Patents Assigned to Ensign-Bickford Aerospace & Defense Company
  • Publication number: 20160223310
    Abstract: A remote detonator system is provided. The remote detonator system includes a receiver and a transmitter. The receiver includes a transducer configured to receive an ultrasonic acoustic signal. The transducer is electrically coupled to a first controller, the first controller having a processor responsive to executable computer instructions for detonating a charge in response to the transducer receiving the ultrasonic acoustic signal. A transmitter is provided having a transmitter configured to selectively emit the ultrasonic acoustic signal in response to an actuation by an operator.
    Type: Application
    Filed: March 5, 2014
    Publication date: August 4, 2016
    Applicant: Ensign-Bickford Aerospace & Defense Company
    Inventors: Marc A. Morris, Karl Edminster, Andrew DeMedeiros, Stephen W. Bartholomew
  • Patent number: 9309832
    Abstract: A rocket having a motor with a user adjustable thrust is provided. The rocket includes a main cylinder containing a rocket propellant, the propellant configured to generate gas during operation and one or more nozzles arranged to direct the gas in a first direction. A thrust adjustment device is arranged to receive a portion of the gas, the thrust adjustment device configured to change the direction of flow of at least a portion of the gas.
    Type: Grant
    Filed: June 29, 2012
    Date of Patent: April 12, 2016
    Assignee: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY
    Inventors: Andrew M. Kochanek, Kurt Nelson, Daniel P. Sutula, Jr.
  • Patent number: 9134100
    Abstract: A semiconductor bridge die may have an “H-design” or “trapezoidal” configuration in which a center bridge segment is flanked by one or more angled walls on each side of the bridge segment. Each wall is plated with a conductive material, thereby providing a continuous conductive path across the top surface of the die. A bottom surface of the die may be connected to a top surface of a header by epoxy in various configurations. The plated angled walls facilitate the solderable connection of the walls to a plated top surface of each of several pins on a top surface of the header, thereby providing a continuous electrical connection between the pins and the die. Also, a method is provided for manufacturing a semiconductor bridge die in accordance with the various embodiments of the die.
    Type: Grant
    Filed: April 6, 2010
    Date of Patent: September 15, 2015
    Assignee: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY
    Inventors: Bernardo Martinez-Tovar, Craig J. Boucher
  • Patent number: 8727654
    Abstract: A system for separating a first component and a second component is provided. The system includes a first joinder flange having at least one first fastener feature for coupling the first joinder flange to the first component. A second joinder flange is provided having at least one second fastener feature for coupling the second joinder flange to the second component. A separation portion is coupled between the first joinder flange and the second joinder flange, the frangible joint having at least one groove extending along width of the separation portion. An explosive member is arranged adjacent the separation portion. Wherein the first joinder flange includes at least one integral shock attenuation feature formed therein between the explosive member and the at least one first fastener feature.
    Type: Grant
    Filed: May 29, 2012
    Date of Patent: May 20, 2014
    Assignee: Ensign-Bickford Aerospace & Defense Company
    Inventor: John A. Graham
  • Patent number: 8695473
    Abstract: An elastomeric charge holder includes one or more holes formed therein into which is disposed an explosive charge. The elastomeric charge holder further includes one or more metal wires also disposed within the elastomeric charge holder. The elastomeric charge holder may be over molded or over extruded over each of the one or more metal wires, thereby retaining each of the one or more wires in place during use of the elastomeric charge holder. The one or more wires are also a better match of thermal coefficients to a metal confinement tube that holds the elastomeric charge holder, which results in improved retention of the elastomeric charge holder in place, particularly during initiation of the explosive charge.
    Type: Grant
    Filed: March 7, 2012
    Date of Patent: April 15, 2014
    Assignee: Ensign-Bickford Aerospace & Defense Company
    Inventors: David Kametz, Kevin Duprey
  • Publication number: 20140007554
    Abstract: A rocket having a motor with a user adjustable thrust is provided. The rocket includes a main cylinder containing a rocket propellant, the propellant configured to generate gas during operation and one or more nozzles arranged to direct the gas in a first direction.
