Patents by Inventor Richard P. Wells
Richard P. Wells 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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Publication number: 20230067936Abstract: An apparatus includes a satellite in the form of a plate having a thickness being smaller than a width of the satellite. The apparatus also includes a plurality of contact points distributed on a face of the satellite, allowing for one or more additional satellites to be stacked upon the satellite.Type: ApplicationFiled: October 19, 2022Publication date: March 2, 2023Applicant: The Aerospace CorporationInventor: Richard P. Welle
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Patent number: 11492147Abstract: An apparatus includes a satellite in the form of a plate having a thickness being smaller than a width of the satellite. The apparatus also includes a plurality of contact points distributed on a face of the satellite, allowing for one or more additional satellites to be stacked upon the satellite.Type: GrantFiled: July 30, 2020Date of Patent: November 8, 2022Assignee: THE AEROSPACE CORPORATIONInventor: Richard P. Welle
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Patent number: 11212187Abstract: A communications network comprising of n-hop local neighborhoods. The network includes a plurality of communication nodes and a plurality of local neighborhoods wherein each local neighborhood includes a central node around which the local neighborhood is defined. The network also includes a subset of the plurality of nodes located within the local neighborhoods of each of the central nodes. Each of the subset of the plurality of nodes in a local neighborhood is not more than n hops away over currently existing links from the central node of the local neighborhood.Type: GrantFiled: August 11, 2020Date of Patent: December 28, 2021Assignee: THE AEROSPACE CORPORATIONInventor: Richard P. Welle
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Patent number: 11161630Abstract: A free-floating spherical gimbal (“gimbal”) that includes a moving portion substantially spherical in shape and partially enclosed within a larger spherical and stationary cavity. The moving portion of the spherical gimbal is maintained in a location without direct mechanical contact with the stationary cavity.Type: GrantFiled: January 14, 2020Date of Patent: November 2, 2021Assignee: THE AEROSPACE CORPORATIONInventor: Richard P. Welle
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Patent number: 10763967Abstract: An apparatus for simultaneously receiving and transmitting data in space may include a receiver configured to receive an incoming beam transmitted from a source along a receive vector between the source and the receiver. The apparatus may also include a transmitter to generate a transmitted beam along a transmit vector. The apparatus may further include a single-axis gimbal configured to rotate the transmit vector about an axis substantially perpendicular to the receive vector, and an attitude-control system configured to rotate the apparatus about an axis parallel to the receive vector or the transmit vector.Type: GrantFiled: June 5, 2019Date of Patent: September 1, 2020Assignee: The Aerospace CorporationInventor: Richard P. Welle
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Patent number: 10484095Abstract: An apparatus for simultaneously receiving and transmitting data in space may include a receiver configured to receive an incoming beam transmitted from a source along a receive vector between the source and the receiver. The apparatus may also include a transmitter to generate a transmitted beam along a transmit vector. The apparatus may further include a single-axis gimbal configured to rotate the transmit vector about an axis substantially perpendicular to the receive vector, and an attitude-control system configured to rotate the apparatus about an axis parallel to the receive vector or the transmit vector.Type: GrantFiled: June 15, 2017Date of Patent: November 19, 2019Assignee: The Aerospace CorporationInventor: Richard P. Welle
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Publication number: 20180367216Abstract: An apparatus for simultaneously receiving and transmitting data in space may include a receiver configured to receive an incoming beam transmitted from a source along a receive vector between the source and the receiver. The apparatus may also include a transmitter to generate a transmitted beam along a transmit vector. The apparatus may further include a single-axis gimbal configured to rotate the transmit vector about an axis substantially perpendicular to the receive vector, and an attitude-control system configured to rotate the apparatus about an axis parallel to the receive vector or the transmit vector.Type: ApplicationFiled: June 15, 2017Publication date: December 20, 2018Inventor: Richard P. Welle
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Patent number: 10142012Abstract: A dedicated satellite to reduce the cost and increase the rate and reliability of data transmission from space to ground is provided. For each client satellite producing data in Earth orbit, a dedicated relay satellite is provided. The relay satellite may fly near the client satellite and receive data from the client satellite by RF communication. The relay satellite may transmit the data to a ground terminal or to another satellite using a laser communication system. Because the relay satellite is not physically connected to the client satellite, the attitude-control requirements of an optical communication system are not imposed on the client satellite. The relay satellite may also be deployed from the client satellite. The relay satellite may allow downlinking large amounts of data for new satellite operators without an existing ground network and for established satellite operators seeking higher data rates, lower latency, or reduced ground system operating costs.Type: GrantFiled: March 11, 2016Date of Patent: November 27, 2018Assignee: THE AEROSPACE CORPORATIONInventor: Richard P. Welle
