Patents by Inventor Luis J. Lazaro, Jr.

Luis J. Lazaro, Jr. has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 9300104
    Abstract: An electrical contact insertion tool includes an insertion assembly, a handle assembly slidably coupled to the insertion assembly such that the insertion assembly is translatable between a first position with respect to the handle assembly and a second position with respect to the handle assembly, and a retention mechanism selectively movable between a first configuration and a second configuration. The handle assembly is configured to retain the insertion assembly in the first position with a first predetermined amount of force when the insertion assembly is in the first position. The retention mechanism is configured to retain an object between the retention mechanism and the insertion assembly with a second predetermined amount of force when the retention mechanism is in the second configuration.
    Type: Grant
    Filed: March 20, 2013
    Date of Patent: March 29, 2016
    Assignee: The Boeing Company
    Inventors: Luis J. Lazaro, Jr., Wesley M. Johnson, Curtis A. Davis
  • Patent number: 9263840
    Abstract: An electrical contact insertion tool includes a handle, an insertion tip assembly extending from the handle, a surface probe assembly extending from the handle, and an indicator. The insertion tip assembly is configured to apply a force to an electrical contact to accomplish insertion of the electrical contact into an electrical connector. The surface probe assembly is configured to determine a displacement associated with the insertion tip assembly. The indicator is configured to present an indication of positive electrical contact insertion based at least in part on the force and the displacement associated with the insertion tip assembly.
    Type: Grant
    Filed: March 20, 2013
    Date of Patent: February 16, 2016
    Assignee: The Boeing Company
    Inventors: Luis J. Lazaro, Jr., Wesley M. Johnson, Frederick Boyd McGalliard, III
  • Patent number: 8382523
    Abstract: A cable terminating and grounding apparatus and method comprises a backshell including a cable terminating and grounding adapter shield which comprises a cable receiving and positioning portion comprising a plurality of individual cable passages around the outer rim of the receiving and positioning portion and a gathering portion adjacent the receiving and positioning portion comprising a plurality of individual cable receiving slots around an outer periphery of the gathering portion, each slot having a side wall receiving a cable shield enclosing one or more wires comprising the cable. A gathering mechanism may engage each of the cable shields oppositely from the respective slot side wall and force the respective shield into engagement with the respective slot side wall. There may be a cable passage in a center portion of the receiving and positioning portion and the gathering portion. A locking portion of the adapter shield may engage a connector.
    Type: Grant
    Filed: June 13, 2012
    Date of Patent: February 26, 2013
    Assignee: The Boeing Company
    Inventor: Luis J. Lazaro, Jr.
  • Patent number: 8221164
    Abstract: A cable terminating and grounding apparatus and method may comprise a backshell including a cable terminating and grounding adapter shield which may comprise a cable receiving and positioning portion comprising a plurality of individual cable passages around the outer rim of the receiving and positioning portion; and, a gathering portion adjacent the receiving and positioning portion comprising a plurality of individual cable receiving slots around an outer periphery of the gathering portion, each slot having a side wall receiving a cable shield enclosing one or more wires comprising the cable. A gathering mechanism may engage each of the cable shields oppositely from the respective slot side wall and force the respective shield into engagement with the respective slot side wall. There may be a cable passage in a center portion of the receiving and positioning portion and the gathering portion. A locking portion of the adapter shield may engage a connector.
    Type: Grant
    Filed: October 30, 2009
    Date of Patent: July 17, 2012
    Assignee: The Boeing Company
    Inventor: Luis J. Lazaro, Jr.
  • Patent number: 7252536
    Abstract: A self-aligning coupling apparatus incorporates a first connecting element having a body with a first set of accessory teeth and a second connecting element having a body and a second set of accessory teeth for engagement of the first set. A coupling ring joins the first and second element. The first set of accessory teeth includes spaced indexing teeth having an apex angle less than an apex angle of the remaining teeth of the first set and a height greater than the remaining teeth of the first set. The second set of accessory teeth is has an apex angle complementing the apex angle of the remaining teeth of the first set. The second set of accessory teeth have canals intermediate the teeth to receive the indexing teeth upon joining of the first and second element by the interconnecting coupling.
    Type: Grant
    Filed: November 22, 2005
    Date of Patent: August 7, 2007
    Assignee: The Boeing Company
    Inventors: Luis J. Lazaro, Jr., Brian W. Graebel
  • Patent number: 6986683
    Abstract: A grounding contact member for electrically connecting cooperating metal shells in a coupling comprises a metal band divided along both edges into several spring contact fingers that are bent inwardly into two U-shape portions. The contact member is located in an annular recess around the inside of a coupling ring with the fingers at one end engaging the metal shell on which the coupling ring is mounted and the fingers at the other end engaging the other metal shell to which the coupling ring is connected.
