Wil Baker resumes & CV records
Resumes
Wil Baker
Location:
Phoenix, Arizona Area
Industry:
Aviation & Aerospace
Wil L BakerSun City, AZ
Wil Baker Phones & Addresses
Sun City West, AZ
Colorado Springs, CO
Mentions for Wil L Baker
Publications & IP owners
Us Patents
Methods For Fabricating High Temperature Castable Articles And Gas Turbine Engine Components
US Patent:
2012022, Sep 13, 2012
Filed:
Mar 8, 2011
Appl. No.:
13/042893
Inventors:
Jason Smoke - Phoenix AZ, US
Wil Baker - Phoenix AZ, US
Dennis Wolski - Chandler AZ, US
Wil Baker - Phoenix AZ, US
Dennis Wolski - Chandler AZ, US
Assignee:
HONEYWELL INTERNATIONAL INC. - Morristown NJ
International Classification:
B29C 33/38
B29C 39/26
B29C 39/02
B29C 35/08
B29C 33/72
B29C 39/26
B29C 39/02
B29C 35/08
B29C 33/72
US Classification:
264401, 264 39
Abstract:
Embodiments of a method are provided for fabricating a high temperature castable article, such as a casting mold or a core. In one embodiment, the method includes the steps of providing a suspension containing a plurality of ceramic particles and a photo-curable monomer; photo-curing selected portions of the suspension to produce a green body coated, at least partially, with uncured suspension; and removing the uncured suspension from the green body under process conditions at which the viscosity of the uncured suspension is reduced. The process conditions include exposing the green body to one of the group consisting of: (i) microwave energy sufficient to excite a dipole moment of the uncured suspension and (ii) sonic energy sufficient to induce shear-thinning of the uncured suspension. The green body is then heat treated to produce the high temperature castable article.
Quinary, Low-Conductivity Thermal Barrier Coatings For Turbine Engine Components
US Patent:
2019020, Jul 4, 2019
Filed:
Jan 3, 2018
Appl. No.:
15/860861
Inventors:
- Morris Plains NJ, US
Wil Baker - Phoenix AZ, US
Vladimir K. Tolpygo - Scottsdale AZ, US
Wil Baker - Phoenix AZ, US
Vladimir K. Tolpygo - Scottsdale AZ, US
Assignee:
HONEYWELL INTERNATIONAL INC. - Morris Plains NJ
International Classification:
F01D 5/28
F01D 9/04
F01D 9/04
Abstract:
Thermal barrier coatings, which may be used in gas turbine engines, comprise or consist of a tantala-niobia-zirconia mixture that is stabilized with two or more stabilizers. An exemplary thermal barrier coating comprises or consists of, by mole percent: about 2% to about 30% YO; about 8% to about 30% YbOor GdOor combination thereof; about 6% to about 30% TaO; about 0.1% to about 10% NbO; about 0% to about 10% HfO; and a balance of ZrO.
Thermal Barrier Coatings For Turbine Engine Components
US Patent:
2015019, Jul 9, 2015
Filed:
Jun 24, 2014
Appl. No.:
14/312869
Inventors:
- Morristown NJ, US
Wil Baker - Phoenix AZ, US
Wil Baker - Phoenix AZ, US
Assignee:
HONEYWELL INTERNATIONAL INC. - Morristown NJ
International Classification:
C23C 28/00
C23C 14/08
F02K 1/82
C23C 14/30
C09D 1/00
F01D 5/28
C23C 14/08
F02K 1/82
C23C 14/30
C09D 1/00
F01D 5/28
Abstract:
Thermal barrier coatings consist of a tantala-zirconia mixture that is stabilized with two or more stabilizers. An exemplary thermal barrier coating consists of, by mole percent: about 8% to about 30% YO; about 8% to about 30% YbOor GdOor combination thereof; about 8% to about 30% TaO; about 0% to about 10% HfO; and a balance of ZrO.
Turbine Engine, Engine Structure, And Method Of Forming An Engine Structure With Thermal Barrier Coating Protection
US Patent:
2015006, Mar 12, 2015
Filed:
Sep 10, 2013
Appl. No.:
14/023084
Inventors:
- Morristown NJ, US
Wil Baker - Phoenix AZ, US
Wil Baker - Phoenix AZ, US
International Classification:
F01D 25/00
F01D 5/28
F01D 5/28
US Classification:
60 3901, 4283128, 428613, 4274192, 20419215
Abstract:
A turbine engine, an engine structure, and a method of forming an engine structure are provided herein. In an embodiment, an engine structure includes a metal substrate, a thermal barrier coating layer, and a metal silicate protective layer. The thermal barrier coating layer overlies the metal substrate, and the thermal barrier coating layer has columnar grains with gaps defined between the columnar grains. The metal silicate protective layer is formed over the thermal barrier coating layer, and the metal silicate protective layer covers the columnar grains and the gaps between the columnar grains.
Low Conductivity Thermal Barrier Coating
US Patent:
2014027, Sep 18, 2014
Filed:
Mar 18, 2013
Appl. No.:
13/846574
Inventors:
HONEYWELL INTERNATIONAL INC. - , US
Wil Baker - Phoenix AZ, US
Wil Baker - Phoenix AZ, US
Assignee:
HONEYWELL INTERNATIONAL INC. - Morristown NJ
International Classification:
F01D 5/28
US Classification:
416241 B, 252 62
Abstract:
A ceramic composition of matter includes a solvent material and a solute material. The solvent material comprises zirconia or hafnia, or a mixture thereof, which is stabilized with a stabilizing oxide. The solute material comprises a metal oxide of the formula, XO, where X is a metallic element, O is oxygen, and “a” and “b” are stoichiometric coefficients. The difference in density between the solvent material and the solute material is less than about 30%.
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