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Christopher F Rajecki

from Mckean, PA
Age ~62
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Also known as:
Christopher E Rajecki, Chris F Rajecki, Christphr F Rajecki, Christophe F Rajecki
Phone and address:
9242 Shadduck Rd, Mc Kean, PA 16426
(814) 476-7770
Related to:
Donna Rajecki, 84Michele M Rajecki, 57William J Theisen, 42Frank R Rajecki, 88Cindy M Rajecki, 49Suzanne Rajecki, 55Rita M Rajecki, 84Barbara A Rajecki, 64Michael J Rajecki, 57
Connected to:
Ardra Rajeev, 36Bindu Rajeev, 48Deva V Rajeev, 38Pratik Rajeevan, 41Timothy J Rajeff, 65Phillip M Rajek, 48William P Rajek, 77Deepan C Rajendiran, 36Akila Rajendran, 49Hemavathy Rajendran, 39

Christopher Rajecki Phones & Addresses

  • 9242 Shadduck Rd, Mckean, PA 16426 (814) 476-7770
  • Mc Kean, PA
  • 3008 Marcella Dr, Erie, PA 16506 (814) 833-3361

Work

Company: Lord corporation Aug 2007 Position: Staff engineer

Education

Degree: Bachelor of Mechanical Engineering School / High School: Gannon University 1981 to 1985 Specialities: Mechanical Engineering

Skills

Injection Molding • Finite Element Analysis • Engineering Management • Aerospace • Sheet Metal • Product Development • Automotive • Software Documentation • Assemblies • Pro Engineer

Industries

Mechanical Or Industrial Engineering

Resumes

Resumes

Christopher Rajecki Photo 1

Staff Engineer

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Location:
9242 Shadduck Rd, Mckean, PA 16426
Industry:
Mechanical Or Industrial Engineering
Work:
Lord Corporation since Aug 2007
Staff Engineer
Lord Corporation 1989 - 2007
Engineering Specialist
Ervite Corporation Oct 1985 - Aug 1989
Senior Product Engineer
Education:
Gannon University 1981 - 1985
Bachelor of Mechanical Engineering, Mechanical Engineering
Skills:
Injection Molding
Finite Element Analysis
Engineering Management
Aerospace
Sheet Metal
Product Development
Automotive
Software Documentation
Assemblies
Pro Engineer

Business Records

Name / Title
Company / Classification
Phones & Addresses
Christopher Rajecki
Director Information Technology
Lord Industrial Products
Chemicals · Mfg Aircraft Engine/Part Mfg Adhesives/Sealants Business Services Mfg Motor Vehicle Parts Mfg Power Transmsn Equip · Mfg Adhesives/Sealants · Mfg Fabrcatd Rubber Prdt Mfg Process Cntrl Instr Mfg Home Audio/Video Eqp Mfg Adhesives/Sealants Mfg Paints/Allied Prdts · All Other Rubber Prod Mfg
PO Box 10038, Erie, PA 16514
2000 W Grandview Blvd, Erie, PA 16509
(814) 868-0924, (814) 868-5424

Publications

Us Patents

Rotary Wing Aircraft Rod End And Method Of Making A Helicopter Vehicle Rod End With A Precocked Orientation

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US Patent:
7866025, Jan 11, 2011
Filed:
Sep 26, 2007
Appl. No.:
11/861866
Inventors:
Frank O. James - Girard PA, US
Christopher F. Rajecki - McKean PA, US
Assignee:
LORD Corporation - Cary NC
International Classification:
B23P 25/00
US Classification:
29458, 295271, 295272, 384221, 416134 A
Abstract:
The invention provides a rotary wing aircraft helicopter vehicle rod end and method of making a rod end. The rotary wing aircraft rod end includes a nonelastomeric inner member having an outer bonding surface segment and an axial bore with a center bore axis, a nonelastomeric outer member having an inner bonding surface segment and an axial bore center bore axis, and molded in place alternating elastomeric shims and nonelastomeric shims connecting the nonelastomeric inner member to the nonelastomeric outer member. The rod end includes a first inner elastomeric shim bonded to the nonelastomeric inner member outer bonding surface segment and to a first inner nonelastomeric shim and a second outer elastomeric shim bonded to the nonelastomeric outer member inner bonding surface segment and to a second outer nonelastomeric shim. The nonelastomeric inner member has a molded misalignment rotary wing aircraft rod end orientation with the outer nonelastomeric outer member.

Rotary Wing Aircraft Rod End And Method Of Making A Helicopter Vehicle Rod End With A Precocked Orientation

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US Patent:
8336185, Dec 25, 2012
Filed:
Dec 21, 2010
Appl. No.:
12/974285
Inventors:
Frank O. James - Girard PA, US
Christopher F. Rajecki - McKean PA, US
Assignee:
Lord Corporation - Cary NC
International Classification:
B23P 25/00
US Classification:
29458, 295271, 295272, 384221, 416134 A
Abstract:
The invention provides a rotary wing aircraft helicopter vehicle rod end and method of making a rod end. The rotary wing aircraft rod end includes a nonelastomeric inner member having an outer bonding surface segment and an axial bore with a center bore axis, a nonelastomeric outer member having an inner bonding surface segment and an axial bore center bore axis, and molded in place alternating elastomeric shims and nonelastomeric shims connecting the nonelastomeric inner member to the nonelastomeric outer member. The rod end includes a first inner elastomeric shim bonded to the nonelastomeric inner member outer bonding surface segment and to a first inner nonelastomeric shim and a second outer elastomeric shim bonded to the nonelastomeric outer member inner bonding surface segment and to a second outer nonelastomeric shim. The nonelastomeric inner member has a molded misalignment rotary wing aircraft rod end orientation with the outer nonelastomeric outer member.

Rotary Wing Aircraft Rod End And Method Of Making A Helicopter Vehicle Rod End With A Precocked Orientation

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US Patent:
20070231140, Oct 4, 2007
Filed:
Jan 14, 2005
Appl. No.:
11/036737
Inventors:
Frank James - Girard PA, US
Christopher Rajecki - McKean PA, US
International Classification:
B64C 27/50
US Classification:
41613400A
Abstract:
The invention provides a rotary wing aircraft helicopter vehicle rod end and method of making a rod end. The rotary wing aircraft rod end includes a nonelastomeric inner member having an outer bonding surface segment and an axial bore with a center bore axis, a nonelastomeric outer member having an inner bonding surface segment and an axial bore center bore axis, and molded in place alternating elastomeric shims and nonelastomeric shims connecting the nonelastomeric inner member to the nonelastomeric outer member. The rod end includes a first inner elastomeric shim bonded to the nonelastomeric inner member outer bonding surface segment and to a first inner nonelastomeric shim and a second outer elastomeric shim bonded to the nonelastomeric outer member inner bonding surface segment and to a second outer nonelastomeric shim. The nonelastomeric inner member has a molded misalignment rotary wing aircraft rod end orientation with the outer nonelastomeric outer member.
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Christopher F Rajecki from Mckean, PA, age ~62 Get Report