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Patent number: 9941967Abstract: A system for reducing the cost and increasing the rate and reliability of data transmission from space to ground includes a network of relay satellites in low Earth orbit (LEO). Each relay satellite is configured to receive data from one or more client satellites, and configured to transmit data from LEO to ground using optical communications. The system may also include multiple optical ground stations configured to receive the data and transmit the received data using terrestrial networks to client locations. The network may provide an alternative to downlinking large amounts of data for new satellite operators without an existing ground network and for established satellite operators seeking higher data rates, lower latency, or reduced ground system operating costs.Type: GrantFiled: March 11, 2016Date of Patent: April 10, 2018Assignee: THE AEROSPACE CORPORATIONInventors: Richard P. Welle, Siegfried W. Janson, Roger Yang, John Serafini
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Patent number: 9468867Abstract: A microfluidic device is provided for inducing the separation of constituent elements from a microfluidic sample by introducing phase changes in the microfluidic sample while contained in a microfluidic channel in the device. At least a portion of the microfluidic sample is frozen to cause fractional exclusion of the constituent element from the frozen portion of the microfluidic sample. Different portions of the microfluidic sample may be frozen in different sectors and at different times in order to cause movement in a desired direction of the separated constituent element. Portions of the microfluidic sample may be frozen in a sequential order of adjacent sectors within the microfluidic channel in order to cause sequential movement of the excluded constituent element toward one portion of the microfluidic channel. The frozen portion of the microfluidic sample is then thawed, wherein the separated constituent element remains substantially separated from the thawed, purified microfluidic sample.Type: GrantFiled: December 24, 2013Date of Patent: October 18, 2016Assignee: The Aerospace CorporationInventor: Richard P. Welle
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Patent number: 8642353Abstract: A microfluidic device is provided for inducing the separation of constituent elements from a microfluidic sample by introducing phase changes in the microfluidic sample while contained in a microfluidic channel in the device. At least a portion of the microfluidic sample is frozen to cause fractional exclusion of the constituent element from the frozen portion of the microfluidic sample. Different portions of the microfluidic sample may be frozen in different sectors and at different times in order to cause movement in a desired direction of the separated constituent element. Portions of the microfluidic sample may be frozen in a sequential order of adjacent sectors within the microfluidic channel in order to cause sequential movement of the excluded constituent element toward one portion of the microfluidic channel. The frozen portion of the microfluidic sample is then thawed, wherein the separated constituent element remains substantially separated from the thawed, purified microfluidic sample.Type: GrantFiled: March 22, 2007Date of Patent: February 4, 2014Assignee: The Aerospace CorporationInventor: Richard P. Welle
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Patent number: 8245731Abstract: A fluid transport/containment apparatus includes a fluid-bearing module and an actuation module. The fluid-bearing module includes a substrate and fluid transport/containment elements distributed therein, with one or more of the fluid transport/containment elements having microfluidic dimensions. The actuation module is detachably secured to the fluid-bearing module such that the actuation elements are operatively interfaced with the fluid transport/containment elements.Type: GrantFiled: July 19, 2010Date of Patent: August 21, 2012Assignee: The Aerospace CorporationInventor: Richard P. Welle
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Patent number: 8240336Abstract: A valve apparatus includes a substrate, a main flow channel formed in the substrate, a control channel formed in the substrate such that the main flow channel and the control channel meet at a junction, a bi-phase material within the control channel, a heating element adjacent the control channel and the junction, the heating element being controllable to generate sufficient energy to cause the bi-phase material to transition from a solid phase to a liquid phase, and a pumping mechanism for forcing the bi-phase material either into or out of the junction when the bi-phase material is in the liquid phase.Type: GrantFiled: April 13, 2010Date of Patent: August 14, 2012Assignee: The Aerospace CorporationInventor: Richard P. Welle
