公开(公告)号：EP4474292A3

公开(公告)日：2025-03-05

申请号：EP24207041.5

申请日：2021-09-20

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： NASLUND, Brian Brent ,  KANE, Brian D. ,  SCHAUB, Steven ,  MATHEIS, Brian Daniel

IPC: G01P13/02 ,  G01P21/02 ,  G01P15/00 ,  B64D45/02 ,  B64D43/02 ,  G01D3/08 ,  B64D45/00

Abstract: An angle of attack sensor includes a rotatable vane (12) away and support from a mounting plate (68), a housing (36) extending way from an opposite side of the mounting plate, and a sensor (10) coupled to the vane. The angle of attack sensor communicates with an electronics module enclosed within the housing or mounted remotely with respect to the angle of attack sensor. The electronics module (72) includes a processor (88), computer-readable memory (90), and a communication device (92). The computer-readable memory is encoded with instructions that, when executed by the processor, cause the electronics module to perform steps of a damage detection method.

公开(公告)号：EP4509842A1

公开(公告)日：2025-02-19

申请号：EP24194673.0

申请日：2024-08-14

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： SCHWIE, Chester M. ,  PITERA, Rudy L.

IPC: G01P5/165 ,  B64D43/02 ,  G01P13/02

Abstract: An air-data probe component includes an additively manufactured inner member (102). The inner member includes integrally formed, monolithic structures including a mandrel bulkhead (104) defining a plurality of pneumatic chambers (106, 108, 110, 112, 114) therein in fluid communication with an outer surface (116) of the mandrel bulkhead through respective pressure ports, and a plurality of pneumatic tubes (120, 122, 124, 126, 128) extending aft of the mandrel bulkhead along a probe axis, each in fluid communication with a respective one of the plurality of pneumatic chambers. An outer cover tip (144) can be engaged about the mandrel bulkhead with a plurality of bores (146) therethrough for fluid communication of outside air pressure into the plurality of pneumatic tubes through the outer cover tip. A forward surface of the outer cover tip can be flush, conformal, and continuous with an aerodynamic outer surface of an aircraft.

公开(公告)号：EP4498094A1

公开(公告)日：2025-01-29

申请号：EP24191256.7

申请日：2024-07-26

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： BOELMAN, Joshua ,  ACOTT, Phillip

IPC: G01P5/26 ,  G01S7/48 ,  G01S17/42 ,  G01S17/58 ,  G01S17/933 ,  B64D43/00 ,  G01P13/02 ,  G01S17/95

Abstract: Apparatus and associated methods relate to improving measurement of metrics determined by laser air-data systems subject to unwanted background light. Such measurements are improved by estimating and excising the unwanted background light from the total light received by an optical receiver (14) which receives a Doppler-shifted reflected portion of a projected beam of light backscattered by aerosols and air molecules of an atmosphere. The background light is estimated using a background-light rejection filter (16) that receives the light received by the optical receiver (14) after it has been filtered by a vapor cell filter (22) and separates the light received by the optical receiver (14) into a beam sampling portion and a complementary non-beam portion. The non-beam sampling portion is used to estimate the background light portion within the beam sampling portion, which also contains the Doppler-shifted reflected portion of the projected beam used for calculating the metrics of air data.

公开(公告)号：EP4491464A1

公开(公告)日：2025-01-15

申请号：EP24188121.8

申请日：2024-07-11

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： BOJJANAPALLI, Muralidhar Rao ,  JAYARAJ, Sandeep

IPC: B60S1/48 ,  B60S1/50 ,  B60S1/52

Abstract: A windshield wash system includes a pump (12) with an inlet (12a) and an outlet (12b), and a fluid reservoir (11) fluidically connected to the inlet of the pump. A fluid delivery line (14) is fluidically connected to the outlet of the pump and at least one nozzle (18) is fluidically connected to the fluid delivery line. An electronic control unit (18) is in controlling communication with the pump. A pressure sensor (20) is in the fluid delivery line and is in communication with the electronic control unit.

