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Philip M Bastnagel

from Indianapolis, IN
Age ~63
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Also known as:
Philip M Bastragel, Phil Bastnagel, Philip L
Phone and address:
6314 Hythe Rd, Indianapolis, IN 46220
(317) 578-1982
Related to:
John BastnagelLaura G Collins, 63Kathi A Collins, 59Jonathan W Bastnagel, 35Laurene M CollinsJoyce A Jones, 79Lavonne Vonne Bastnagel, 96Eugene E Collins, 97Jessica La BastnagelRamiro Dejesus Bastnagel, 32Steven R Jones, 54Jessica L Bastnagel, 37Victoria P Bastnagel, 66Matthew C Wilhite, 35Richard A Collins, 60Kathy Ann CollinsMichael Kelly CollinsBrittany M Wilhite, 35Tanya G Farreras, 53
Connected to:
James P Bastnagel, 69Flor M Basto, 66Michael Basto, 49Miguel Basto, 49Susana G Basto, 78Yolanda Basto, 96Jennifer Bastock, 34Anil Bastola, 46Hridaya Bastola, 39Madhu M Bastola, 42

Philip Bastnagel Phones & Addresses

  • 6314 Hythe Rd, Indianapolis, IN 46220 (317) 578-1982
  • 3029 Courthouse Dr E, West Lafayette, IN 47906
  • W Lafayette, IN
  • Denver, CO

Work

Position: Professional/Technical

Education

Degree: Associate degree or higher

Resumes

Resumes

Philip Bastnagel Photo 1

Chief Engineer Of Research And Technology

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Location:
Greenwood, IN
Industry:
Defense & Space
Work:
Rolls-Royce
Chief Engineer of Research and Technology
Rolls-Royce Sep 2007 - Oct 2014
Chief Project Engineer - Gas Turbine Modules
Rolls-Royce Aug 2003 - Sep 2007
Product Definition Manager of Hot Static Structures
Allison Advanced Development Company Jul 2000 - Aug 2003
Manager of Structural Analysis
Allison Advanced Development Company Jul 1997 - Jul 2000
Development Engineer
Education:
Purdue University 1984 - 1985
Master of Science, Masters, Engineering Purdue University 1980 - 1984
Bachelors, Bachelor of Science, Engineering Brebeuf High School
Skills:
Engineering Management
Resource Management
Structural Analysis
Engineer Configuration Management
Product Safety
Project Management
Consulting Engineering
Gas Turbines
Technical Leadership
Engineering Leadership
Stress Analysis
Finite Element Analysis
Safety Management
Risk Management
Power Generation
Requirements Management
Propulsion
Engineering
Aerospace
Systems Engineering
Program Management
Continuous Improvement
Six Sigma
Manufacturing
Aircraft
Aerospace Engineering
Aviation
Aerodynamics
Philip Bastnagel Photo 2

Philip Bastnagel

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Publications

Us Patents

Relief Slot For Combustion Liner

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US Patent:
8511089, Aug 20, 2013
Filed:
Jul 31, 2009
Appl. No.:
12/533467
Inventors:
Philip Michael Bastnagel - Indianapolis IN, US
Jack Dwayne Petty - Indianapolis IN, US
Assignee:
Rolls-Royce Corporation - Indianapolis IN
International Classification:
F23R 3/002
US Classification:
60752, 60754
Abstract:
A combustion liner has an aft seal ring defines a relief slot in a wall of the combustion liner. The relief slot defined in the wall includes a first slot portion extending from a first end of the wall to a termination point. An arcuate slot portion intersects the termination point of the first slot portion, and a generally circular aperture is defined in the wall at each end of the arcuate slot portion.

Paneled Combustion Liner

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US Patent:
20100162716, Jul 1, 2010
Filed:
Dec 18, 2009
Appl. No.:
12/642215
Inventors:
Philip M. Bastnagel - Indianapolis IN, US
Jack Petty - Indianapolis IN, US
International Classification:
F23R 3/42
F02C 7/00
US Classification:
60752
Abstract:
The present invention relates to combustors, and provides a combustion liner that may at least partially contain a combustion process. The combustion liner may include a support structure that supports a plurality of panels. The panels may be in the form of thermal barrier panels, e.g., that are attached to the support structure and/or other parts of the machine.

Gas Turbine Engine Component Construction

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US Patent:
20110185738, Aug 4, 2011
Filed:
Nov 22, 2010
Appl. No.:
12/951152
Inventors:
Philip M. Bastnagel - Indianapolis IN, US
Edward Claude Rice - Indianapolis IN, US
International Classification:
F02C 7/12
B23P 11/00
US Classification:
60754, 29888
Abstract:
A gas turbine engine component is disclosed having a construction that permits a working fluid to flow from one side of the component to the other. In one embodiment the construction includes multiple layers, and in one particular embodiment the construction includes three layers. One or more layers can have different properties. Additionally, one or more layers of the construction can include a cellular structure. In one embodiment the component is a gas turbine engine combustor liner.

High Strength Aerospace Components

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US Patent:
20170297673, Oct 19, 2017
Filed:
Mar 14, 2017
Appl. No.:
15/458489
Inventors:
- Indianapolis IN, US
Maxwell Layman - Indianapolis IN, US
Robert F. Proctor - Carmel IN, US
Philip M. Bastnagel - Indianapolis IN, US
Mark E. Bartolomeo - Brownsburg IN, US
Jonathan Michael Rivers - Indianapolis IN, US
Eric Handa - Indianapolis IN, US
Aaron Martin - Indianapolis IN, US
Christopher I. Hamilton - Carmel IN, US
Jonathan P. Acker - Westfield IN, US
Nathan J. Cooper - Avon IN, US
International Classification:
B64C 1/00
C23C 30/00
B64F 5/00
B64C 1/00
B64C 1/00
Abstract:
An article that includes a structured substrate having a macro-porous structure that defines a plurality of pores, and a metallic nano-crystalline coating on at least a portion of the structured substrate, where the metallic nano-crystalline coating defines an average grain size less than about 20 nanometers.

High Strength Vibrational-Dampened Components

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US Patent:
20170268120, Sep 21, 2017
Filed:
Mar 14, 2017
Appl. No.:
15/458458
Inventors:
- Indianapolis IN, US
Maxwell Layman - Indianapolis IN, US
Robert F. Proctor - Carmel IN, US
Philip M. Bastnagel - Indianapolis IN, US
Mark E. Bartolomeo - Brownsburg IN, US
Jonathan Michael Rivers - Indianapolis IN, US
Eric Handa - Indianapolis IN, US
Aaron Martin - Indianapolis IN, US
Christopher I. Hamilton - Carmel IN, US
Jonathan P. Acker - Westfield IN, US
Nathan J. Cooper - Avon IN, US
International Classification:
C25D 5/56
C25D 5/16
C25D 3/56
C25D 3/12
C25D 5/12
Abstract:
An article that includes a polymer-based substrate; and a metallic nano-crystalline coating on at least a portion of the polymer-based substrate, where the metallic nano-crystalline coating defines an average grain size less than about 20 nanometers, where the portion of the polymer-based substrate has a first Young's modulus and the metallic nano-crystalline coating has a second Young's modulus, where the first Young's modulus is at least five times less than the second Young's modulus.
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Philip M Bastnagel from Indianapolis, IN, age ~63 Get Report