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Ernest S Blazic

from Yorba Linda, CA
Deceased
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Also known as:
Ernie Blazic, Ernrst Blaz
Phone and address:
6062 Candle Light Ln, Yorba Linda, CA 92886
(714) 528-6589
Related to:
John P BlazicDaniel O Otero, 72Callie A Wehrman, 48Dorothy Lazar, 94Laura Blazic, 30Steven Blazic BlazicSteve M Blazic, 52Patricia H LazarPatricia Lynn Blazic, 66Steven C Wehrman, 52Sharron S Blazic, 58Kenneth H LazarLisa R Blazic, 52Barbara L Wehrman, 86
Connected to:
Carol S Blazic, 80David F Blazic, 83Randall J Blazic, 57Nicole F Blazicek, 28Alanna M Blazier, 67Elizabeth R Blazier, 50Stefan E Blazier, 45Stacey L Blazina, 43Stephen Blazina, 59Erik R Blazing, 43

Ernest Blazic Phones & Addresses

  • 6062 Candle Light Ln, Yorba Linda, CA 92886 (714) 528-6589
  • Agoura Hills, CA

Resumes

Resumes

Ernest Blazic Photo 1

Ernest Blazic

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Position:
Manager, Development Engineering at Tyco Electronics
Location:
Greater Los Angeles Area
Industry:
Aviation & Aerospace
Work:
Tyco Electronics since Sep 2010
Manager, Development Engineering
Crane Aerospace Nov 2006 - Sep 2010
Engineering Department Manager
Northrop Grumman, Navigation Systems Division (Litton GCSD) May 2002 - Nov 2006
Supervisor/Lead Engineer
ATK (SAT, Inc.) Jul 1998 - Mar 2002
Senior Engineer
TRW Automotive (Kelsey-Hayes) Feb 1993 - Jun 1998
Senior Systems Engineer
Education:
California State University Northridge - Graduate School 2004 - 2006
MS, Engineering Management University of Michigan - Rackham Graduate School 1983 - 1984
MS, Mechanical Engineering University of Michigan 1977 - 1981
BS, Mechanical Engineering
Skills:
Im a creative and dynamic team player with proven capacity to lead teams through strong interpersonal and communication skills
Skillful at new product development and making existing designs more producible
Interests:
weight training, hiking, biking, backpacking, classic cars
Honor & Awards:
Shock and Vibration Isolation for Aircraft Brake Control Valve, Crane Aerospace, 04/2008, App. # 12/422,923, Guided munitions electronic package & method, ATK Missile Company, 06/2004, Patent # 6,744,637, Solenoid coil structure & interconnection, Kelsey-Hayes, 03/2002, Patent # 6,352,317, Solenoid coil structure, Kelsey-Hayes, 09/2000, Patent # 6,120,114, ABS valve body heat sink for control module electronics, Kelsey-Hayes, 09/1999, Patent # 5,957,547, Virtual image display management system with head-up display, Hughes Aircraft, 05/1996, Patent # 5,519,410, Conformal circuit with harsh environment isolation materials, Hughes Aircraft, 12/1994, Patent # 5,375,471, Conformal circuit for structural health monitoring & assessment, Hughes Aircraft, 02/1993, Patent # 5,184,516
Ernest Blazic Photo 2

Ernest Blazic

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Ernest Blazic Photo 3

Mechanical Or Industrial Engineering Professional

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Location:
Orange County, California Area
Ernest Blazic Photo 4

Ernest Blazic

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Publications

Us Patents

Guided Munitions Electronics Package And Method

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US Patent:
6744637, Jun 1, 2004
Filed:
Nov 27, 2002
Appl. No.:
10/307127
Inventors:
Ernest Steven Blazic - Agoura Hills CA
Kent Carl Nelson - Simi Valley CA
Farhad James Nekoogar - Oak Park CA
Assignee:
Alliant Techsystems Inc. - Edina MN
International Classification:
H05K 718
US Classification:
361796, 361752, 361730, 361807, 211 4117, 174 50
Abstract:
A method and system for packaging electronics with an electronic card rack of radial panels, an outer casing, a stabilizing ring, and a flex-circuit interconnect, whereby electronic cards inserted into the sectors formed by the radial panels do not carry the structural load. The card-mounted devices are optimally oriented for set back forces, and minimal potting and/or structural foam is required, if any. The present invention provides a lightweight, highly serviceable assembly that is relatively less expensive to produce, test and rework compared with potted assemblies.

Shock And Vibration Isolation For Aircraft Brake Control Valve

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US Patent:
8136894, Mar 20, 2012
Filed:
Apr 13, 2009
Appl. No.:
12/422923
Inventors:
Ernest Blazic - Agoura Hills CA, US
Assignee:
Hydro-Aire, Inc., a Subsidiary of Crane Co. - Burbank CA
International Classification:
B60T 8/36
US Classification:
3031192, 3031193, 267293, 248635, 248638
Abstract:
The shock and vibration isolation system for hard mounting of a manifold of a brake control valve protects the brake control valve manifold from shock and vibration by incorporation of shock and vibration isolators in mounting feet of the manifold. The shock and vibration isolators have a pre-selected natural frequency chosen to protect components of the brake control valve damaging shock and vibration. The shock and vibration isolators each include a silicone rubber insert portion, a first outer sheath secured about a first end of the silicone rubber insert portion, a second outer sheath member secured about a second end of the silicone rubber insert portion, with a gap between the first and second outer sheaths.

