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Galdemir C Botura

from Copley, OH
Age ~60
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Also known as:
Galdemir Cezar Botura, Galdemir E Botura, Glademir Cezar Botura, Glademir C Botura, Botura C Galdemir
Phone and address:
1160 Lisa Ann Dr, Akron, OH 44313
(234) 678-7856
Related to:
Meirelles B Matheus, 34Gabriela Botura, 31Matheus Botura, 34
Connected to:
Melissa F Botvinick, 44Dmitry Y Botvinnik, 41Amanda J Botway, 38Lloyd F Botway, 76Alex Botwin, 39David H Botwin, 41Laura C Botwin, 49Adam S Botwinik, 47Carol L Botwinick, 68David M Botwinick, 81

Galdemir Botura Phones & Addresses

  • 1160 Lisa Ann Dr, Akron, OH 44313 (234) 678-7856
  • Copley, OH
  • Atlanta, GA
  • San Diego, CA
  • 7766 Satellite Cir, North Canton, OH 44720 (330) 497-9863
  • Wadsworth, OH

Work

Company: Collins aerospace Oct 2018 Position: Associate director - chief programs engineer - ice protection, composites and water solutions

Education

Degree: Masters School / High School: Universidade Do Estado De SãO Paulo 1982 Specialities: Management

Skills

Aerospace • Engineering • Engineering Management • Systems Engineering • Six Sigma • Program Management • Continuous Improvement • Product Development • Cross Functional Team Leadership • Aircraft • Process Improvement • R&D • Lean Manufacturing • Leadership • Integration • Aviation • Strategic Planning • Business Strategy • Project Management • Project Planning • Earned Value Management • Electronics • Strategic Partnerships • Team Building • Analysis • Supply Chain Management • Aircraft Design • Aircraft Analysis • Aerothermodynamics • Mitigation • Change Management • Problem Solving • Market Research • Planning • Risk Management • Value Stream Mapping • Team Leadership • Business Process Improvement • Research and Development

Languages

English • Portuguese • French • Spanish

Ranks

Certificate: Lean Pratictioner Certified

Interests

Innovation • Environment • Emergent Technologies • Continuous Improvement • Leadership and Management • Biking • Processes • Science and Technology • Advanced Materials • Tennis • Animal Welfare • Arts and Culture • Health

Industries

Aviation & Aerospace

Resumes

Resumes

Galdemir Botura Photo 1

Associate Director - Chief Programs Engineer - Ice Protection, Composites And Water Solutions

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Location:
1160 Lisa Ann Dr, Akron, OH 44313
Industry:
Aviation & Aerospace
Work:
Collins Aerospace
Associate Director - Chief Programs Engineer - Ice Protection, Composites and Water Solutions
United Technologies
Chief Programs Engineer - Associate Director, Engineering
United Technologies Jan 2013 - Mar 2016
Lead - Specialty Analysis - Aerostructures
Goodrich Jan 2011 - Jan 2013
Senior Manager, Technology Office
United Technologies May 1999 - Jan 2011
Senior Manager, Advanced Materials and Systems - Innovation and Applied Technologies
Education:
Universidade Do Estado De SãO Paulo 1982
Masters, Management Universidade Do Estado De São Paulo 1982
Masters, Management University of Sao Paulo State 1982 - 1982
Bachelors, Mechanical Engineering
Skills:
Aerospace
Engineering
Engineering Management
Systems Engineering
Six Sigma
Program Management
Continuous Improvement
Product Development
Cross Functional Team Leadership
Aircraft
Process Improvement
R&D
Lean Manufacturing
Leadership
Integration
Aviation
Strategic Planning
Business Strategy
Project Management
Project Planning
Earned Value Management
Electronics
Strategic Partnerships
Team Building
Analysis
Supply Chain Management
Aircraft Design
Aircraft Analysis
Aerothermodynamics
Mitigation
Change Management
Problem Solving
Market Research
Planning
Risk Management
Value Stream Mapping
Team Leadership
Business Process Improvement
Research and Development
Interests:
Innovation
Environment
Emergent Technologies
Continuous Improvement
Leadership and Management
Biking
Processes
Science and Technology
Advanced Materials
Tennis
Animal Welfare
Arts and Culture
Health
Languages:
English
Portuguese
French
Spanish
Certifications:
Lean Pratictioner Certified
Project Management
Achieving Competitive Excellence
Supervisory
Fundamentals of Leadership & Financial Intelligence
Lean Pratictioner
Goodrich
Project Management Institute
United Technologies
Kent State University
University of Minnesota