    Type: Grant
    Filed: October 17, 2002
    Date of Patent: January 17, 2006
    Inventor: Luis J. Lazaro, Jr.
  • Patent number: 6846201
    Abstract: A strain relief, modular, self-aligning, corrosion resistant, highly conductive, environmentally sealing cable clamp or “backshell” has a female adapter having a coupling ring at its proximal end which is connected to a rotatable flexible tubing with a split saddle clamp at is distal end and a male adapter which can be a ground or EMI/RFI adapter. This cable clamp, or “backshell”, ensures full engagement on the interfacing accessory teeth, “backshell” and connector, and resistive to environmental hazards, maintains electrical/electronic shielding integrity, improve mechanical reliability and provides form factor capability.
    Type: Grant
    Filed: December 20, 2002
    Date of Patent: January 25, 2005
    Assignee: The Boeing Company
    Inventor: Luis J. Lazaro, Jr.
  • Patent number: 6709274
    Abstract: An aircraft fixed receptacle connector and a ground supply free plug connector used in commercial and military aircraft. This high performance external power connector is capable of operating in the 120 KVA rating to meet the electrical load requirement on today's newer, larger, and higher capacity aircraft. An array of high amperage power contacts and conventional pin and socket relay contacts are used.
    Type: Grant
    Filed: August 7, 2001
    Date of Patent: March 23, 2004
    Assignee: The Boeing Company
    Inventors: Luis J. Lazaro, Jr., David P. Carter
  • Patent number: 6514104
    Abstract: A grounding contact member for electrically connecting cooperating metal shells in a coupling comprises a metal band divided along both edges into several spring contact fingers that are bent inwardly into two U-shape portions. The contact member is located in an annular recess around the inside of a coupling ring with the fingers at one end engaging the metal shell on which the coupling ring is mounted and the fingers at the other end engaging the other metal shell to which the coupling ring is connected.
    Type: Grant
    Filed: August 23, 2000
    Date of Patent: February 4, 2003
    Assignee: The Boeing Company
    Inventor: Luis J. Lazaro, Jr.
  • Patent number: 6406329
    Abstract: An EMI terminating and grounding strain release clamp assembly or “backshell” is provided having male and female component members and coupling intermediate members constructed of conductive metals. Upon coupling of the female and male component members a split metallic ring is compressed and envelopes a termination platform with electrical cable shields enclosed in a BeCu wrap-around band. This joint connection produces an electrical grounding path which provides EMI protection. Assembly of the component parts is accomplished without the aid or use of a tool. A sealing member can be used for environmental protection of the backshell interior parts.
    Type: Grant
    Filed: August 17, 2000
    Date of Patent: June 18, 2002
    Assignee: The Boeing Company
    Inventor: Luis J. Lazaro, Jr.
  • Patent number: 6146204
    Abstract: A grounding contact member for electrically connecting cooperating metal shells in a coupling comprises a metal band divided along both edges into several spring contact fingers that are bent inwardly into two U-shape portions. The contact member is located in an annular recess around the inside of a coupling ring with the fingers at one end engaging the metal shell on which the coupling ring is mounted and the fingers at the other end engaging the other metal shell to which the coupling ring is connected.
    Type: Grant
    Filed: March 3, 1998
    Date of Patent: November 14, 2000
    Assignee: The Boeing Company
    Inventor: Luis J. Lazaro, Jr.
  • Patent number: 6116955
    Abstract: An EMI terminating and grounding strain release clamp assembly or "backshell" is provided having male and female component members and coupling intermediate members constructed of conductive metals. Upon coupling of the female and male component members a split metallic ring is compressed and envelopes a termination platform with electrical cable shields enclosed in a BeCu wrap-around band. This joint connection produces an electrical grounding path which provides EMI protection. Assembly of the component parts is accomplished without the aid or use of a tool. A sealing member can be used for environmental protection of the backshell interior parts.
    Type: Grant
    Filed: September 8, 1998
    Date of Patent: September 12, 2000
    Assignee: The Boeing Company
    Inventor: Luis J. Lazaro, Jr.
  • Patent number: 6048229
    Abstract: An electrical rectangular connector having an expanded range on the lower limit of the environment resisting wire sealing webs, a dielectric hard face socket insert to detect splayed or bent pin contacts, a controlled configuration on the contact retention clips which provides easy insertion and removal on the contacts. Additionally, the modular insert construction of the connector allows flexibility to the wiring system, meaning, the connector can have a signal, power, coaxial or twinaxial or combination circuitry and also a bayonet coupling mechanism assembly using dowel pins and dual helical ramp grooves to retrin the connector halves in the coupled condition. Consequently, a visual indicator consisting of an arrowhead opposite a marker labeled "HOME" provides assurance on a fully coupled plug and receptacle connector.
