Mitchell Glenn LaBiche
Engineering at Misty Ln, Friendswood, TX

License number
Louisiana EI.0009933
Issued Date
May 22, 1984
Expiration Date
Sep 30, 1984
Category
Civil Engineer
Address
Address
503 Misty Ln, Friendswood, TX 77546

Professional information

Mitchell Labiche Photo 1

Mitchell Labiche - Friendswood, TX

Work:
AAR Composites - Bombardier
Engineering Consultant - FAA DER, Stress Analysis and Design Guidance/Support
Lockheed-Martin - NASA (JSC)
Engineering Consultant - Design, Thermal & Stress Analysis
Lockheed-Martin - NASA (JSC)
Engineering Consultant - Management, Design, and Analysis
ARMY AMRDEC
Stress Analysis, Design Lead, Manufacturing and Testing Liason
Emivest Aerospace
Aero Studies, Stress Analysis, Manufacturing Liason
DRS Technologies
Engineering Consultant - Design, Analysis, & Manufacturing
Wyle Laboratories
Engineering Consultant - Design, Analysis, Manufacturing
ITT Space Systems Division
Engineering Consultant - Analyst and System Engineering
Northrop-Grumman
Engineering Consultant - Design and Aero Anaylsis
Lockheed
Consultant on Joint Strike Fighter SDD
Lockheed
PRO-ENGINEER & PROMECHANICA
NASA / Lockheed Martin
Consultant on Robonaut Generation
Lockheed Martin - Houston, TX
Consultant - Management, Design, and Analysis
Borsig Technologies
Petro/Chemical Industry Analyst
Johnson Engineering - International Space Station
PRO-ENGINEER, PROMECHANICA, NASTRAN
Raytheon Airborne Technology System
PRO-ENGINEER
InterActive Digitial Devices, Inc
Founder and President
Lockheed Aeronautical System Company
manufacturing, marketing
Very Large Wing
Principal Investigator/Engineer
McDonnell-Douglas Helicopter Co. (Boeing)
ENGINEER
Allied-Signal Aerospace Company (Bendix)
R&D Principal Investigator of "fly
FBW
Author of technical proposals for military and commercial
General Engineering, Inc
2-axis large displacement side stick controller
Education:
University of - Southwestern, Louisiana, US
Bachelors of Science in Mechanical Engineering


Mitchell Labiche Photo 2

Mitchell Labiche - Friendswood, TX

Work:
AAR Composites - Bombardier
Engineering Consultant - FAA DER, Stress Analysis and Design Guidance/Support
Lockheed-Martin - NASA (JSC)
Engineering Consultant - Design, Thermal & Stress Analysis
Lockheed-Martin - NASA (JSC)
Engineering Consultant - Management, Design, and Analysis
ARMY AMRDEC
Stress Analysis, Design Lead, Manufacturing and Testing Liason
Emivest Aerospace
Aero Studies, Stress Analysis, Manufacturing Liason
DRS Technologies
Engineering Consultant - Design, Analysis, & Manufacturing
Wyle Laboratories
Engineering Consultant - Design, Analysis, Manufacturing
ITT Space Systems Division
Engineering Consultant - Analyst and System Engineering
Northrop-Grumman
Engineering Consultant - Design and Aero Anaylsis
Lockheed
Consultant on Joint Strike Fighter SDD
NASA / Lockheed Martin
Consultant on Robonaut Generation
Lockheed Martin - Houston, TX
Consultant - Management, Design, and Analysis
Borsig Technologies
Petro/Chemical Industry Analyst
Johnson Engineering - International Space Station
PRO-ENGINEER, PROMECHANICA, NASTRAN
Lockheed-Martin Astronautics
PRO-ENGINEER & PROMECHANICA
Raytheon Airborne Technology System
PRO-ENGINEER
InterActive Digitial Devices, Inc
Founder and President
Lockheed Aeronautical System Company
Principal Investigator/Engineer
McDonnell-Douglas Helicopter Co. (Boeing)
Contributing author
Allied-Signal Aerospace Company (Bendix)
R&D Principal Investigator of "fly
Hub City Iron Works, Inc
Hydrostatic Pressure Tester
Education:
University of - Southwestern, Louisiana, US
Masters in Mechanical Engineering


Mitchell Labiche Photo 3

Flyable Automobile

US Patent:
2003009, May 22, 2003
Filed:
Oct 25, 2002
Appl. No.:
10/281344
Inventors:
Mitchell LaBiche - Friendswood TX, US
International Classification:
B64C037/02, B64D005/00
US Classification:
244/002000
Abstract:
A flyable automobile comprising a right main wing connected to the flyable automobile and comprising a right wing inner portion and a right wing outer portion, the right wing outer portion hingedly connected to the right wing inner portion so that the right wing outer portion can be folded above the right wing inner portion, and the right main wing connected to the flyable automobile so that the right main wing can pivot into a storage compartment underneath in the flyable automobile, and a left main wing connected to the flyable automobile and having a left wing inner portion and an left wing outer portion, the left wing outer portion hingedly connected to the left wing inner portion so that the left wing outer portion can be folded above the left wing inner portion, the left main wing connected to the flyable automobile so that the left main wing can pivot into the storage compartment in the flyable automobile.