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公开(公告)号：US20230344104A1
公开(公告)日：2023-10-26
申请号：US17659865
申请日：2022-04-20
Applicant: Raytheon Company
Inventor： David D. Crouch , Eachan Russell Landreth , David R. Sar
Abstract: An apparatus for and a method of a coaxial-to-waveguide power combiner/divider. The apparatus includes a single-fin coaxial-to-waveguide power combiner/divider, including a waveguide having one open end, one closed end, and two sides that are broader than two other sides; two fins in a plane within the waveguide, wherein the plane is configured to be parallel to the broader sides of the waveguide; and at least one coaxial input joined to each of the two fins. Signals may be applied to the at least one coaxial input joined to each of the two fins are in phase with each other, and a number of the at least one coaxial input joined to each of the two fins may include one of a same number and a different number.
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公开(公告)号：US11612668B2
公开(公告)日：2023-03-28
申请号：US16986761
申请日：2020-08-06
Applicant: Raytheon Company
Inventor： David D. Crouch , David R. Sar , Alf L. Carroll, III , John Carcone
Abstract: A system includes a containment vessel configured to receive and hold one or more pieces of personal protection equipment to be heated and decontaminated during a decontamination process. The system also includes a solar collection device configured to heat the containment vessel based on received solar energy. The solar collection device includes a body having a first portion and a second portion. The first portion includes a solar aperture configured to receive the solar energy. The second portion is configured to receive the containment vessel within the body of the solar collection device. The solar collection device also includes louvered slats across the solar aperture. The louvered slats are configured to be rotated in order to control an amount of solar energy passing through the solar aperture into the body of the solar collection device.
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公开(公告)号：US20170125896A1
公开(公告)日：2017-05-04
申请号：US14928143
申请日：2015-10-30
Applicant: Raytheon Company
Inventor： David D. Crouch , David R. Sar
IPC: H01Q1/42
CPC classification number: H01Q1/422
Abstract: A monolithic, wideband, millimeter-wave radome is provided. The radome includes a solid layer formed of a single material and a lattice layer formed of the single material and disposed on an exterior surface of the solid layer. The lattice layer includes void regions formed from selective omission of the single material during lattice layer buildup.
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公开(公告)号：US12283738B2
公开(公告)日：2025-04-22
申请号：US17991460
申请日：2022-11-21
Applicant: Raytheon Company
Inventor： David D. Crouch , David R. Sar
Abstract: An axially-fed RF power combiner combines a plurality of input signals to generate a single fundamental-mode transverse electromagnetic (TEM) output. The combiner comprises a vacuum coaxial transmission line having a plurality of coaxial vacuum feedthroughs configured to receive the input signals. The feedthroughs are arranged axially around the vacuum coaxial transmission line. An increasing gap is provided between the inner conductive surface and the outer conductive surface of the vacuum coaxial transmission line to gradually transition the input signals from each coaxial vacuum feedthrough to quasi-TEM mode signals within the vacuum envelope of the vacuum coaxial transmission line. In some conductive-ridge embodiments, the inner conductive surface of the vacuum coaxial transmission line may comprise a cylindrical conductive base and a plurality of radially-aligned conductive ridges azimuthally distributed within a vacuum envelope of the vacuum coaxial transmission line. In some ridge-less embodiments, the inner conductive surface includes a tapered region within the vacuum envelope to provide an increasing gap between the inner conductive surface and the outer conductive surface.
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公开(公告)号：US20210330842A1
公开(公告)日：2021-10-28
申请号：US17169260
申请日：2021-02-05
Applicant: Raytheon Company
Inventor： Alf L. Carroll, III , David R. Sar , David D. Crouch , John Carcone
Abstract: A system for decontaminating personal protection equipment includes a microwave oven and a decontamination apparatus configured to be placed in and heated by the microwave oven. The decontamination apparatus includes a containment vessel having an interior space configured to be sealed. The decontamination apparatus also includes one or more stands within the interior space, where the one or more stands are configured to receive and hold one or more pieces of personal protection equipment to be heated by the microwave oven and decontaminated within the interior space. The decontamination apparatus further includes a pressure-relief valve configured to be opened to release a pressure within the interior space.