Business Records

Name / Title
Company / Classification
Phones & Addresses
Galdemir Botura
MANAGER
UTC Aerospace Systems
Aircraft Manufacturers
1555 Corporate Woods Pkwy, Uniontown, OH 44685
(330) 374-3040
Galdemir Botura
MANAGER
Utc Aerospace Systems
Business Services
1555 Corporate Wood Pkwy, Uniontown, OH 44685
(330) 374-3040, (330) 374-2290

Publications

Us Patents

Aircraft Engine Nacelle Ice Protection System

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US Patent:
7780117, Aug 24, 2010
Filed:
Jul 11, 2006
Appl. No.:
11/456629
Inventors:
Galdemir C. Botura - North Canton OH, US
David C. Flosdorf - Akron OH, US
Assignee:
Goodrich Corporation - Charlotte NC
International Classification:
B64D 15/12
US Classification:
244134D, 244134 R
Abstract:
A nacelle inlet lip () for an aircraft engine () comprises a structural body () and an ice protection system (). The ice protection system () comprises a plurality of ice-protectors () independently controllable to allow inner zones () to be operated in different modes, different power levels, different time intervals and/or different energy amounts. In this manner, an inner aft zone (), an inner mid zone (), and an inner aft zone () can be anti-iced and/or de-iced to best preserve desired airflow patterns, to minimize ice particle shed size, and to optimize power consumption.

Ice Protection System For A Multi-Segment Aircraft Component

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US Patent:
7837150, Nov 23, 2010
Filed:
Dec 21, 2007
Appl. No.:
11/963014
Inventors:
Joseph Christopher Zecca - San Diego CA, US
Galdemir Cezar Botura - North Canton OH, US
Brian Bobby Burkett - Akron OH, US
Claude Marc Hubert - Riverside CA, US
Michael John Layland - Bonita CA, US
Timothy Robert Olson - La Jolla CA, US
James Michael Roman - Uniontown OH, US
Assignee:
Rohr, Inc. - Chula Vista CA
Goodrich Corporation - Charlotte NC
International Classification:
B64D 15/12
US Classification:
244134D
Abstract:
An aircraft component includes a first segment having a first leading edge surface that extends to a first end of the first segment. The aircraft component also includes a second segment having a second leading edge surface that extends to a second end of the second segment. The second end is substantially adjacent to the first end of the first segment, and is connected to the first end. The first leading edge surface includes electrical resistance heating that extends to the first end of the first segment. In addition, the second leading edge surface includes electrical resistance heating that extends to the second end of the second segment. The electrical resistance heating is capable of providing ice protection heating immediately on either side of a juncture between the connected first and second ends.

Aircraft Electrical Power System

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US Patent:
8260522, Sep 4, 2012
Filed:
Feb 9, 2010
Appl. No.:
12/702685
Inventors:
Galdemir C. Botura - North Canton OH, US
Richard J. Cole - Stow OH, US
James M. Roman - Uniontown OH, US
Assignee:
Goodrich Corporation - Charlotte NC
International Classification:
G06F 19/00
US Classification:
701 99, 701 22, 307 91, 307 22, 307 29, 307 31, 307 32, 180 658, 700295
Abstract:
An aircraft electric power supply system () for supplying electric power to onboard electric devices () during flight. To reduce the devices' power draw, the electric power is supplied via modulation at an increment-percentage that is determined by present conditions. An optimum portfolio can be established for the electrical devices () collectively, this portfolio being selected in accordance with an energy-management criterion or other aircraft objectives.

