Patents by Inventor Anthony Beckman Hays
Anthony Beckman Hays 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).
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Patent number: 8333347Abstract: For each capture mechanism of a plurality of three capture mechanisms, a necked coupling element received by a corresponding socket slides therealong and engages a corresponding latch lever biased in an open position and rotates the latch lever to a closed position as the necked coupling element is slid within the socket towards a bottom thereof. A latch locked biased against the latch lever engages a notch in the latch lever when the latch lever is closed so as to latch the latch lever in the closed position and thereby capture the necked coupling element within the socket. The latch lever is unlatched by releasing the latch lock from engagement with the latch. Different latch levers incorporate different shaped surfaces that engage different corresponding necked coupling elements captured thereby so as to provide for respectively constraining in one, two and three degrees-of-freedom, respectively.Type: GrantFiled: April 16, 2012Date of Patent: December 18, 2012Assignee: Michigan Aerospace CorporationInventors: Greg Alan Ritter, Anthony Beckman Hays, Peter Tchoryk, Jr., Jane Camile Pavlich, Gregory Joseph Wassick
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Publication number: 20120291241Abstract: For each capture mechanism of a plurality of three capture mechanisms, a necked coupling element received by a corresponding socket slides therealong and engages a corresponding latch lever biased in an open position and rotates the latch lever to a closed position as the necked coupling element is slid within the socket towards a bottom thereof. A latch locked biased against the latch lever engages a notch in the latch lever when the latch lever is closed so as to latch the latch lever in the closed position and thereby capture the necked coupling element within the socket. The latch lever is unlatched by releasing the latch lock from engagement with the latch. Different latch levers incorporate different shaped surfaces that engage different corresponding necked coupling elements captured thereby so as to provide for respectively constraining in one, two and three degrees-of-freedom, respectively.Type: ApplicationFiled: April 16, 2012Publication date: November 22, 2012Applicant: MICHIGAN AEROSPACE CORPORATIONInventors: Greg Alan RITTER, Anthony Beckman HAYS, Peter TCHORYK, JR., Jane Camile PAVLICH, Gregory Joseph WASSICK
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Patent number: 8245370Abstract: A capture mechanism provides for receiving a necked coupling element within a socket, providing for the necked coupling element to slide therewith, biasing a latch lever in an open position so as to provide for receiving the necked coupling element within the socket adjacent to the latch lever, rotating the latch lever with the necked coupling element from the open position to a closed position as the necked coupling element is slid within the socket towards a bottom of the socket, biasing a latch lock against the latch lever, engaging the latch lock with the latch lever when the latch lever is in the closed position so as to provide for latching the latch lever in the closed position and capturing the necked coupling element within the socket, and providing for unlatching the latch lever by releasing the latch lock from engagement with the latch lever.Type: GrantFiled: November 2, 2008Date of Patent: August 21, 2012Assignee: Michigan Aerospace CorporationInventors: Greg Alan Ritter, Anthony Beckman Hays, Peter Tchoryk, Jr., Jane Camile Pavlich, Gregory Joseph Wassick
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Patent number: 8240613Abstract: First and second portions of a docking system are releasably connected with one another using at least one latch mechanism that can be reusably released either from the first portion of the docking system or from the second portion of the docking system.Type: GrantFiled: March 23, 2009Date of Patent: August 14, 2012Assignee: Michigan Aerospace CorporationInventors: Greg Alan Ritter, Anthony Beckman Hays, Peter Tchoryk, Jr., Jane Camile Pavlich, Gregory Joseph Wassick
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Patent number: 8056864Abstract: A convex forward surface of a forward-biased probe head of a first portion of a docking system engages a central concave conical surface of a second portion of the docking system. A first linear actuator moves a flexible docking cable assembly relative to a support structure through bores therein and through the probe head. An aftward retraction of the docking cable assembly causes a linearly-actuated cam element thereof to rotate a rotary cam follower pivoted from the support structure, which engages an aft edge portion of the probe head, forcing the probe head forward. A plurality of distal coupling elements operatively coupled to the support structure around a central axis thereof engage with and become releasably captured by a corresponding socket and associated capture mechanism of a mating second portion of the docking system, and rigidized when the probe head is forced against the central concave conical surface.Type: GrantFiled: August 20, 2010Date of Patent: November 15, 2011Assignee: Michigan Aerospace CorporationInventors: Anthony Beckman Hays, Greg Alan Ritter, Peter Tchoryk, Jr., Jane Camile Pavlich, Gregory Joseph Wassick
