Patents by Inventor David Hinkley

David Hinkley 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: 8820359
    Abstract: A fluid storage and transport module includes complex plumbing features such as fluid reservoirs, filters, heat exchangers, three-dimensionally routed tubing, valves, mixing chambers, and exit apertures formed in and on a monolithic common bulk material using an additive rapid prototyping process of depositing multiple layers of rapid prototyping materials without welds, adhesives or compression fittings, being made by a method that minimizes leaks, maximizes packing density of the functional components, and increases the plumbing robustness to leaks.
    Type: Grant
    Filed: October 21, 2008
    Date of Patent: September 2, 2014
    Assignee: The Aerospace Corporation
    Inventor: David A. Hinkley
  • Patent number: 8428925
    Abstract: Method for reducing the time needed to perform geophysical inversion by using simultaneous encoded sources in the simulation steps of the inversion process. The geophysical survey data are prepared by encoding (3) a group of source gathers (1), using for each gather a different encoding signature selected from a set (2) of non-equivalent encoding signatures. Then, the encoded gathers are summed (4) by summing all traces corresponding to the same receiver from each gather, resulting in a simultaneous encoded gather. (Alternatively, the geophysical data are acquired from simultaneously encoded sources.) The simulation steps needed for inversion are then calculated using a particular assumed velocity (or other physical property) model (5) and simultaneously activated encoded sources using the same encoding scheme used on the measured data. The result is an updated physical properties model (6) that may be further updated (7) by additional iterations.
    Type: Grant
    Filed: January 6, 2012
    Date of Patent: April 23, 2013
    Assignee: ExxonMobil Upstream Research Company
    Inventors: Jerome R. Krebs, John E. Anderson, Ramesh Neelamani, Charlie Jing, David Hinkley, Thomas A. Dickens, Christine E. Krohn, Peter Traynin
  • Publication number: 20120109612
    Abstract: Method for reducing the time needed to perform geophysical inversion by using simultaneous encoded sources in the simulation steps of the inversion process. The geophysical survey data are prepared by encoding (3) a group of source gathers (1), using for each gather a different encoding signature selected from a set (2) of non-equivalent encoding signatures. Then, the encoded gathers are summed (4) by summing all traces corresponding to the same receiver from each gather, resulting in a simultaneous encoded gather. (Alternatively, the geophysical data are acquired from simultaneously encoded sources.) The simulation steps needed for inversion are then calculated using a particular assumed velocity (or other physical property) model (5) and simultaneously activated encoded sources using the same encoding scheme used on the measured data. The result is an updated physical properties model (6) that may be further updated (7) by additional iterations.
    Type: Application
    Filed: January 6, 2012
    Publication date: May 3, 2012
    Inventors: Jerome R. Krebs, John E. Anderson, Ramesh Neelamani, Charlie Jing, David Hinkley, Thomas A. Dickens, Christine E. Krohn, Peter Traynin
  • Patent number: 8121823
    Abstract: Method for reducing the time needed to perform geophysical inversion by using simultaneous encoded sources in the simulation steps of the inversion process. The geophysical survey data are prepared by encoding (3) a group of source gathers (1), using for each gather a different encoding signature selected from a set (2) of non-equivalent encoding signatures. Then, the encoded gathers are summed (4) by summing all traces corresponding to the same receiver from each gather, resulting in a simultaneous encoded gather. (Alternatively, the geophysical data are acquired from simultaneously encoded sources.) The simulation steps needed for inversion are then calculated using a particular assumed velocity (or other physical property) model (5) and simultaneously activated encoded sources using the same encoding scheme used on the measured data. The result is an updated physical properties model (6) that may be further updated (7) by additional iterations.
    Type: Grant
    Filed: September 11, 2007
    Date of Patent: February 21, 2012
    Assignee: ExxonMobil Upstream Research Company
    Inventors: Jerome R. Krebs, John E. Anderson, Ramesh Neelamani, Charlie Jing, David Hinkley, Thomas A. Dickens, Christine E. Krohn, Peter Traynin
  • Publication number: 20100096030
    Abstract: A fluid storage and transport module includes complex plumbing features such as fluid reservoirs, filters, heat exchangers, three-dimensionally routed tubing, valves, mixing chambers, and exit apertures formed in and on a monolithic common bulk material using an additive rapid prototyping process of depositing multiple layers of rapid prototyping materials without welds, adhesives or compression fittings, being made by a method that minimizes leaks, maximizes packing density of the functional components, and increases the plumbing robustness to leaks.
