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公开(公告)号：EP4386459A1
公开(公告)日：2024-06-19
申请号：EP23211149.2
申请日：2023-11-21
Applicant: Rosemount Aerospace Inc.
Inventor： DANICICH, Jeffrey P. , WICKS, Curtis J.
Abstract: A positional lens locking assembly for focusing and maintaining focus of a camera lens assembly includes a lens tube, a camera housing, a sealing member, and a locking member. The lens tube has a head and a barrel. The head extends outward from the barrel and the barrel has a threaded portion. The camera housing has a first threaded bore configured to receive the threaded portion of the barrel. The sealing member is disposed between the head and the camera housing and is configured to be compressed between the head and the camera housing. The locking member is configured to retain the lens tube in a position.
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公开(公告)号：EP4371887A1
公开(公告)日：2024-05-22
申请号：EP23211108.8
申请日：2023-11-21
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： LINCOLN, David L. , WANG, Longke , SNYDER, Jordan A. , CASTILLO-GARZA, Rodrigo , EMERSON, Sean C. , JACKSON, Darren G. , RAY, Mark D. , ANDERSON, Kaare Josef
CPC classification number: G01W1/08 , B64D45/00 , B64G1/1042
Abstract: A system includes a first sensor (102) positioned to sense presence of a contrail in a first volume (104), wherein the first volume at least partially overlaps an expected volume of a contrail (106) proximate an aircraft. A second sensor (108) is positioned to sense a background reference in a second volume (110), where the second volume (110) does not overlap the expected volume of a contrail (106) proximate an aircraft. A controller (118) is operatively connected to the first and second sensors (102, 108). The controller (118) includes machine readable instructions configured to cause the controller (118) to utilize data input from both the first and second volumes (104, 110) to determine if a contrail is present from the aircraft. A system includes machine readable instructions configured to cause the controller (118) to predict persistence of contrails on an intended route through the volume of airspace and to determine an improved route and/or propulsion operation to reduce contrail formation and persistence relative to the intended route.
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公开(公告)号：EP4235189A3
公开(公告)日：2023-11-22
申请号：EP23165129.0
申请日：2019-12-12
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： WIGEN, Scott , Seidel, Greg , RANJAN, Ram , GOLLY, Timothy Thomas
Abstract: An air data probe (10;26;42) includes an air data probe body (12;28;44) and an additively manufactured heater (100-900) on the air data probe body.
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公开(公告)号：EP4253928A1
公开(公告)日：2023-10-04
申请号：EP23163464.3
申请日：2023-03-22
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： BERG, Brandon T. , GILKISON, Brian A.
Abstract: Apparatus and associated methods relate to sensing pressure and mitigating the error introduced by the thermoelectric effect. A pressure sensing device includes a pressure sensor (102, 202), a temperature sensor (110), and an error correction device. The pressure sensor (102, 202) produces a voltage output proportional to a sensed pressure. The temperature sensor (110) measures a first temperature at a first location and a second temperature at a second location to produce a temperature difference signal. The error correction device modifies the pressure output proportionally to the temperature difference signal to produce a temperature adjusted pressure output which compensates for error introduced from the temperature difference.
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公开(公告)号：EP4194832A3
公开(公告)日：2023-09-27
申请号：EP22208879.1
申请日：2022-11-22
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： POTASEK, David P. , STUELKE, Robert
Abstract: A pressure sensor includes a Wheatstone bridge circuit including a first resistor (R1), a second resistor (R2), a third resistor (R3), and a fourth resistor (R4) having matching output characteristics. The pressure sensor further includes a first trim resistor (RG, RS) in series with the Wheatstone bridge circuit, wherein the first trim resistor has output characteristics matching the output characteristics of the first resistor, the second resistor, the third resistor, and the fourth resistor of the Wheatstone bridge. The pressure sensor additionally includes a second trim resistor (RZ, RV) in parallel or a parallel loop with the Wheatstone bridge circuit, wherein the second trim resistor has output characteristics matching the output characteristics of the first resistor, the second resistor, the third resistor, and the fourth resistor of the Wheatstone bridge.