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Patent number: 7992824Abstract: An end effector operatively coupled to an extendable tensile element extended from a first vehicle engages a primary receptacle of a second vehicle. The first and second vehicles are drawn together by retracting the extendable tensile element into the first vehicle until contact therebetween, after which roll axes of the first and second vehicles become substantially aligned responsive to a further retraction of the extendable tensile element into the first vehicle and a resulting tension in the extendable tensile element. At least one alignment post of at least one of the first and second vehicles engages with at least one surface of at least one corresponding secondary receptacle so as to at least substantially align the first and second vehicles in roll responsive to the tension in the extendable tensile element.Type: GrantFiled: August 9, 2010Date of Patent: August 9, 2011Assignee: Michigan Aerospace CorporationInventors: Peter Tchoryk, Jr., Jane Camile Pavlich, Anthony Beckman Hays, Gregory Joseph Wassick, Greg Alan Ritter
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Publication number: 20110058892Abstract: An end effector operatively coupled to an extendable tensile element extended from a first vehicle engages a primary receptacle of a second vehicle. The first and second vehicles are drawn together by retracting the extendable tensile element into the first vehicle until contact therebetween, after which roll axes of the first and second vehicles become substantially aligned responsive to a further retraction of the extendable tensile element into the first vehicle and a resulting tension in the extendable tensile element. At least one alignment post of at least one of the first and second vehicles engages with at least one surface of at least one corresponding secondary receptacle so as to at least substantially align the first and second vehicles in roll responsive to the tension in the extendable tensile element.Type: ApplicationFiled: August 9, 2010Publication date: March 10, 2011Applicant: MICHIGAN AEROSPACE CORPORATIONInventors: Peter TCHORYK, JR., Jane Camile PAVLICH, Anthony Beckman HAYS, Gregory Joseph WASSICK, Greg RITTER
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Publication number: 20110008102Abstract: A convex forward surface of a forward-biased probe head of a first portion of a docking system engages a central concave conical surface of a second portion of the docking system. A first linear actuator moves a flexible docking cable assembly relative to a support structure through bores therein and through the probe head. An aftward retraction of the docking cable assembly causes a linearly-actuated cam element thereof to rotate a rotary cam follower pivoted from the support structure, which engages an aft edge portion of the probe head, forcing the probe head forward. A plurality of distal coupling elements operatively coupled to the support structure around a central axis thereof engage with and become releasably captured by a corresponding socket and associated capture mechanism of a mating second portion of the docking system, and rigidized when the probe head is forced against the central concave conical surface.Type: ApplicationFiled: August 20, 2010Publication date: January 13, 2011Applicant: MICHIGAN AEROSPACE CORPORATIONInventors: Anthony Beckman HAYS, Greg Alan RITTER, Peter TCHORYK, JR., Jane Camile PAVLICH, Gregory Joseph WASSICK
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Publication number: 20110004717Abstract: First and second portions of a docking system are releasably connected with one another using at least one latch mechanism that can be reusably released either from the first portion of the docking system or from the second portion of the docking system.Type: ApplicationFiled: March 23, 2009Publication date: January 6, 2011Applicant: MICHIGAN AEROSPACE CORPORATIONInventors: Greg Alan Ritter, Anthony Beckman Hays, Peter Tchoryk, JR., Jane Camile Pavlich, Gregory Joseph Wassick
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Patent number: 7861974Abstract: A convex forward surface of a forward-biased probe head of a first portion of a docking system engages a central concave conical surface of a second portion of the docking system. A first linear actuator moves a flexible docking cable assembly relative to a support structure through bores therein and through the probe head. An aftward retraction of the docking cable assembly causes a linearly-actuated cam element thereof to rotate a rotary cam follower pivoted from the support structure, which engages an aft edge portion of the probe head, forcing the probe head forward. A plurality of distal coupling elements operatively coupled to the support structure around a central axis thereof engage with and become releasably captured by a corresponding socket and associated capture mechanism of a mating second portion of the docking system, and rigidized when the probe head is forced against the central concave conical surface.Type: GrantFiled: March 18, 2009Date of Patent: January 4, 2011Assignee: Michigan Aerospace CorporationInventors: Anthony Beckman Hays, Greg Alan Ritter, Peter Tchoryk, Jr., Jane Camile Pavlich, Gregory Joseph Wassick