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Patent number: 8158433Abstract: The present invention relates to identification tagging, and is specifically directed to identification tagging of ammunition. An isotopic taggant is deposited in a layer at the interface between the primer and the propellant so that, as the ammunition is fired, the taggant is dispersed throughout the propellant. The taggant is thus contained in the gunshot residue formed during the firing, and can be read by analysis of residue particles. Alternatively, the taggant may be deposited in a layer under the primer reactants, or in pellets which are easily destroyed by the chemical reactions involved in firing the ammunition, again dispersing the taggant throughout the propellant and the gunshot residue. Non-isotopic chemical taggants may also be employed if they are encoded so as to minimize the possibility of the information being destroyed or improperly read after the taggants are exposed to the chemical reactions in firing the ammunition.Type: GrantFiled: September 18, 2006Date of Patent: April 17, 2012Inventor: Richard P Welle
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Patent number: 8156964Abstract: Embodiments of valve apparatuses are described.Type: GrantFiled: May 24, 2010Date of Patent: April 17, 2012Assignee: The Aerospace CorporationInventor: Richard P. Welle
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Patent number: 8066031Abstract: A microfluidic device includes a substrate including multiple electro-hydraulic valves and/or electro-hydraulic pumps that each include a flow channel and one or more hydraulic control channels, actuators for controlling the electro-hydraulic valves and/or electro-hydraulic pumps, and a hydraulic pressure source operatively connected to the hydraulic control channels.Type: GrantFiled: March 29, 2010Date of Patent: November 29, 2011Assignee: The Aerospace CorporationInventor: Richard P. Welle
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Publication number: 20110210082Abstract: A microfluidic device is provided for inducing the separation of constituent elements from a microfluidic sample by introducing phase changes in the microfluidic sample while contained in a microfluidic channel in the device. At least a portion of the microfluidic sample is frozen to cause fractional exclusion of the constituent element from the frozen portion of the microfluidic sample. Different portions of the microfluidic sample may be frozen in different sectors and at different times in order to cause movement in a desired direction of the separated constituent element. Portions of the microfluidic sample may be frozen in a sequential order of adjacent sectors within the microfluidic channel in order to cause sequential movement of the excluded constituent element toward one portion of the microfluidic channel. The frozen portion of the microfluidic sample is then thawed, wherein the separated constituent element remains substantially separated from the thawed, purified microfluidic sample.Type: ApplicationFiled: March 22, 2007Publication date: September 1, 2011Inventor: Richard P. Welle
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Publication number: 20110100495Abstract: A fluid transport/containment apparatus includes a fluid-bearing module and an actuation module. The fluid-bearing module includes a substrate and fluid transport/containment elements distributed therein, with one or more of the fluid transport/containment elements having microfluidic dimensions. The actuation module is detachably secured to the fluid-bearing module such that the actuation elements are operatively interfaced with the fluid transport/containment elements.Type: ApplicationFiled: July 19, 2010Publication date: May 5, 2011Inventor: Richard P. Welle
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Patent number: 7861538Abstract: A refrigerator apparatus includes a housing with an interior chamber, thermoelectric devices that are thermally coupled to the interior chamber, and dual redundant electronics configured to generate and apply input power to the thermoelectric devices.Type: GrantFiled: July 26, 2006Date of Patent: January 4, 2011Assignee: The Aerospace CorporationInventors: Richard P. Welle, Siegfried W. Janson
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Publication number: 20100258718Abstract: The present invention relates to identification tagging, and is specifically directed to identification tagging of ammunition. An isotopic taggant is deposited in a layer at the interface between the primer and the propellant so that, as the ammunition is fired, the taggant is dispersed throughout the propellant. The taggant is thus contained in the gunshot residue formed during the firing, and can be read by analysis of residue particles. Alternatively, the taggant may be deposited in a layer under the primer reactants, or in pellets which are easily destroyed by the chemical reactions involved in firing the ammunition, again dispersing the taggant throughout the propellant and the gunshot residue. Non-isotopic chemical taggants may also be employed if they are encoded so as to minimize the possibility of the information being destroyed or improperly read after the taggants are exposed to the chemical reactions in firing the ammunition.Type: ApplicationFiled: September 18, 2006Publication date: October 14, 2010Inventor: Richard P. Welle