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John Kannapell Phones & Addresses

  • 23247 Sesame St, Torrance, CA 90502 (310) 549-5121 (310) 480-5120
  • Inglewood, CA
  • Hawthorne, CA
  • Redondo Beach, CA
  • El Segundo, CA
  • Hermosa Beach, CA
  • San Pedro, CA
  • Carson, CA
  • 23247 Sesame St, Torrance, CA 90502

Work

Position: Professional/Technical

Education

Degree: Graduate or professional degree

Resumes

Resumes

John Kannapell Photo 1

Cable

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Location:
Torrance, CA
Industry:
Telecommunications
Work:
Comcast Cable
Cable
John Kannapell Photo 2

John Kannapell

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Position:
Team Leader, F-35 Mechanisms IPT at Northrop Grumman Corp.
Location:
Greater Los Angeles Area
Industry:
Defense & Space
Work:
Northrop Grumman Corp. since Jan 2002
Team Leader, F-35 Mechanisms IPT

Northrop Grumman Sep 1992 - Jan 2002
Team Leader, F/A-18E/F Mechanical Systems

Northrop Grumman Aug 1983 - Aug 1992
Design Lead, B-2 Mechanical Systems
Education:
University of Missouri-Columbia 1978 - 1981
BSME, Mechanical and Aerospace Engineering
Skills:
Aerospace
Engineering Management
Systems Engineering

Publications

Us Patents

Actuator With Helical Cam Guides

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US Patent:
7185852, Mar 6, 2007
Filed:
Sep 29, 2004
Appl. No.:
10/953230
Inventors:
John Trouy Kannapell - Torrance CA, US
Assignee:
North Rop Grumman Corporation - Los Angeles CA
International Classification:
B64C 1/14
US Classification:
2441294, 49139
Abstract:
The invention is an actuator assembly for actuating a door or aerodynamic surface of an aircraft. In detail, the invention includes a housing having first and second ends and a longitudinal axis. The housing center portion further includes first and second helical slots extending along the longitudinal axis. A cam follower, having first and second ends, is movably mounted in the center portion, the cam follower movable along the longitudinal axis of the housing. An actuator is provided for actuating the cam follower in first and second directions along the longitudinal axis. A bolt assembly, having first and second ends, is mounted through the cam follower with the first and second ends thereof extending into the first and second helical slots. First and second bearings are mounted to the first and second ends of bolt assembly such that the first and second bearings are movably mounted in the first and second helical slots. An actuation rod has its first end in the form of a clevis with first and second lugs movably connected to the first and second ends of the bolt assembly.

Dual Release Actuator Assembly

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US Patent:
20080272607, Nov 6, 2008
Filed:
May 1, 2007
Appl. No.:
11/799241
Inventors:
John Trouy Kannapell - Torrance CA, US
Benjamin Ming Lee - Lawndale CA, US
International Classification:
E05C 3/16
US Classification:
292216
Abstract:
The invention is a dual release actuating assembly. In detail, the invention includes a link having first and second ends and a center section. A locking mechanism having a pin coupled to the center section of the is provided to prevent movement of the pin. An actuation rod is coupled to the second end of the link. A first actuator coupled to the first end of the link for moving the actuation rod in a first direction. A second actuator is coupled to the first end of the link for moving the actuation rod in a second direction. A unlocking system is includes to release the locking mechanism such that pin may translate allowing the link to rotate about the first end.

Stores Magazine And Launch System

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US Patent:
47021454, Oct 27, 1987
Filed:
Jun 17, 1986
Appl. No.:
6/875422
Inventors:
John T. Kannapell - Hermosa Beach CA
Haig Asdurian - Fullerton CA
Robert F. Buttles - Torrance CA
Assignee:
Northrop Corporation - Hawthorne CA
International Classification:
F41F 306
B64D 102
US Classification:
89 1803
Abstract:
A stores handling system for an aircraft having a fuselage including a chamber for enclosing the stores handling system proximate an area openable through said fuselage through which stores may be loaded into and ejected from the aircraft. The handling system comprises a magazine arranged substantially vertically within the chamber for storing and positioning ejectable stores and including a flexible drive having stores holding shoes spaced apart thereon for engaging and retaining stores against movement within the aircraft, and for lifting and/or lowering stores within the magazine; and a launching mechanism for receiving stores individually from said magazine drive, and including an actuator having hands pivotable between a first closed position and a second open position for engaging the lowermost store to preclude ejecting movement when said hands are in said first position, and for engaging said stores to eject same from the aircraft when said hands are in said second position.
John T Kannapell from Torrance, CA, age ~67 Get Report