Shock And Vibration Isolation For Aircraft Brake Control Valve

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US Patent:
8308149, Nov 13, 2012
Filed:
Jul 1, 2009
Appl. No.:
12/496557
Inventors:
Ernest Blazic - Agoura Hills CA, US
Assignee:
Hydro-Alre, Inc. - Burbank CA
International Classification:
F16F 7/00
US Classification:
267141, 267293, 3031193, 248635, 248638
Abstract:
The shock and vibration isolation system for hard mounting of a manifold of a brake control valve includes shock and vibration isolators that can be assembled in the mounting feet of the manifold of the brake control valve. The shock and vibration isolators have a pre-selected, predetermined natural frequency operative to protect components of the brake control valve from shock and vibration. Each of the shock and vibration isolators includes a radially inner generally spool shaped rigid insert portion and a radially outer generally spool shaped vibration insulating sheath portion.

Conformal Circuit With Harsh Environment Isolation Materials

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US Patent:
53754719, Dec 27, 1994
Filed:
Jun 30, 1992
Appl. No.:
7/906594
Inventors:
Ernest S. Blazic - Hawthorne CA
Joseph P. Smalanskas - Westchester CA
Assignee:
Hughes Aircraft Company - Los Angeles CA
International Classification:
G01B 716
US Classification:
73767
Abstract:
A multilayer flexible circuit for sensing physical properties of a structural surface 12 capable of surviving exposure in harsh environments through the use of isolation materials 70 disposed within the flexible circuit 10.

Virtual Image Display Management System With Head-Up Display

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US Patent:
55194109, May 21, 1996
Filed:
Sep 19, 1994
Appl. No.:
8/308489
Inventors:
Joseph P. Smalanskas - Westchester CA
Dale W. Hopkins - Garden Grove CA
Scott T. Wood - Los Angeles CA
Ernest S. Blazic - Ypsilanti MI
Assignee:
Hughes Aircraft Company - Los Angeles CA
International Classification:
G09G 500
US Classification:
345 7
Abstract:
A virtual image display management system using a head-up display that improves the ability of an operator of an automobile, or other equipment, to focus on primary functions, such as vehicle operation, while providing secondary information within the operator's primary visual field without requiring the operator to refocus. The present virtual image display management system integrates one or more secondary function displays into one reconfigurable virtual image head-up display. Several secondary functions are displayed sequentially using analog/digital symbology, icon representation, alphanumeric text or static/motion picture format. The operator may select secondary functions to be monitored, the display format, and the data acquisition intervals. A reconfigurable virtual image display processor accommodates more sophisticated sensor and communication functionality without penalizing efficiency and safety of the operator's primary functions. The present system integrates, interprets, selects and displays data derived from multiple sensors and communications systems at an optimum visual location within the operator's primary field of view.

Conformal Circuit For Structural Health Monitoring And Assessment

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US Patent:
51845164, Feb 9, 1993
Filed:
Jul 31, 1991
Appl. No.:
7/738389
Inventors:
Ernest S. Blazic - Hawthorne CA
Robert A. Bueker - Anaheim Hills CA
Lynn O. Waters - Hermosa Beach CA
William D. Farwell - Thousand Oaks CA
Joseph P. Smalanskas - Westchester CA
Assignee:
Hughes Aircraft Company - Los Angeles CA
International Classification:
G01N 1908
US Classification:
73799
Abstract:
A strain, crack and acoustic emission conformal structural health monitoring circuit with integral preprocessor and provisions for connectorization to a central processing system includes a strain gauge (11) having crack sensing traces (21), (23), and (25) sandwiched between a bottom layer (13) and a top layer (39). Strain gauge (11) is attached to an aircraft structural surface (51) to be monitored. Successive alternating layers of interconnecting sheet layers (61) and dielectric layers (63) joined by successive layers of non-structural adhesive (65) are added sufficient to effectively attenuate any stress forces, and forces directly from the strain and cracks, from traveling upward from the aircraft structural surface (51). A metalization layer (47) tops the successive layers and supports an integrated circuit (43) which may be multi-chip hybrid package, discretely packaged components or conformally coated chip/circuit assemblies, and provides a means of interconnect to and protection from the ambient environment.

Isolation System For An Electronic Device

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US Patent:
20140138121, May 22, 2014
Filed:
Nov 16, 2012
Appl. No.:
13/679681
Inventors:
- Berwyn PA, US
ERNEST STEVEN BLAZIC - Agoura Hills CA, US
Assignee:
Tyco Electronics Corporation - Berwyn PA
International Classification:
H01B 5/16
US Classification:
174135
Abstract:
An isolation system is provided for an electronic device that is configured to be mounted to a structure. The isolation system includes a flexible conductor configured to be electrically connected to the electronic device. The isolation system also includes an isolator configured to be coupled between the electronic device and the structure such that the isolator is configured to attenuate at least one of shock or vibration exerted on the electronic device. At least a portion of the isolator is electrically conductive. The isolator is electrically connected to the flexible conductor and is configured to be electrically connected to the structure such that the isolator provides an electrical path between the flexible conductor and the structure.

Isolator For An Electronic Device

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US Patent:
20140139979, May 22, 2014
Filed:
Nov 16, 2012
Appl. No.:
13/679710
Inventors:
- Berwyn PA, US
ERNEST STEVEN BLAZIC - Agoura Hills CA, US
Assignee:
Tyco Electronics Corporation - Berwyn PA
International Classification:
H05K 7/02
US Classification:
36167901
Abstract:
An electronic device assembly includes an electronic device having a mount that includes a mounting opening. The mounting opening is configured to receive mounting hardware therein for mounting the electronic device to a structure. An isolator is coupled to the mount. The isolator includes an elastomeric bushing configured to attenuate at least one of shock or vibration exerted on the electronic device. The isolator is incorporated within the mount such that the elastomeric bushing is received into the mounting opening of the mount.
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Ernest S Blazic from Yorba Linda, CADeceased Get Report