    Type: Application
    Filed: June 29, 2012
    Publication date: January 9, 2014
    Applicant: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY
    Inventors: Andrew M. Kochanek, Kurt Nelson, Daniel P. Sutula, JR.
  • Patent number: 8608878
    Abstract: A heat generating structure includes a substrate, a coating and a polymeric material. The substrate comprises a first material. The coating comprises a second material, different from the first material that covers at least a portion of the substrate. The coating and substrate, upon being thermally energized to their minimum alloying temperature, react in a first exothermic reaction that is an alloying reaction. The relative quantities of the substrate and coating are such that the first exothermic reaction yields a first amount of exothermic energy that is insufficient to cause self-sustained propagation of the first exothermic reaction. The polymeric material covers substantially all of the substrate and coating, and is different from the first and second materials. The polymeric layer, upon being thermally energized, reacts with at least one of the substrate and coating in a second exothermic reaction.
    Type: Grant
    Filed: September 8, 2010
    Date of Patent: December 17, 2013
    Assignee: Ensign-Bickford Aerospace & Defense Company
    Inventors: Richard M. Kellett, David F. Irwin
  • Publication number: 20130236234
    Abstract: A frangible joint for separating a pair of components is provided. The frangible joint includes a first portion coupled one of the pair of components and a second portion coupled to the other of the pair of components. The first portion and the second portion are spaced apart by a gap. At least one plate is coupled between the first portion and the second portion across the gap. A first tube having a first explosive cord is disposed therein and a first pliable member arranged between the first explosive cord and the first tube, the first tube being disposed in the gap. A second tube having a second explosive cord is disposed therein and a second pliable member arranged between the second explosive cord and the second tube, the second tube being disposed in the gap adjacent the first tube.
    Type: Application
    Filed: April 9, 2012
    Publication date: September 12, 2013
    Applicant: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY
    Inventor: Geoffrey Paul Kaczynski
  • Publication number: 20130233161
    Abstract: An elastomeric charge holder includes one or more holes formed therein into which is disposed an explosive charge. The elastomeric charge holder further includes one or more metal wires also disposed within the elastomeric charge holder. The elastomeric charge holder may be over molded or over extruded over each of the one or more metal wires, thereby retaining each of the one or more wires in place during use of the elastomeric charge holder. The one or more wires are also a better match of thermal coefficients to a metal confinement tube that holds the elastomeric charge holder, which results in improved retention of the elastomeric charge holder in place, particularly during initiation of the explosive charge.
    Type: Application
    Filed: March 7, 2012
    Publication date: September 12, 2013
    Applicant: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY
    Inventors: David Kametz, Kevin Duprey
  • Publication number: 20130136525
    Abstract: A system for separating a first component and a second component is provided. The system includes a first joinder flange having at least one first fastener feature for coupling the first joinder flange to the first component. A second joinder flange is provided having at least one second fastener feature for coupling the second joinder flange to the second component. A separation portion is coupled between the first joinder flange and the second joinder flange, the frangible joint having at least one groove extending along width of the separation portion. An explosive member is arranged adjacent the separation portion. Wherein the first joinder flange includes at least one integral shock attenuation feature formed therein between the explosive member and the at least one first fastener feature.
    Type: Application
    Filed: May 29, 2012
    Publication date: May 30, 2013
    Applicant: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY
    Inventor: John A. Graham
  • Publication number: 20120061520
    Abstract: A frangible joint structure includes shock attenuation features formed as an integral part of the joint structure. Shock attenuation is achieved through use of, for example, slots or grooves that are machined directly, or otherwise formed integrally, into the frangible joint structure. Adequate shock attenuation is achieved solely by the features machined or otherwise formed in the frangible joint together with the typical assembly of the frangible joint into various structures (e.g., as a payload separator for rockets, missiles, satellites, etc.), without the need for additional hardware components and thus without the need for assembly of the frangible joint shock attenuation device.
