Patents by Inventor Timothy M. Davis
Timothy M. Davis 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: 12271452Abstract: Apparatus, systems, methods, and articles of manufacture related to end-point media watermarking are disclosed. An example device includes a media receiver to receive a media signal, a watermark generator to generate a watermark, a trigger to activate the watermark generator to generate the watermark based on an external input, an encoder to encode the media signal with the watermark to synthesize an encoded media signal, a media output to render the encoded media signal.Type: GrantFiled: April 19, 2024Date of Patent: April 8, 2025Assignee: The Nielsen Company (US), LLCInventors: Arun Ramaswamy, Timothy Scott Cooper, Jeremey M. Davis, Alexander Topchy
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Patent number: 12246429Abstract: An electronic power tool device includes an electronic processor, a communication interface in communication with the electronic processor, and a wake-up sensor configured to generate a wake signal for activating the communication interface and the electronic processor responsive to a stimulus. The communication interface is configured to receive a first electronic message that includes an activation state and transmit the first received electronic message to the electronic processor. The electronic processor is configured to control the activation state of the electronic power tool device to allow or prevent operation of the electronic power tool device based on the first received electronic message.Type: GrantFiled: October 12, 2021Date of Patent: March 11, 2025Assignee: MILWAUKEE ELECTRIC TOOL CORPORATIONInventors: Timothy R. Obermann, Anthony M. Davis
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Patent number: 11549588Abstract: A brush seal is provided that includes a top plate, a back plate, and a bristle pack. The bristle pack is secured at a joint between the top plate and the back plate. The bristle pack includes a first bristle set extending from the joint, a second bristle set extending from the joint, and a sliding backing plate. The sliding backing plate includes a sliding portion and a support portion. The sliding portion is disposed contiguous with the second bristle set. The support portion has an inner face and a support face. The inner face is in contact with a distal end of the second bristle set. The support face is configured to support at least a portion of the first bristle set. The sliding backing plate is configured to slide relative to the second bristle set.Type: GrantFiled: April 5, 2018Date of Patent: January 10, 2023Assignee: Raytheon Technologies CorporationInventors: Jeremy Drake, Timothy M. Davis, Mark J. Rogers, Jose R. Paulino
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Patent number: 11486497Abstract: A seal structure may comprise a cavity defined at least partially by an axial surface and a radial surface. A brush seal may be disposed in the cavity. The brush seal may comprise a bristle pack and a backing plate coupled to the bristle pack. A first surface of the backing plate may contact the axial surface, and a second surface of the backing plate may contact the radial surface.Type: GrantFiled: July 19, 2017Date of Patent: November 1, 2022Assignee: Raytheon Technologies CorporationInventors: Timothy M. Davis, Mark J. Rogers, Jeffrey M. Wittman, James R. Plante
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Patent number: 11365641Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components. A wave spring and/or a rope seal is disposed between the first and second seal sections biases the first and second seal sections away from one another.Type: GrantFiled: February 1, 2019Date of Patent: June 21, 2022Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Timothy M. Davis, Paul M. Lutjen
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Patent number: 11359504Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components. One or more spring tabs extend from the second seal section and bias the first and second seal sections away from one another.Type: GrantFiled: April 15, 2019Date of Patent: June 14, 2022Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Paul M. Lutjen, Jeremy Drake, Timothy M. Davis
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Patent number: 11225877Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components. A wave spring and/or a rope seal is disposed between the first and second seal sections biases the first and second seal sections away from one another.Type: GrantFiled: February 1, 2019Date of Patent: January 18, 2022Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Timothy M. Davis, Paul M. Lutjen
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Patent number: 11220923Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components. One or more spring tabs extend from the second seal section and bias the first and second seal sections away from one another.Type: GrantFiled: April 15, 2019Date of Patent: January 11, 2022Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Paul M. Lutjen, Jeremy Drake, Timothy M. Davis
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Patent number: 11193386Abstract: A core assembly for fabricating an air cooled engine component for a gas turbine engine includes an end portion for defining passages within a side of an engine component. The end portion defines a first cross-section. A middle portion is spaced apart from the end portion and defines passages through a middle part of the engine component. The middle portion defines a second cross-section. One of the first cross-section and the second cross-section includes a first height greater than a second height. An air cooled engine component for a gas turbine engine and a gas turbine engine are also disclosed.Type: GrantFiled: May 18, 2016Date of Patent: December 7, 2021Assignee: Raytheon Technologies CorporationInventors: Timothy M. Davis, Paul M. Lutjen, Kevin J. Ryan
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Patent number: 11125095Abstract: A seal for sealing a space defined between first and second components, the seal having: an annular member having a substantially U-shaped cross section along at least a portion thereof, the portion configured to provide a seal interface at each of the first and second components.Type: GrantFiled: October 16, 2018Date of Patent: September 21, 2021Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventor: Timothy M. Davis
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Patent number: 11098606Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section and an uncoupled second seal section which allows the first and second seal sections to move relative to one another during relative movement between the two components. A wave spring disposed between the first and second seal sections biases the first and second seal sections away from one another. A compliant seal is carried by the second seal section. Other combinations of seal sections, wave springs, and compliant seals are also disclosed.Type: GrantFiled: August 5, 2019Date of Patent: August 24, 2021Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Timothy M. Davis, Paul M. Lutjen