Aircraft Ice Protection System

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US Patent:
20100123044, May 20, 2010
Filed:
Nov 17, 2009
Appl. No.:
12/620408
Inventors:
Galdemir C. Botura - North Canton OH, US
International Classification:
B64D 15/14
B64D 15/00
US Classification:
244134 D, 244134 R
Abstract:
An ice protection system () is provided for an aircraft surface having a plurality of ice-susceptible regions. The system () comprises an ice protector (-) for each ice-susceptible region, a controller () which independently controls each of the ice protectors (-), and input channels (-) which conveys data to the controller (). The controller () uses the channel-conveyed data to determine optimum operation for each of the ice protectors and controls the supply electrical energy thereto in accordance with such optimization.

Aircraft Ice Protection System

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US Patent:
20110233340, Sep 29, 2011
Filed:
Feb 22, 2011
Appl. No.:
13/032296
Inventors:
Daniel P. Christy - Akron OH, US
Galdemir C. Botura - San Diego CA, US
International Classification:
B64D 15/14
US Classification:
244134 D
Abstract:
An ice protection system () wherein a heater array () comprises a series of consecutive electrothermal heaters () which proceed one after another in a substantially aft-fore-aft path. A power source () supplies the heater array () with electrical energy and a heater interface () switches each heater () into either an ON condition or an OFF condition. The heater array () can be architected to effectively and efficiently protect an ice-susceptible aircraft surface () by strategic heater shaping, concentrated power-density allocation, and/or tactical heating-episode execution.

Deicer Zones With Shedding-Enhanced Borders

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US Patent:
20130270253, Oct 17, 2013
Filed:
Apr 11, 2013
Appl. No.:
13/860868
Inventors:
Galdemir Botura - San Diego CA, US
Brian Burkett - Akron OH, US
Milan Mitrovic - Del Mar CA, US
Assignee:
GOODRICH CORPORATION - Charlotte NC
International Classification:
B64D 15/12
H05B 1/02
US Classification:
219475, 219486
Abstract:
An ice protection system comprises deicing zones each including an envelope defining an ice-protection area. Adjacent envelopes have spanwise edge regions flanking shared interzone borders. The edge regions are provided with nonlinear contours having features which project-and-recess in a direction generally parallel to the airstream direction.

Aircraft Feature With Heating System Formed Of Laser-Induced Graphene

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US Patent:
20220411076, Dec 29, 2022
Filed:
Jun 24, 2021
Appl. No.:
17/357676
Inventors:
- Charlotte NC, US
Jin Hu - Hudson OH, US
Casey Slane - Tallmadge OH, US
Galdemir Cezar Botura - Akron OH, US
Wenping Zhao - Glastonbury CT, US
International Classification:
B64D 15/12
B23K 26/00
B23K 26/352
B23K 26/70
B32B 5/18
B32B 3/12
B32B 5/02
B32B 7/12
B32B 9/04
B32B 25/20
B32B 27/34
B32B 27/28
Abstract:
Disclosed is a first method of providing a heating system to an outer skin of an aircraft, that has the steps of forming laser-induced graphene (LIG) on a polymer sheet by directing laser energy towards the polymer sheet; coupling electrical leads to the LIG; and bonding the polymer sheet against the outer skin or erosion protection layer secured to the outer skin so that to the polymer sheet conforms with a shape of the outer skin.

Impact And Knife Cut Resistant Pre-Impregnated Woven Fabric For Aircraft Heated Floor Panels

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US Patent:
20220288887, Sep 15, 2022
Filed:
May 27, 2022
Appl. No.:
17/804436
Inventors:
- Charlotte NC, US
Jin Hu - Hudson OH, US
Casey Slane - Tallmadge OH, US
Nathaniel Ching - Hartville OH, US
Galdemir Cezar Botura - Akron OH, US
International Classification:
B32B 5/02
B32B 3/12
B32B 15/14
B32B 27/08
B64C 1/18
Abstract:
A heated floor panel assembly for aircraft includes an impact layer made from a 2-D or 3-D woven high temperature thermoplastic fiber matrix impregnated with a resin. The impact layer can further include woven metallic fibers. The assembly also includes a stack of structural layers, a heating layer, and a core layer for absorbing shear stress.
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Galdemir C Botura from Copley, OH, age ~60 Get Report