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Patent number: 7857261Abstract: An automatically aligned docking system, comprises a multi-point kinematic rigidization system that provides precise, repeatable rotational alignment at the spacecraft-docking interface without over-constraining the interface.Type: GrantFiled: September 12, 2006Date of Patent: December 28, 2010Assignee: Michigan Aerospace CorporationInventors: Peter Tchoryk, Jr., Jane Camile Pavlich, Anthony Beckman Hays, Gregory Joseph Wassick, Greg Ritter
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Patent number: 7828249Abstract: First and second releasably connectable portions of a docking system are moved together. A relatively central concave element of the second portion of the docking system contacts a corresponding relatively central mating convex element of the first portion of the docking system. A plurality of relatively distal coupling elements rigidly connected to one of the first and second portions of the docking system are inserted into a corresponding plurality of relatively distal sockets of the other of the first and second portions of the docking system. The plurality of relatively distal coupling elements are captured with a corresponding plurality of relatively distal latch mechanisms associated with the plurality of relatively distal sockets responsive to inserting the plurality of relatively distal coupling elements into the corresponding plurality of relatively distal sockets.Type: GrantFiled: March 23, 2009Date of Patent: November 9, 2010Assignee: Michigan Aerospace CorporationInventors: Greg Alan Ritter, Anthony Beckman Hays, Peter Tchoryk, Jr., Jane Camile Pavlich, Gregory Joseph Wassick
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Publication number: 20090173832Abstract: A convex forward surface of a forward-biased probe head of a first portion of a docking system engages a central concave conical surface of a second portion of the docking system. A first linear actuator moves a flexible docking cable assembly relative to a support structure through bores therein and through the probe head. An aftward retraction of the docking cable assembly causes a linearly-actuated cam element thereof to rotate a rotary cam follower pivoted from the support structure, which engages an aft edge portion of the probe head, forcing the probe head forward. A plurality of distal coupling elements operatively coupled to the support structure around a central axis thereof engage with and become releasably captured by a corresponding socket and associated capture mechanism of a mating second portion of the docking system, and rigidized when the probe head is forced against the central concave conical surface.Type: ApplicationFiled: March 18, 2009Publication date: July 9, 2009Applicant: MICHIGAN AEROSPACE CORPORATIONInventors: Anthony Beckman HAYS, Greg Alan RITTER, Peter TCHORYK, JR., Jane Camile PAVLICH, Gregory Joseph WASSICK
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Publication number: 20090173833Abstract: First and second releasably connectable portions of a docking system are moved together. A relatively central concave element of the second portion of the docking system contacts a corresponding relatively central mating convex element of the first portion of the docking system. A plurality of relatively distal coupling elements rigidly connected to one of the first and second portions of the docking system are inserted into a corresponding plurality of relatively distal sockets of the other of the first and second portions of the docking system. The plurality of relatively distal coupling elements are captured with a corresponding plurality of relatively distal latch mechanisms associated with the plurality of relatively distal sockets responsive to inserting the plurality of relatively distal coupling elements into the corresponding plurality of relatively distal sockets.Type: ApplicationFiled: March 23, 2009Publication date: July 9, 2009Applicant: MICHIGAN AEROSPACE CORPORATIONInventors: Greg Alan RITTER, Anthony Beckman HAYS, Peter TCHORYK, JR., Jane Camile PAVLICH, Gregory Joseph WASSICK
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Publication number: 20090146011Abstract: A capture mechanism provides for receiving a necked coupling element within a socket, providing for the necked coupling element to slide therewith, biasing a latch lever in an open position so as to provide for receiving the necked coupling element within the socket adjacent to the latch lever, rotating the latch lever with the necked coupling element from the open position to a closed position as the necked coupling element is slid within the socket towards a bottom of the socket, biasing a latch lock against the latch lever, engaging the latch lock with the latch lever when the latch lever is in the closed position so as to provide for latching the latch lever in the closed position and capturing the necked coupling element within the socket, and providing for unlatching the latch lever by releasing the latch lock from engagement with the latch lever.Type: ApplicationFiled: November 2, 2008Publication date: June 11, 2009Inventors: Greg Alan RITTER, Anthony Beckman HAYS, Peter TCHORYK, JR., Jane Camile PAVLICH, Gregory Joseph WASSICK