    Type: Application
    Filed: October 21, 2008
    Publication date: April 22, 2010
    Inventor: David A. Hinkley
  • Publication number: 20100018718
    Abstract: Method for reducing the time needed to perform geophysical inversion by using simultaneous encoded sources in the simulation steps of the inversion process. The geophysical survey data are prepared by encoding (3) a group of source gathers (1), using for each gather a different encoding signature selected from a set (2) of non-equivalent encoding signatures. Then, the encoded gathers are summed (4) by summing all traces corresponding to the same receiver from each gather, resulting in a simultaneous encoded gather (Alternatively, the geophysical data are acquired from simultaneously encoded sources.) The simulation steps needed for inversion are then calculated using a particular assumed velocity (or other physical property) model (5) and simultaneously activated encoded sources using the same encoding scheme used on the measured data. The result is an updated physical properties model (6) that may be further updated (7) by additional iterations.
    Type: Application
    Filed: September 11, 2007
    Publication date: January 28, 2010
    Inventors: Jerome R. Krebs, John E. Anderson, Ramesh Neelamani, Charlie Jing, David Hinkley, Thomas A. Dickens, Christine E. Krohn, Peter Traynin
  • Patent number: 6889411
    Abstract: A conductive hinge is made of a superelastic shape memory alloy such as nitinol (NiTi) having a large elastic strain limit for enabling the hinge to bend to a small radius during stowage and flexible return to a trained rigid hinge position by training the shape memory alloy to assume a predetermined deployed configuration when released from a stowage configuration. The hinge is trained by forging at a temperature above a training temperature. The hinge is stowed and released in the superelastic state to deploy solar cell panels as the hinges unfold to the trained deployed configuration.
    Type: Grant
    Filed: June 9, 2003
    Date of Patent: May 10, 2005
    Assignee: The Aerospace Corporation
    Inventors: David A. Hinkley, Edward J. Simburger
  • Publication number: 20050011551
    Abstract: A wrap around contact is disposed on the edge of a solar cell panel for providing electrical connections between a thin film solar cell contact and electrical conductors in a flex circuit for routing electrical energy produced by the solar cells to a power bus. The wrap around contact wraps around an edge of a solar cell on top of which is the solar cell contact. Under the solar cell, power bus conductor traces are laser welded to the wrap around contract so as to connect the flex circuit power bus to the silver contact of the thin film solar cell.
    Type: Application
    Filed: July 14, 2003
    Publication date: January 20, 2005
    Inventors: Edward Simburger, David Hinkley, Craig Marshall, Alan Perry, Suraj Rawal
  • Patent number: 6772479
    Abstract: A conductive hinge is made of a superelastic shape memory alloy such as nitinol (NiTi) having a large elastic strain limit for enabling the hinge to bend around a small radius during stowage and flexible return to a trained rigid hinge position. The hinge is conductive enabling use of the hinge as a conductor for routing power through multiple solar cell panels interconnected by the hinges forming a hinged solar cell array that is deployed when the hinges are released from the bent stowed configuration to the rigid deployed configuration when the hinges further function as latches to lock the panels in place.
    Type: Grant
    Filed: June 21, 2001
    Date of Patent: August 10, 2004
    Assignee: The Aerospace Corporation
    Inventors: David A. Hinkley, Edward J. Simburger
  • Publication number: 20030196298
    Abstract: A conductive hinge is made of a superelastic shape memory alloy such as nitinol (NiTi) having a large elastic strain limit for enabling the hinge to bend around a small radius during stowage and flexible return to a trained rigid hinge position. The hinge is conductive enabling use of the hinge as a conductor for routing power through multiple solar cell panels interconnected by the hinges forming a hinged solar cell array that is deployed when the hinges are released from the bent stowed configuration to the rigid deployed configuration when the hinges further function as latches to lock the panels in place.
