BackgroundCheck.run
Search For

Jerome J Connolly, 7121302 Atascocita Place Dr, Humble, TX 77346

Known as:
Jerome Dr Connolly Jerome John Connolly Jerome Y Connolly Jerome John Connelly
Related to:
Mauren L Connolly 67

Jerome Connolly Phones & Addresses

21302 Atascocita Place Dr, Humble, TX 77346    817-8463807    979-8472806   

Atascocita, TX   

2703 Broadacres Ln, Arlington, TX 76016    817-4683277    817-4682615   

2818 Glen Hollow Cir, Arlington, TX 76016   

4205 Annies Ln, Arlington, TX 76016    817-4681618   

Grand Prairie, TX   

Wichita, KS   

21302 Atascocita Place Dr, Humble, TX 77346   

Work

Position: Professional/Technical

Education

Degree: High school graduate or higher

Emails

f***[email protected]
Get Report
Control this profile

Mentions for Jerome J Connolly

Jerome Connolly resumes & CV records

Resumes

Jerome Connolly Photo 19

Structures Engineer

Location:
Houston, TX
Industry:
Aviation & Aerospace
Work:
Triumph Industries
Structures Engineer
Jerome Connolly Photo 20

Jerome Connolly

Jerome Connolly Photo 21

Jerome Connolly

Publications & IP owners

Us Patents

Structurally-Embedded Electronics Assembly

US Patent:
5184141, Feb 2, 1993
Filed:
Apr 5, 1990
Appl. No.:
7/505757
Inventors:
Jerome J. Connolly - Arlington TX
Michael D. Barrick - Arlington TX
William L. D'Agostino - Irving TX
Gerald F. Thomas - Arlington TX
Thomas W. Williams - Grand Prairie TX
Assignee:
Vought Aircraft Company - Dallas TX
International Classification:
H01Q 1280
H01Q 1420
H01Q 13000
US Classification:
343705
Abstract:
A structurally-embedded electronics assembly is disclosed and includes an outer skin member which is lightly loaded structurally, a primary load-carrying member positioned inboard from the outer skin member, a core member positioned between the primary load-carrying member and the outer skin member, an intermediate skin member positioned between the outer skin member and the core member and an electronics structure positioned between a predetermined two of the members or intermingled with a predetermined number of the members set forth above which are adjacent each other. In another embodiment, a thermally conductive baseplate member is positioned inboard from the primary load-carrying member. In another embodiment, a vibration damping member is positioned inboard from the primary load-carrying member.

Heat Blanket Buffer Assembly

US Patent:
6036464, Mar 14, 2000
Filed:
May 14, 1998
Appl. No.:
9/078792
Inventors:
Maro W. Heimerdinger - Torrance CA
Jerome J. Connolly - Dalworthington Gardens TX
Assignee:
Northrop Grumman Corporation - Los Angeles CA
International Classification:
B29C 7334
B32B 3500
US Classification:
425 11
Abstract:
An apparatus and method is disclosed using a blanket (50) which is an assembly of at least one graphite fiber element of high thermal conductivity and at least one metal sheet element such as a copper sheet element to repair an aircraft structure (10) made of composite fiber materials. The blanket (50) is placed in thermal contact with a silicone rubber heat blanket (22), having an internal heat source, and the aircraft structure, such as composite laminates (12, 14). Use of the blanket (50) increases the rate at which the temperature of the laminates can be elevated to the proper range for repair and transfers heat from hot spots to cold spots to ensure a uniform temperature throughout the laminates.

Isbn (Books And Publications)

Aise-Ce-Bon, A Raccoon

Author:
Jerome P. Connolly
ISBN #:
0817848010

Possible Relatives

David P Connolly  Dean W Connolly  Dale S Connolly  Damien M Connolly  Deborah A Connolly  Dana I Connolly  Daniel Connolly  Jerome A Johnson  Jerome Stancil  Jerome L Johnston 

NOTICE: You may not use BackgroundCheck or the information it provides to make decisions about employment, credit, housing or any other purpose that would require Fair Credit Reporting Act (FCRA) compliance. BackgroundCheck is not a Consumer Reporting Agency (CRA) as defined by the FCRA and does not provide consumer reports.