    Type: Application
    Filed: July 13, 2009
    Publication date: March 15, 2012
    Applicant: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY
    Inventor: John A. Graham
  • Publication number: 20120055594
    Abstract: A heat generating structure includes a substrate, a coating and a polymeric material. The substrate comprises a first material. The coating comprises a second material, different from the first material that covers at least a portion of the substrate. The coating and substrate, upon being thermally energized to their minimum alloying temperature, react in a first exothermic reaction that is an alloying reaction. The relative quantities of the substrate and coating are such that the first exothermic reaction yields a first amount of exothermic energy that is insufficient to cause self-sustained propagation of the first exothermic reaction. The polymeric material covers substantially all of the substrate and coating, and is different from the first and second materials. The polymeric layer, upon being thermally energized, reacts with at least one of the substrate and coating in a second exothermic reaction.
    Type: Application
    Filed: September 8, 2010
    Publication date: March 8, 2012
    Applicant: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY
    Inventors: Richard M. Kellett, David F. Irwin
  • Patent number: 7987787
    Abstract: An electronic ignition safety device configured to reject signals below a predetermined ‘all-fire’ voltage comprising an exploding foil initiator having an electrical input and an output end, a pickup comprising a secondary explosive donor charge adjacent to the exploding foil initiator's output end and separated from a secondary explosive acceptor charge by an integral barrier, and an output charge adjacent to the acceptor charge.
    Type: Grant
    Filed: March 7, 2007
    Date of Patent: August 2, 2011
    Assignee: Ensign-Bickford Aerospace & Defense Company
    Inventor: John A. Sudick
  • Patent number: 7930976
    Abstract: A structure includes a substrate of a first material and a second material coating at least a portion of the substrate, where the second material is different from the first material, where the first and second materials, upon being thermally energized, react with each other in an exothermic and self-sustaining alloying reaction that propagates from a first location within the structure along a travel path to a second location within the structure at a rate that depends upon one or more characteristics of the first and second materials.
    Type: Grant
    Filed: August 2, 2007
    Date of Patent: April 26, 2011
    Assignee: Ensign-Bickford Aerospace & Defense Company
    Inventors: Richard M. Kellett, Carl F. Mallery, Jr., Robert B. Korcsmaros
  • Patent number: 7921776
    Abstract: This invention relates to a detonating cord (10) having a core (12) of reactive material and a composite jacket around the core, and the method of its manufacture. The composite jacket includes an interior jacket (14) in contact with the core and a sacrificial jacket (20) disposed over the interior jacket. The sacrificial jacket prevents the cord from being cut off by the detonation of another detonating cord of like core load disposed adjacent thereto. The sacrificial jacket is separable from the interior jacket beneath it under the force of the adjacent detonating cord, thus absorbing energy and allowing the first detonating cord to remain intact. The detonating cord may have a core load of not more than 3.2 grams/meter (15 grains/ft) or, optionally, less than 1.25 g/m (6 grains/ft). The interior jacket may be free of metal jacket layers. Optionally, the outer cross-sectional diameter of the cord may be not more than about 3.8 mm (0.15 inch) so that it can be inserted into a standard detonator.
    Type: Grant
    Filed: June 1, 2004
    Date of Patent: April 12, 2011
    Assignee: Ensign-Bickford Aerospace & Defense Company
    Inventors: Brendan M. Walsh, P. Cary Franklin
  • Publication number: 20100258914
    Abstract: A semiconductor bridge die may have an “H-design” or “trapezoidal” configuration in which a center bridge segment is flanked by one or more angled walls on each side of the bridge segment. Each wall is plated with a conductive material, thereby providing a continuous conductive path across the top surface of the die. A bottom surface of the die may be connected to a top surface of a header by epoxy in various configurations. The plated angled walls facilitate the solderable connection of the walls to a plated top surface of each of several pins on a top surface of the header, thereby providing a continuous electrical connection between the pins and the die. Also, a method is provided for manufacturing a semiconductor bridge die in accordance with the various embodiments of the die.