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Patent Agency Ranking
公开(公告)号：US20210278183A1
公开(公告)日：2021-09-09
申请号：US16828200
申请日：2020-03-24
Applicant: RAYTHEON COMPANY
Inventor： David D. Crouch , David R. Sar , Michael J. Holihan , Alf L. Carroll
Abstract: A non-lethal naval vessel interdiction weapon is provided. The non-lethal naval vessel interdiction weapon includes a hydrodynamic hull, guidance and delivery systems housed in the hydrodynamic hull with the delivery system being controllable by the guidance system to drive a naval vessel impeding payload toward a target and a deployment system. The deployment system is configured to prepare the hydrodynamic hull for payload deployment and to deploy the naval vessel impeding payload toward the target following hull preparation.
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公开(公告)号：US20190120600A1
公开(公告)日：2019-04-25
申请号：US16100749
申请日：2018-08-10
Applicant: Raytheon Company
Inventor： Michael J. Holihan , Michael C. Prescott , David D. Crouch , David R. Sar , Thomas L. Obert
IPC: F41H11/02
Abstract: An apparatus includes a capsule configured to be launched or carried towards an unmanned aerial vehicle (UAV). The apparatus also includes a directed energy device within or carried by the capsule. The directed energy device includes a first inductor configured to generate an inductive magnetic field that is able to inductively couple into one or more electronics of the UAV in order to disable or destabilize the UAV. The capsule can be configured to be launched towards the UAV and can include a loiter mechanism (such as a rotor, umbrella, or parachute) configured to maintain a position of the capsule or to slow a descent of the capsule after launch. The capsule can also be configured to be carried towards the UAV by a different UAV, and the apparatus can further include a tether coupling the capsule to the different UAV.
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公开(公告)号：US12194181B2
公开(公告)日：2025-01-14
申请号：US16944617
申请日：2020-07-31
Applicant: Raytheon Company
Inventor： David D. Crouch , Alf L. Carroll, III , John Carcone , David R. Sar , Travis B. Feenstra
Abstract: An apparatus includes a containment vessel having an interior space configured to be sealed. The interior space is configured to receive at least one reservoir of liquid to be vaporized during a decontamination process. The apparatus also includes a base configured to be inserted into the interior space. The base is configured to receive one or more pieces of personal protection equipment to be heated and decontaminated within the interior space during the decontamination process. The base is configured to hold the one or more pieces of personal protection equipment above the at least one reservoir of liquid. The apparatus further includes a pressure-relief valve configured to be opened to release a pressure within the interior space. In some cases, the apparatus may include a filter configured to filter material passing through the pressure-relief valve.
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公开(公告)号：US11951222B2
公开(公告)日：2024-04-09
申请号：US17124208
申请日：2020-12-16
Applicant: Raytheon Company
Inventor： David D. Crouch , Alf L. Carroll, III , John Carcone , Travis B. Feenstra , David R. Sar , Anthony Serino
CPC classification number: A61L2/186 , A61L2/084 , F24S23/74 , F24S50/80 , A61L2202/122 , A61L2202/14 , F24S2025/01 , F24S2025/6007
Abstract: A system includes a containment vessel configured to receive and retain equipment to be decontaminated. The system also includes a solar reflector configured to reflect solar energy towards the containment vessel in order to heat the containment vessel. The system further includes end supports configured to receive and retain the solar reflector and the containment vessel. The system also includes a base having or coupled to multiple side supports, where each side support is configured to contact and support a corresponding one of the end supports. In addition, the system includes one or more semi-transparent solar shades configured to reduce the solar energy reaching the solar reflector and the containment vessel.
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10.发明授权公开(公告)号：US11798769B1
公开(公告)日：2023-10-24
申请号：US18121937
申请日：2023-03-15
Applicant: Raytheon Company
Inventor： Eric Alan Berry , David R. Sar , Sandra Stein , Alexander T. Burke
Abstract: A high-power microwave (HPM) vacuum tube source and method of precise coaxial alignment of the field emission (FE) cathode, cylindrical RF generating tube and magnet field includes positioning a low-power thermionic emission (TE) cathode inside the FE cathode in a “cathode-in-cathode” arrangement. With the HPM source under vacuum and the FE cathode deactivated, the TE cathode emits a surrogate electron beam through the generating tube. Measurement circuits measure the surrogate electron beam's position with respect to a longitudinal axis fore and aft of the generating tube. The measurements circuits may, for example, be a repositionable fluorescent target or electric field sensors embedded in the cylindrical RF generating tube. The coaxial alignment of the primary cathode, cylindrical RE generating tube and magnet is adjusted until the position of the surrogate electron beam satisfies a coaxial alignment tolerance.
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