    Type: Grant
    Filed: July 29, 1999
    Date of Patent: April 11, 2000
    Assignee: The Boeing Company
    Inventor: Luis J. Lazaro, Jr.
  • Patent number: 5989065
    Abstract: An improved MIL-C-26500 type electrical connector having improved environment resisting wire sealing webs, a hard dielectric face socket insert to detect splayed or bent pins, and a controlled configuration of contact retention clips providing improved electrical performance, easy insertion and removal of contacts and improved assembly, serviceability and maintainability. Additionally, the Mil-C-26500 receptacle circular connector having a set of ground wavesprings assembled on the receptacle connector flange to assure a secure ground path on electrically bonded connectors.
    Type: Grant
    Filed: December 8, 1997
    Date of Patent: November 23, 1999
    Assignee: The Boeing Company
    Inventor: Luis J. Lazaro, Jr.
  • Patent number: 5722846
    Abstract: A cable clamp which utilizes a bayonet coupling attachment mechanism when coupled into an electrical connector. Helical ramp grooves formed in the interior of a coupling ring act against bayonet pins mounted on the electrical connector to effect coupling between the two components. A preloaded disc cone shape spring washer becomes effected during the coupling procedure to maintain a no-motion condition on the cable clamp used in high vibration or large shock forces areas. Additionally, a plurality of detent pins are automatically shifted into a holding position at the completion of the coupling action, thereby further contributing to the maintenance of the coupled condition between the cable clamp and electrical connector. Also, a grounding spring is centrally located on the cable clamp body which when coupled to an electrical connector makes interengageable contact thus providing low impedance and additional mechanical strengthening properties to the cable clamp.
    Type: Grant
    Filed: November 4, 1996
    Date of Patent: March 3, 1998
    Assignee: The Boeing Company
    Inventor: Luis J. Lazaro, Jr.
  • Patent number: 5458501
    Abstract: A cable clamp which utilizes a bayonet coupling attachment mechanism when coupled into an electrical connector. Attachment means of the cable clamp may utilize one of the two designs for two airplane general environments, such as the pressurized and unpressurized high vibration areas. Helical ramp grooves formed in the interior of a coupling ring act against bayonet pins mounted on a connector to effect coupling between the two components. A preloaded wavespring washer becomes effective during coupling of a Single Leg cable clamp used in the pressurized area, while a specially tapered spring washers become effective during the coupling procedure to maintain a no-motion condition on a Saddle-type cable clamp used in unpressurized, high vibration areas. Additionally, a plurality of detent pins are automatically shifted into a holding position at the completion of the coupling action, thereby further contributing to the maintenance of the coupled condition between the Saddle-type cable clamp and connector.
    Type: Grant
    Filed: April 15, 1993
    Date of Patent: October 17, 1995
    Assignee: The Boeing Company
    Inventors: Luis J. Lazaro, Jr., Franklin D. Harsch
  • Patent number: 5183413
    Abstract: An electrical connector modularly arrayed wherein electrical contacts either manual or automatic assemble through a grommet assembly into retention clips.
    Type: Grant
    Filed: December 13, 1991
    Date of Patent: February 2, 1993
    Assignee: The Boeing Company
    Inventors: Luis J. Lazaro, Jr., Franklin D. Harsch
  • Patent number: 5099572
    Abstract: An electrical connector modularly arrayed for ease in manual and automatic fabrication and assembly of wire bundle assemblies. Increased structural strength, elimination of snap ring, straight bore inside diameter, the addition of an insert alignment key, and elimination of electrical contact retention clips are features of the present modular electrical connector assembly.
    Type: Grant
    Filed: September 28, 1990
    Date of Patent: March 31, 1992
    Assignee: The Boeing Company
    Inventors: Luis J. Lazaro, Jr., Franklin D. Harsch
  • Patent number: 5088191
    Abstract: An electrical connector modularly arranged wherein electrical contacts either manual or automatic assemble though a grommet assembly into retention clips.
    Type: Grant
    Filed: July 30, 1990
    Date of Patent: February 18, 1992
    Assignee: The Boeing Company
    Inventors: Luis J. Lazaro, Jr., Franklin D. Harsch
  • Patent number: 4981446
    Abstract: An electrical connector modularly arrayed for ease in manual and automatic fabrication and assembly of wire bundle assemblies. Increased structural strength, elimination of snap ring, straight bore inside diameter, the addition of an insert alignment key, and elimination of electrical contact retention clips are features of the present modular electrical connector assembly.
    Type: Grant
    Filed: November 6, 1989
    Date of Patent: January 1, 1991
    Assignee: The Boeing Company
    Inventors: Luis J. Lazaro, Jr., Franklin D. Harsch