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Patent number: 7522291Abstract: At least one second beam of light from a first beam of light generated by a laser is directed into an atmosphere. Light therefrom scattered by molecules or aerosols in the atmosphere is collected by at least one telescope as at least one light signal, which together with a reference beam from the first beam of light are simultaneously processed by a Fabry-Pérot etalon, and resulting fringe patterns are imaged onto a detector adapted to output a resulting at least one signal responsive thereto.Type: GrantFiled: October 29, 2007Date of Patent: April 21, 2009Assignee: Michigan Aerospace CorporationInventors: Paul Byron Hays, Charles J. Richey, Anthony Beckman Hays, Greg Alan Ritter
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Patent number: 7495774Abstract: A first beam of light from a laser is split by a beam splitter into a reference beam and at least one second beam of light, the latter of which is directed into an atmosphere. Light from the at least one second beam of light scattered by molecules or aerosols in the atmosphere is collected by at least one telescope as at least one light signal. The at least one light signal and the reference beam are simultaneously processed by a common interferometer, and resulting fringe patterns are imaged onto a detector and processed by a data processor to determine at least one associated air data product.Type: GrantFiled: July 27, 2006Date of Patent: February 24, 2009Assignee: Michigan Aerospace CorporationInventors: Paul Byron Hays, Michael Thomas Dehring, Jane Camile Pavlich, Peter Tchoryk, Jr., Charles J. Richey, Anthony Beckman Hays, Gregory Joseph Wassick, Greg Alan Ritter
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Publication number: 20080180691Abstract: At least one second beam of light from a first beam of light generated by a laser is directed into an atmosphere. Light therefrom scattered by molecules or aerosols in the atmosphere is collected by at least one telescope as at least one light signal, which together with a reference beam from the first beam of light are simultaneously processed by a Fabry-Pérot etalon, and resulting fringe patterns are imaged onto a detector adapted to output a resulting at least one signal responsive thereto.Type: ApplicationFiled: October 29, 2007Publication date: July 31, 2008Applicant: MICHIGAN AEROSPACE CORPORATIONInventors: Paul Byron Hays, Michael Thomas Dehring, Jane Camile Pavlich, Peter Tchoryk, Charles J. Richey, Anthony Beckman Hays, Gregory Joseph Wassick, Greg Alan Ritter
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Publication number: 20080180690Abstract: At least one second beam of light from a first beam of light generated by a laser is directed into an atmosphere. Light therefrom scattered by molecules or aerosols in the atmosphere is collected by at least one telescope as at least one light signal, which together with a reference beam from the first beam of light are simultaneously processed by an interferometer, and resulting fringe patterns are imaged onto a detector adapted to output a resulting at least one signal responsive thereto. In various aspects: a data processor gates the signal to provide a range-responsive measurement; the light signal is multiplexed; a circle-to-line interferometer optic transforms an at least partially circular fringe pattern to a substantially linear fringe pattern; or a CCD detector provides for recording a range-resolved image by successively transferring charges from one adjacent row of photosites to another.Type: ApplicationFiled: October 29, 2007Publication date: July 31, 2008Applicant: MICHIGAN AEROSPACE CORPORATIONInventors: Paul Byron HAYS, Michael Thomas Dehring, Jane Camile Pavlich, Peter Tchoryk, Charles J. Richey, Anthony Beckman Hays, Gregory Joseph Wassick, Greg Alan Ritter
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Publication number: 20080117433Abstract: At least one second beam of light from a first beam of light generated by a laser is directed into an atmosphere. Light therefrom scattered by molecules or aerosols in the atmosphere is collected by at least one telescope as at least one light signal, which together with a reference beam from the first beam of light are simultaneously processed by an interferometer, and resulting fringe patterns are imaged onto a detector adapted to output a resulting at least one signal responsive thereto. A data processor determines at least one air data product responsive thereto.Type: ApplicationFiled: October 29, 2007Publication date: May 22, 2008Applicant: MICHIGAN AEROSPACE CORPORATIONInventors: Paul Byron Hays, Michael Thomas Dehring, Jane Camile Pavlich, Peter Tchoryk, Charles J. Richey, Anthony Beckman Hays, Gregory Joseph Wassick, Greg Alan Ritter