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Michael A Vinup

from Phoenix, AZ
Age ~38
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Also known as:
Michael Allen Vinup, Mike Vinup
Phone and address:
3620 E Lavender Ln, Phoenix, AZ 85044
Related to:
Scott VinupEmily Miracle, 27Jacob Islas, 40Rachel IslasAndrew P Schwager, 55Valerie D Sturdivant, 48
Connected to:
Ann M Vinup, 87Carolyn C Vinup, 62Linda S Vinup, 75Vin T Vinvin, 41Amanda Vinyard, 36Amos A Vinyard, 48Ashlee R Vinyard, 43Brandon C Vinyard, 41Calista M Vinyard, 46Carmen R Vinyard, 42

Michael Vinup Phones & Addresses

  • 3620 E Lavender Ln, Phoenix, AZ 85044
  • Goodyear, AZ
  • Gilbert, AZ
  • Tempe, AZ
  • O Fallon, IL

Work

Company: Honeywell Dec 2018 Position: Principal engineer - product design and project

Education

Degree: Bachelor of Science In Engineering, Bachelors School / High School: Arizona State University 2006 to 2011 Specialities: Mechanical Engineering

Skills

Mechanical Engineering • Microsoft Office • Solidworks • Project Management • Engineering • Gas Turbines • Finite Element Analysis • Ansys • Matlab • Labview • Heat Transfer • Control Systems Design • Design For Manufacturing • Simulink • Thermodynamics

Ranks

Certificate: Green Belt Six Sigma Certified

Industries

Mechanical Or Industrial Engineering

Resumes

Resumes

Michael Vinup Photo 1

Principal Engineer

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Location:
Phoenix, AZ
Industry:
Mechanical Or Industrial Engineering
Work:
Honeywell
Principal Engineer - Product Design and Project
Honeywell
Global Project Engineer and Senior Product Design Engineer
Honeywell Sep 1, 2011 - Jan 2017
Engineer Ii - R and D
National Park Service Through Asu May 2010 - Aug 2010
Greenhouse Gas Project Intern
May 2010 - Aug 2010
Principal Engineer
Education:
Arizona State University 2006 - 2011
Bachelor of Science In Engineering, Bachelors, Mechanical Engineering
Skills:
Mechanical Engineering
Microsoft Office
Solidworks
Project Management
Engineering
Gas Turbines
Finite Element Analysis
Ansys
Matlab
Labview
Heat Transfer
Control Systems Design
Design For Manufacturing
Simulink
Thermodynamics
Certifications:
Green Belt Six Sigma Certified

Publications

Us Patents

Hybrid Bonded Turbine Rotors And Methods For Manufacturing The Same

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US Patent:
20160146024, May 26, 2016
Filed:
Nov 24, 2014
Appl. No.:
14/551293
Inventors:
- Morristown NJ, US
Daira Legzdina - Phoenix AZ, US
Don Mittendorf - Mesa AZ, US
Milton Ortiz - Scottsdale AZ, US
Ardeshir Riahi - Scottsdale AZ, US
Michael Vinup - Phoenix AZ, US
Assignee:
HONEYWELL INTERNATIONAL INC. - Morristown NJ
International Classification:
F01D 5/30
F01D 5/28
B23K 20/12
C22F 1/18
B23K 31/02
B23K 20/00
C22F 1/10
F01D 5/18
B23K 31/12
Abstract:
Hybrid bonded turbine rotors and methods for manufacturing the same are provided. A hybrid bonded turbine rotor comprises a turbine disk and a plurality of turbine blades each metallurgically bonded to a corresponding raised blade attachment surface of a plurality of raised blade attachment surfaces of the turbine disk to define a bond plane located at a selected radial position. Turbine disk has a rim portion comprising a live rim of circumferentially continuous material and a plurality of live rim notches in an outer periphery of the turbine disk alternating with the plurality of raised blade attachment surfaces defining the outer periphery. The selected radial position is outboard of the live rim. Each pair of adjacent turbine blades defines a shank cavity therebetween. The shank cavity extends radially outwardly from the live rim and includes a live rim notch disposed below the bond plane and above the live rim.

Turbine Engines With Ceramic Vanes And Methods For Manufacturing The Same

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US Patent:
20140161623, Jun 12, 2014
Filed:
Nov 20, 2012
Appl. No.:
13/681675
Inventors:
HONEYWELL INTERNATIONAL INC. - , US
Milton Ortiz - Scottsdale AZ, US
Kin Poon - Tempe AZ, US
Michael Vinup - Gilbert AZ, US
Ardeshir Riahi - Scottsdale AZ, US
Assignee:
HONEYWELL INTERNATIONAL INC. - Morristown NJ
International Classification:
F01D 5/12
US Classification:
416241 R, 29889
Abstract:
A vane assembly includes first and second annular metal rings configured to accept a compressed gas flow therebetween. The first and second annular rings each include a cutout portion. The assembly further includes a ceramic matrix composite vane configured as an airfoil having a blunt rounded nose and a flattened and tapered tail. A first radial end of the vane is rigidly disposed on the first annular ring and a second radial end of the vane is slidably disposed within the cutout portion of the second annular ring such that the vane is encompassed by the first and second annular rings. The vane includes a hollow through opening portion extending radially therethrough. Still further, the assembly includes a metallic elongated member disposed within and extending through the hollow portion of vane and through the cutout portion of the first annular ring.
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Michael A Vinup from Phoenix, AZ, age ~38 Get Report