    Type: Application
    Filed: April 6, 2010
    Publication date: October 14, 2010
    Applicant: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY
    Inventors: Bernardo Martinez-Tovar, Craig J. Boucher
  • Patent number: 7804223
    Abstract: An efficient piezoelectric-triggered time delay module may be provided with separate firing and logic capacitors, and may also have corresponding separate piezoelectric transducers. Further, separate firing and logic capacitors may be impedance-matched to corresponding separate piezoelectric transducers. Optionally, the capacitors may be made of the same materials as the corresponding piezoelectric transducers. Further alternately or additionally, low-value, high-voltage rated capacitor(s) may be employed. Further alternately or additionally, the piezoelectric transducer(s) may be selected to offer high charge output within the intended operating temperature range. Further alternately or additionally, the piezoelectric transducer(s) may be constructed with multiple wafers.
    Type: Grant
    Filed: April 16, 2007
    Date of Patent: September 28, 2010
    Assignee: Ensign-Bickford Aerospace & Defense Company
    Inventor: Gimtong Teowee
  • Publication number: 20100043661
    Abstract: An explosive cutting charge is formed by machining or otherwise forming a cavity of a desired configuration within a circular ring of metal cutting material such as copper or aluminum. The cavity may then be filled with an explosive material. The cutting characteristics of the cutting charge may be controlled by the selected cross-section configuration of the cavity. The ring may contain a booster explosive charge with connections to the active portion of the ring having the cutting metal material.
    Type: Application
    Filed: August 20, 2009
    Publication date: February 25, 2010
    Applicant: ENSIGN-BICKFORD AEROSPACE & DEFENSE COMPANY
    Inventor: John A. Graham
  • Patent number: 7650993
    Abstract: A coreless-coil shock tube package system includes a “coreless” bundle of shock tubing, meaning that the tubing is not wrapped around a spool. The bundle may be a generally cylindrical coil of shock tubing. Optionally, two washer-like end plates abut the ends of the tubing coil for axial support. A layer of shrink-wrap or other polymer film partially covers the coil and end plates. A detonator is attached to one end of the tubing and lies tucked into the coil, through an end plate, for storage and transport. An igniter is attached to the tubing's other end. In use, the detonator is removed from the coil and attached to an explosive device. Then, the package is pulled away from the detonator and explosive, thereby uncoiling the tubing through the end plate for deployment. The igniter is actuated for igniting the shock tubing and activating the detonator and explosive.
    Type: Grant
    Filed: August 12, 2005
    Date of Patent: January 26, 2010
    Assignee: Ensign-Bickford Aerospace & Defense Company
    Inventor: A. Jonathan Bawabe
  • Publication number: 20090090440
    Abstract: The compositions of different energetic metallic particles and corresponding coatings are chosen to take advantage of the resulting exothermic alloying reactions when the metals are combined or alloyed through heat activation. Bimetallic particles composed of a core/shell structure of differing metals are chosen such that, upon achieving the melt point for at least one of the metals, a relatively substantial amount of exothermic heat of alloying is liberated. In an embodiment, the core metal is aluminum and the shell metal is nickel. The nickel may be applied to the outer surface of the aluminum particles using an electroless process from a metal salt solution with a reducing agent in an aqueous solution or a solvent media. The aluminum particles may be pretreated with zinc to remove any aluminum oxide. The resulting bimetallic particles may be utilized as an enhanced blast additive by being dispersed within an explosive material.
    Type: Application
    Filed: October 4, 2007
    Publication date: April 9, 2009
    Applicant: Ensign-Bickford Aerospace & Defense Company
    Inventor: Richard M. Kellett