    Type: Application
    Filed: June 9, 2003
    Publication date: October 23, 2003
    Inventors: David A. Hinkley, Edward J. Simburger
  • Publication number: 20020194702
    Abstract: A conductive hinge is made of a superelastic shape memory alloy such as nitinol (NiTi) having a large elastic strain limit for enabling the hinge to bend around a small radius during stowage and flexible return to a trained rigid hinge position. The hinge is conductive enabling use of the hinge as a conductor for routing power through multiple solar cell panels interconnected by the hinges forming a hinged solar cell array that is deployed when the hinges are released from the bent stowed configuration to the rigid deployed configuration when the hinges further function as latches to lock the panels in place.
    Type: Application
    Filed: June 21, 2001
    Publication date: December 26, 2002
    Applicant: The Aerospace Corporation
    Inventors: David A. Hinkley, Edward J. Simburger
  • Publication number: 20020195177
    Abstract: A conductive hinge is made of a superelastic shape memory alloy such as nitinol (NiTi) having a large elastic strain limit for enabling the hinge to bend to a small radius during stowage for flexible return to a trained rigid hinge position by training the shape memory alloy to assume a predetermined deployed configuration when released from a stowage configuration. The hinge is trained by forging at a temperature above a training temperature. The hinge is released to deploy solar cell panels as the hinges unfold to the forged trained deployed configuration.
    Type: Application
    Filed: June 21, 2001
    Publication date: December 26, 2002
    Applicant: The Aerospace Corporation
    Inventors: David A. Hinkley, Edward J. Simburger
  • Patent number: 6284966
    Abstract: A power sphere preferably used as part of a nanosatellite is formed using a plurality of flat panels solar arrays interconnected together by rotating hinges to approximate a spherical shape for use as an enclosure of a payload. The solar array panels are supported by an extending internal strut. The spherical shape provides attitude insensitive solar energy collection and heat radiation.
    Type: Grant
    Filed: March 6, 2000
    Date of Patent: September 4, 2001
    Assignee: The Aerospace Corporation
    Inventors: Edward J. Simburger, David A. Hinkley, Ernest Y. Robinson, David G. Gilmore, Jon V. Osborn
  • Patent number: 4613960
    Abstract: Disclosed is a method for constructing an optimal pilot trace from a gather of seismic traces, which pilot trace can be used to obtain statics estimates for time correction of the gathered traces prior to common depth point stacking. During construction of the optimal pilot trace, the statics estimates are inherently obtained.
    Type: Grant
    Filed: September 8, 1983
    Date of Patent: September 23, 1986
    Assignee: Mobil Oil Corporation
    Inventors: David Hinkley, Keh Pann
  • Patent number: 4577298
    Abstract: Disclosed is a method for estimating and correcting source and receiver statics contained in recorded and gathered seismic traces. Measurements based on the time of arrival of reflection and refraction signal components in the recorded and gathered traces are used to produce source-receiver statics estimates, which are in turn used to correctly time shift the individual traces of the gather for subsequent common depth point (CDP) gathering and stacking.
    Type: Grant
    Filed: September 8, 1983
    Date of Patent: March 18, 1986
    Assignee: Mobil Oil Corporation
    Inventor: David Hinkley
  • Patent number: 4489239
    Abstract: A portable laser system for remote detection of methane gas leaks and concentrations is disclosed. The system transmitter includes first and second lasers, tuned respectively to a wavelength coincident with a strong absorption line of methane and a reference wavelength which is weakly absorbed by methane gas. The lasers are aimed at a topographical target along a system axis and the beams successively interrupted by a chopper wheel.The system receiver includes a spherical mirror for collecting the reflected laser radiation and focusing the collected radiation through a narrowband optical filter onto an optial detector. The filter is tuned to the wavelength of the two lasers, and rejects background noise to substantially improve the signal-to-noise ratio of the detector. The output of the optical detector is processed by a lock-in detector synchronized to the chopper, and which measures the difference between the first wavelength signal and the reference wavelength signal.
    Type: Grant
    Filed: September 24, 1982
    Date of Patent: December 18, 1984
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William B. Grant, E. David Hinkley, Jr.