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John A Arrell, 91403 School Rd, New London Township, PA 19352

John Arrell Phones & Addresses

403 School Rd, Lincoln University, PA 19352    610-8694990   

451 School Rd, Lincoln University, PA 19352    610-2554498    610-2554646   

57 Pickwick Ln, Lincoln University, PA 19352    610-2554536   

39 Pickwick Ln, Lincoln University, PA 19352   

Lincoln Univ, PA   

New London, PA   

Lincoln Univ, PA   

205 Fox Run Ln, Lincoln University, PA 19352    484-9882355   

Work

Company: Servpro - Philadelphia, PA May 2013 Position: Territory representative

Education

School / High School: West Chester University- West Chester, PA 2002 Specialities: In progress in Business Management

Emails

Mentions for John A Arrell

John Arrell resumes & CV records

Resumes

John Arrell Photo 14

John Arrell

John Arrell Photo 15

John Arrell - Wilmington, DE

Work:
Servpro - Philadelphia, PA May 2013 to Nov 2013
Territory Representative
Versitron Inc - Newark, DE Jan 2011 to Feb 2012
Technical Sales Associate
Sikorsky Global Helicopters Jan 2008 to Feb 2010
Avionics Technician
Outback Steak House - Newark, DE Jan 2001 to Feb 2008
Service Leader
Education:
West Chester University - West Chester, PA 2002 to 2007
In progress in Business Management

Publications & IP owners

Us Patents

Methods And Apparatuses For Electronic Time Delay And Systems Including Same

US Patent:
2008009, May 1, 2008
Filed:
Oct 26, 2006
Appl. No.:
11/553361
Inventors:
John A. Arrell - Lincoln University PA, US
Ronald S. Borja - Newark DE, US
William J. Slade - Newark DE, US
Francois X. Prinz - Henderson NV, US
International Classification:
E21B 43/11
US Classification:
166298, 166 55
Abstract:
Electronic time delay apparatuses and methods of use are disclosed. An explosive or propellant system, which may be configured as a well perforating system includes an electronic time delay assembly comprising an input subassembly, an electronic time delay circuit, and an output subassembly. The input subassembly is activated by an external stimulus, wherein an element is displaced to activate an electronic time delay circuit. The electronic time delay circuit comprises a time delay device coupled with a voltage firing circuit. The electronic time delay circuit counts a time delay, and, upon completion, raises a voltage until a threshold firing voltage is exceeded. Upon exceeding the threshold firing voltage, a voltage trigger switch will break down to transfer energy is to an electric initiator to initiate an explosive booster within the output subassembly. The explosive booster provides the detonation output to initiate the next element explosive or propellant element, such as an array of shaped charges in the well perforating system.

Methods And Apparatuses For Electronic Time Delay And Systems Including Same

US Patent:
2008011, May 15, 2008
Filed:
Oct 23, 2007
Appl. No.:
11/876841
Inventors:
Francois X. Prinz - Henderson NV, US
John A. Arrell - Lincoln University PA, US
Ronald S. Borja - Newark DE, US
William J. Slade - Newark DE, US
International Classification:
E21B 29/02
US Classification:
166 552, 102276, 102222
Abstract:
Electronic time delay apparatuses and methods of use are disclosed. An explosive or propellant system, which may be configured as a well perforating system includes an electronic time delay assembly comprising an input subassembly, an electronic time delay circuit, and an output subassembly. The input subassembly is activated by an external stimulus, wherein an element is displaced to activate an electronic time delay circuit. The electronic time delay circuit comprises a time delay device coupled with a voltage firing circuit. The electronic time delay circuit counts a time delay, and, upon completion, raises a voltage until a threshold firing voltage is exceeded. Upon exceeding the threshold firing voltage, a voltage trigger switch will break down to transfer energy is to an electric initiator to initiate an explosive booster within the output subassembly. The explosive booster provides the detonation output to initiate the next element explosive or propellant element, such as an array of shaped charges in the well perforating system.

Low Cost Hermetically Sealed Squib

US Patent:
5230287, Jul 27, 1993
Filed:
Apr 16, 1991
Appl. No.:
7/686187
Inventors:
John A. Arrell - Lincoln University PA
Peter L. Atkeson - Elkton MD
John W. Cooper - Eagleville PA
Paul P. Hebert - Bear DE
Assignee:
Thiokol Corporation - Ogden UT
International Classification:
F42C 1912
US Classification:
1022025
Abstract:
An electrically actuated igniter squib is formed by welding a cup containing a pyrotechnic material to a header inserted in the cup, thus forming a hermetic seal. The diameter of the header exceeds the diameter of the cup and the two are joined by forcing, under pressure, the header into the cup to achieve a tight readily welded joint.

Low Cost Hermetically Sealed Squib

US Patent:
5431101, Jul 11, 1995
Filed:
Oct 22, 1992
Appl. No.:
7/964636
Inventors:
John A. Arrell - Lincoln University PA
Peter L. Atkeson - Newark DE
John W. Cooper - Newark DE
Paul P. Hebert - Bear DE
Assignee:
Thiokol Corporation - Ogden UT
International Classification:
F42C 1912
US Classification:
1022025
Abstract:
An electrically actuated igniter squib is formed by welding a cup containing a pyrotechnic material to a header inserted in the cup, thus forming a hermetic seal. The diameter of the header exceeds the diameter of the cup and the two are joined by forcing, under pressure, the header into the cup to achieve a tight readily welded joint.

Propellant-Powered Fluid Jet Cutting Apparatus And Methods Of Use

US Patent:
2004008, May 13, 2004
Filed:
Nov 13, 2002
Appl. No.:
10/294473
Inventors:
William Slade - Newark DE, US
Brian LeCompte - Havre De Grace MD, US
John Arrell - Lincoln University PA, US
International Classification:
E21B029/10
US Classification:
166/298000, 166/055700, 166/223000
Abstract:
Apparatus providing at least one high pressure fluid cutting jet and methods employing same. A gas generator powered by a combustible propellant supplies pressurized gas to propel a fluid through at least one nozzle to form a cutting jet suitable for cutting materials such as structural elements. Furthermore, nozzles may be configured to rotate in order to circumferentially sever a tubular structural element. Two or more fluid cutting jets may be configured to intersect, and may be configured to intersect proximate to at least a portion of the periphery of the tubular structural element to be severed.

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