Jason Liles resumes & CV records
Resumes
Jason D Liles, 42Bybee, VA
Jason Liles Phones & Addresses
Palmyra, VA
Zion Crossroads, VA
Port St Lucie, FL
West Palm Beach, FL
Fayetteville, GA
Charlotte, NC
Port St Lucie, FL
Williamsfield, OH
Social networks
Jason D Liles
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Mentions for Jason D Liles
Publications & IP owners
Us Patents
Replaceable Rotor Blade Tip Clearance Measurement Device For A Gas Turbine Engine
US Patent:
2021010, 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
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
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.
Turbine Blade With Airfoil Tip Vortex Control
US Patent:
2017014, 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
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
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.
Bench Aft Sub-Assembly For Turbine Exhaust Case Fairing
US Patent:
2016001, 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
Jason David Liles - Port Saint Lucie FL, US
Jonathan Ariel Scott - Tolland CT, US
International Classification:
F02C 7/20
F01D 25/30
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
Public records
Vehicle Records
Jason Liles
Address:
1612 SW Realty St, Port Saint Lucie, FL 34987
Phone:
772-8785017
VIN:
5FNYF18707B023489
Make:
HONDA
Model:
PILOT
Year:
2007
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