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John Christopher Parine

from Fernandina Beach, FL
Age ~64
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Also known as:
John C Parine, Christopher Parine John
Related to:
Mark M Butler, 62Sharon A Kueneke, 75
Connected to:
Charles R Parinello, 68Gary C Parinella, 69Melissa B Parinello, 48Francesca R Parini, 37Shauna R Parini, 53Cheryl A Parino, 63Charles L Parins, 65Matthew S Parins, 47Angel Pariola, 51Shirish A Paripatyadar, 67

John Parine Phones & Addresses

  • Fernandina Beach, FL
  • Encinitas, CA
  • San Diego, CA
  • 1422 Moonflower Ln, Tucson, AZ 85748
  • 187 Stoneway Cir, Madison, AL 35758 (256) 430-3111
  • Vail, AZ
  • Huntsville, AL
  • Pima, AZ

Work

Company: Dynetics Oct 2006 Position: Senior principal engineer - unmanned systems and aerodynamics department

Education

School / High School: The New York Institute of Technology- Old Westbury, NY 1987 Specialities: B.S.M.E. in Mechanical & Aerospace Engineering

Resumes

Resumes

John Parine Photo 1

John Parine Madison, AL

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Work:
DYNETICS

Oct 2006 to 2000
Senior Principal Engineer - Unmanned Systems and Aerodynamics Department
RAYTHEON MISSILE SYSTEMS COMPANY
Tucson, AZ
Jun 1996 to Oct 2006
Senior Engineer II - Advanced Programs Department
TELEDYNE RYAN AERONAUTICAL
San Diego, CA
Jun 1995 to Jun 1996
Senior Engineer II - Global Hawk UAV Design Team
TRW SPACE & TECHNOLOGY DIVISION
Redondo Beach, CA
Feb 1995 to Jun 1995
Senior Engineer - Contract
GULFSTREAM AEROSPACE CORP
Savannah, GA
Feb 1994 to Feb 1995
Senior Engineer - Contract
ROHR INC
Chula Vista, CA
May 1988 to May 1993
Senior Engineer
PRATT & WHITNEY AIRCRAFT
East Hartford, CT
Jan 1990 to Feb 1991
Project Engineer - Tiger Team (Industry Assist)
Education:
The New York Institute of Technology
Old Westbury, NY
1987
B.S.M.E. in Mechanical & Aerospace Engineering
University of Southern California
Arizona State University
Project Management
Dynetics University
Project Management
Dynetics University
Management
Raytheon Learning Institute
Design
Raytheon Learning Institute
Mechanical Design

Publications

Us Patents

Deployment Mechanism For Stowable Fins

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US Patent:
6905093, Jun 14, 2005
Filed:
Sep 26, 2003
Appl. No.:
10/672533
Inventors:
Richard Dryer - Oro Valley AZ, US
Rudolph Adolph Eisentraut - Tucson AZ, US
Martin Allen Kebschull - Tucson AZ, US
John Christopher Parine - Tucson AZ, US
Assignee:
Raytheon Company - Waltham MA
International Classification:
F42B013/32
US Classification:
244 328, 244 329
Abstract:
A deployment mechanism () in combination with a missile (), guided projectile () or other ordnance that automatically pivots and rotates a fin () from a stowed orientation to a deployed orientation. The deployment mechanism () includes a tubular cam () having a retention mechanism () that retains the fin () simply and reliably in the stowed orientation. The tubular cam also guides the fin () quickly to the deployed orientation.

Single-Axis Fin Deployment System

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US Patent:
7642492, Jan 5, 2010
Filed:
Jan 26, 2005
Appl. No.:
11/043870
Inventors:
John C. Parine - Corona de Tucson AZ, US
Jeffrey H. Koessler - Tucson AZ, US
Purnachandra R. Gogineni - Tucson AZ, US
Juan A. Perez - Tucson AZ, US
Martin A. Kebschull - Tucson AZ, US
Assignee:
Raytheon Company - Waltham MA
International Classification:
F42B 10/14
US Classification:
244 327, 102348, 244 328, 244 329
Abstract:
A missile has fins that rotate about a single axis to deploy from a stowed position to a deployed position. A foil longitudinal axis of each fin is angled relative to a shaft of the fin, such that a single-axis rotation of the shaft moves the foil from the stowed position to a deployed position. A coil spring may provide both torsion and compression forces to rotate the fin into the deployed position and lock it into place. Torsion rotates the shaft until it reaches a seat on a bushing that is around the shaft. Then compression forces from the spring engage a keyed protrusion on the shaft with a corresponding keyway in the bushing, locking the shaft in place. There may be an additional lock once the fin is deployed, such as a spring-loaded pin in the missile body that engages a depression in the shaft.

Missile Having Deployment Mechanism For Stowable Fins

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US Patent:
20030178527, Sep 25, 2003
Filed:
Mar 19, 2002
Appl. No.:
10/102032
Inventors:
Rudolph Eisentraut - Tucson AZ, US
Martin Kebschull - Tucson AZ, US
John Parine - Tucson AZ, US
International Classification:
F42B010/14
F42B010/48
F42B015/01
US Classification:
244/003280
Abstract:
A missile () in combination with a deployment mechanism () that automatically pivots and rotates a fin () from a stowed orientation to a deployed orientation. The deployment mechanism () includes a spring () that provides a biasing force that urges the fin () to move quickly, simply and reliably from the stowed orientation to the deployed orientation. The deployment mechanism also includes one or more cams or other means for guiding the fin from the stowed orientation to the deployed orientation.
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John Christopher Parine from Fernandina Beach, FL, age ~64 Get Report