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Patent Agency Ranking
公开(公告)号：EP4224173A2
公开(公告)日：2023-08-09
申请号：EP23165690.1
申请日：2019-12-12
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： JOHNSON, Paul Robert , GOLLY, Timothy Thomas , SEIDEL, Greg Allen
Abstract: A probe head of an air data probe is described herein comprising: an insert (20, 20A) including: a first end (38, 38A), a first end (40, 40A) opposite the first end (38, 38A); and a body portion (42, 42A) extending between the first end (38, 38A) and the first end (40, 40A), the body portion (42, 42A) including a groove; a portion of a heater within the groove; an outer shell (24, 24A) surrounding the insert (20, 20A) and the portion of the heater, the outer shell (24, 24A) including: a tip portion defining a first end (54, 54A) of the outer shell (24, 24A); and a body portion (42, 42A) extending from the tip portion; and a tip weld connected to the first end (38, 38A) of the insert (20, 20A) and the first end (54, 54A) of the outer shell (24, 24A), wherein the tip weld forms the tip of the probe head.
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公开(公告)号：EP4220186A1
公开(公告)日：2023-08-02
申请号：EP23161581.6
申请日：2019-10-04
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： MATHEIS, Brian Daniel , EGBERG, James Barron , SLY, James
Abstract: An aircraft freestream data system can include a first ultrasonic air data system (UADS) (101) configured to sense local acoustic properties at a first location on an aircraft, a first local air data module (103) operatively connected to the first UADS and configured to determine first local air data of the first location and to output first local air data, and a freestream data module (105) operatively connected to the first local air data module. The freestream data module can be configured to receive the first local air data from the local air data module, determine one or more freestream air data parameters based on at least the first local air data, and output the one or more freestream air data parameters to one or more aircraft consuming systems.
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公开(公告)号：EP4194832A2
公开(公告)日：2023-06-14
申请号：EP22208879.1
申请日：2022-11-22
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： POTASEK, David P. , STUELKE, Robert
Abstract: A pressure sensor includes a Wheatstone bridge circuit including a first resistor (R1), a second resistor (R2), a third resistor (R3), and a fourth resistor (R4) having matching output characteristics. The pressure sensor further includes a first trim resistor (RG, RS) in series with the Wheatstone bridge circuit, wherein the first trim resistor has output characteristics matching the output characteristics of the first resistor, the second resistor, the third resistor, and the fourth resistor of the Wheatstone bridge. The pressure sensor additionally includes a second trim resistor (RZ, RV) in parallel or a parallel loop with the Wheatstone bridge circuit, wherein the second trim resistor has output characteristics matching the output characteristics of the first resistor, the second resistor, the third resistor, and the fourth resistor of the Wheatstone bridge.
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公开(公告)号：EP4187256A1
公开(公告)日：2023-05-31
申请号：EP22209319.7
申请日：2022-11-24
Applicant: ROSEMOUNT AEROSPACE INC.
Inventor： TEIGEN, Daniel James , ROSE, Kyle H. , KUHA, Chad , WACHTER, Karl
Abstract: A corrosion-resistant air data probe includes a hollow tube (104, 204, 304) having at least one opening, an inner surface of the hollow tube (104, 204, 304) defining an interior cavity (112), a heating element, and a continuous layer of a braze material. The heating element is disposed adjacent to the inner surface, within the interior cavity (112). The continuous layer of the braze material completely covers the heating element and covers at least a portion of the inner surface.
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公开(公告)号：EP4095003A1
公开(公告)日：2022-11-30
申请号：EP22185837.6
申请日：2018-08-23
Applicant: Rosemount Aerospace Inc.
Inventor： VADGAONKAR, Prashant , MAHAPATRA, Guru Prasad , KHANRA, Sujoy , DUSSA, Pullaiah
IPC: B60S1/08
Abstract: A method of controlling a windshield wiper assembly with configurable variable sweep angle or variable sweep speed in a vehicle. The method includes operably connecting a bidirectional motor (24, 24') in a vehicle wiper system (10), commanding an operation of the motor (24, 24') in a selected direction at a selected motor speed, the motor speed selected to achieve at least one of a configured wiper arm sweep speed and a configured sweep angle, and selecting at least one of a duration and a motor reversal position for end of sweep to achieve the configured sweep angle for the wiper arm. After at least one of the duration and reaching the motor reversal position, the method includes directing the motor (24, 24') in the opposite direction at another motor speed, the another motor speed selected to achieve another configured wiper arm speed, and repeating the commanding, selecting and directing. Finally, the method includes configuring at least one of the sweep angle, the sweep speed, the duration, the reversal position and the repeating.
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