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Patent number: 11085314Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a first seal section, a second seal section, and (in some embodiments) a third seal section. Two or three of the seal sections are uncoupled, which allows the uncoupled seal sections to move relative to one another during relative movement between the two components. One or more spring tabs extend from the second seal section and bias the first and third (or in some embodiments, the first and second) seal sections away from one another.Type: GrantFiled: February 8, 2019Date of Patent: August 10, 2021Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Timothy M. Davis, Paul M. Lutjen
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Patent number: 11073034Abstract: A seal assembly extends along an axis and seals an axial (and/or radial) gap between a first component and a second component. The seal assembly includes a seal carrier and a seal element. The seal element extends axially (and/or radially) between a first portion and a second portion. The first portion of the seal element is slidingly arranged within a slot in an axial end (or a radial side) of the seal carrier. The second portion of the seal element is configured to axially (and/or radially) engage the second component.Type: GrantFiled: April 17, 2019Date of Patent: July 27, 2021Assignee: Raytheon Technologies CorporationInventors: Paul M. Lutjen, Timothy M. Davis, Mark J. Rogers
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Patent number: 11021983Abstract: The present disclosure relates generally to a seal between two components. The seal includes a plurality of seal sections including convolutions therein that are inter-engaged with one another to form flexible and resilient seals.Type: GrantFiled: June 14, 2018Date of Patent: June 1, 2021Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Timothy M. Davis, Michael S. Stevens
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Patent number: 10962117Abstract: A brush seal for a gas turbine engine may comprise a spring-loaded support plate and a plurality of bristles located over the spring-loaded support plate. The spring-loaded support plate may comprise a support bar and a plurality of arms extending from the support bar. The support arms may be configured to apply a biasing load to the support bar.Type: GrantFiled: December 18, 2017Date of Patent: March 30, 2021Assignee: Raytheon Technologies CorporationInventors: James N Knapp, Timothy M Davis
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Patent number: 10935139Abstract: A dual-ended brush seal assembly that may be for turbine engine includes a first structure having a first surface and a second structure having a second surface. A brush seal of the assembly includes a bent bristle pack having a first end in sealing contact with the first surface and an opposite second end in sealing contact with the second surface. The first and second ends project in respective first and second directions that generally traverse one-another.Type: GrantFiled: July 18, 2019Date of Patent: March 2, 2021Assignee: Raytheon Technologies CorporationInventor: Timothy M. Davis
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Patent number: 10830357Abstract: The present disclosure relates to advanced materials, particularly single crystal grain structures including the formation of single crystal grain structures. Single crystal grain structures offer improved mechanical properties when used with individual components. Improving mechanical properties is favorable for components that are used in applications with high temperature, pressure, and stress. In these applications, mechanical failure is extremely undesirable. Individual components, such as seals, can be designed with a single crystal grain structure in a preferred direction. By selecting a preferred direction, and orienting the single crystal grain structure accordingly, the single crystal grain structure can improve the component's mechanical properties. Single crystal grain structure seals and the method of forming the seals, therefore, offer various improvements to individual components, specifically when the components are designed for high temperature, pressure, and stress applications.Type: GrantFiled: April 24, 2015Date of Patent: November 10, 2020Assignee: RAYTHEON TECHNOLOGIES CORPORATIONInventors: Michael G. McCaffrey, Jeffrey M. Wittman, Dilip M. Shah, Alan D. Cetel, Timothy M. Davis, Mark J. Rogers
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Patent number: 10822990Abstract: An active clearance control system of a gas turbine engine includes a multiple of blade outer air seal assemblies and a multiple of rotary ramps. Each of the multiple of rotary ramps is associated with one of the multiple of blade outer air seal assemblies. A method of active blade tip clearance control for a gas turbine engine is provided. The method includes rotating a multiple of rotary ramps to control a continuously adjustable radial position for each of a respective multiple of blade outer air seal assemblies.Type: GrantFiled: April 30, 2019Date of Patent: November 3, 2020Assignee: Raytheon Technologies CorporationInventors: Timothy M. Davis, Brian Duguay
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Patent number: 10731493Abstract: A seal for sealing a radially outer component of a gas turbine engine stator to a radially inner component thereof includes an axially resilient seal carrier adapted for mounting the seal carrier and including at a radially inner portion thereof, a pair of radially spaced, axially extending, radially resilient jaws adapted to clamp a sealing element such as a rope seal there between in sealing engagement with a radially inner component of the engine stator.Type: GrantFiled: April 10, 2014Date of Patent: August 4, 2020Assignee: Ratheyon Technologies CorporationInventors: Timothy M. Davis, Mark J. Rogers, Mark Broomer, Craig R. McGarrah, Carson A. Roy Thill
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Patent number: 10641119Abstract: The present disclosure relates generally to a sliding seal between two components. The sliding seal includes a seal ring including a radially extending base and an axially-extending leg disposed in a seal cavity between first and second components. A retaining ring having a first leg and a second leg defining a cavity therebetween is disposed with a portion of the base and a portion of the first component contained therein, thereby providing loading forces to help the seal ring seal against both the first and second components. One or more rope seals are carried by the seal ring in an embodiment. Other combinations of seal rings, retaining rings, and rope seals are also disclosed.Type: GrantFiled: December 15, 2017Date of Patent: May 5, 2020Assignee: UNITED TECHNOLOGIES CORPORATIONInventors: Timothy M. Davis, Paul M. Lutjen