feb 8, 2016

Appl. No.:

15/018025

Inventors:

- Farmington CT, US
Kyle C. Lana - Portland CT, US
Jason David Liles - Port Saint Lucie FL, US

International Classification:

F01D 5/14
F02C 3/04
F01D 5/22

Abstract:

A rotor blade for a gas turbine engine is provided. The rotor blade having: an attachment; an airfoil extending from the attachment to a tip; and a squealer pocket located in a surface of the tip, wherein the squealer pocket is at least partially surrounded by a first surface of a wall located between the squealer pocket and a pressure side of the airfoil, wherein the first surface of the wall has a convex configuration with respect to the pressure side of the airfoil as it extends from a leading edge to a trailing edge of the airfoil.

US Patent:

20160017807, Jan 21, 2016

Filed:

Mar 11, 2014

Appl. No.:

14/773807

Inventors:

- Hartford CT, US
Jason David Liles - Port Saint Lucie FL, US
Jonathan Ariel Scott - Tolland CT, US

International Classification:

F02C 7/20
F01D 25/30

Abstract:

A fairing sub-assembly for a turbine frame comprises an inner ring , an outer ring and a plurality of strut-shells. The inner ring is formed of a plurality of inner segments . The outer ring is formed of a plurality of outer segments . The plurality of strut-shells connecting the inner ring and the outer ring . In another embodiment, the fairing sub-assembly comprises an inner band joining the plurality of inner segments and the plurality of strut-shells to form outer slots, and an outer band joining the plurality of outer segments and the plurality of strut-shells to form inner slots. A method of assembling a fairing comprises inserting the aforementioned fairing sub-assembly into an aft end of a turbine frame , inserting a plurality of forward strut-shells into the outer and inner slots at a forward end of the turbine frame , and joining the forward strut-shells to the fairing sub-assembly

Address:

1612 SW Realty St, Port Saint Lucie, FL 34987

Phone:

7728785017

VIN:

5FNYF18707B023489

Make:

HONDA

Model:

PILOT

Year:

2007