公开(公告)号：EP4428091A3

公开(公告)日：2024-12-18

申请号：EP24161954.3

申请日：2024-03-07

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： ZHENG, Jun ,  ZHANG, Weibin

IPC: B81B3/00

Abstract: A packaged pressure sensor assembly is disclosed that includes a pressure sensor (100, 200) including an upper substrate and a lower substrate bonded to one another by way of a first glass frit having a first bonding temperature, so as to define a hermetically sealed pressure sensing chamber therebetween, and a housing defining an internal cavity having a base with a support surface for supporting the pressure sensor (100, 200), wherein the pressure sensor (100, 200) is bonded to the support surface of the base by a second glass frit having a second bonding temperature that is lower than the first bonding temperature.

公开(公告)号：EP4435474A1

公开(公告)日：2024-09-25

申请号：EP24165250.2

申请日：2024-03-21

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： RAY, Mark D. ,  ANDERSON, Kaare J.

IPC: G01S17/95 ,  G01S7/499 ,  G01S7/48

CPC classification number: G01S17/95 ,  G01S7/499 ,  G01S7/4802 ,  G01N15/00

Abstract: A cloud phase detection system can include a light receiver system (101) configured to receive reflected light from a cloud, and a cloud phase module (103) operatively connected to the light receiver system and configured to calculate a fourth Stokes parameter and a multiple scattering ratio (MSR) parameter based on the reflected light. The cloud phase module can be configured to determine a phase of a cloud based on a relationship between the fourth Stokes parameter and the MSR parameter.

公开(公告)号：EP4417423A1

公开(公告)日：2024-08-21

申请号：EP24157967.1

申请日：2024-02-15

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： ROMAN, Jamison K. ,  SCHWEITZER, Jeremiah

IPC: B33Y80/00 ,  B64D15/20 ,  G01K13/02

CPC classification number: B64D15/20 ,  G01K13/028 ,  B33Y80/00

Abstract: A detector includes a scoop portion (102). The scoop portion (102) includes a top surface (104) extending continuously from a forward tip to an aft end, a bottom surface (110) opposite from the top surface (104), and a receiving portion therebetween. The bottom surface (110) includes an aperture. The top surface (104) includes a detent formed therein opposite from the aperture across the receiving portion. The detent is configured and adapted to receive at least a portion of a sensor. A method includes additively manufacturing a scoop portion (102) and brazing a strut portion to the scoop portion (102). The scoop portion (102) includes an upper surface, a lower surface, and a receiving portion therebetween.

公开(公告)号：EP4401359A1

公开(公告)日：2024-07-17

申请号：EP24151200.3

申请日：2024-01-10

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： JENSEN, Isaac A. ,  LUND, Kraig S. ,  WOODS, Timothy J. ,  FRANKLIN, Jeremy M. ,  EUCKEN, Douglas

IPC: H04L9/40

CPC classification number: H04L63/0209 ,  H04L63/0281 ,  H04L63/164 ,  H04L63/20

Abstract: A secure network interface system includes a secure domain interface (206), a processing system (208), a network function device (220), and a network interface (230). The processing system is configured to send and receive information within secure systems, transmit configuration data for the network interface, compile data from the secure systems into a plurality of data packets, and transmit the plurality of data packets to the network function device without being physically capable of receiving data packets from the network function device, thus providing a demonstration of security partitioning. The network function device receives the configuration data, configures the network interface using the configuration data, and provides discrete feedback to the processing system regarding a configuration status. The network interface sends the plurality of data packets to one or more external unsecure systems (234) and to limits a communication protocol type received from one or more external unsecure systems.

公开(公告)号：EP4366094A3

公开(公告)日：2024-07-17

申请号：EP24160288.7

申请日：2018-05-11

Applicant: Rosemount Aerospace Inc.

Inventor： DEANGELO, Tim

IPC: H05K1/11 ,  H01R12/52 ,  H05K3/36 ,  H01R12/58 ,  B33Y80/00 ,  H05K1/14

CPC classification number: H01R12/52 ,  H05K1/11 ,  H05K1/145 ,  H05K3/368 ,  H05K2201/1018920130101 ,  H05K2201/1029520130101 ,  H05K2201/201820130101 ,  B33Y80/00 ,  H01R12/58 ,  H05K1/144 ,  H05K3/366 ,  H05K2201/04220130101

Abstract: A circuit card assembly (10; 110; 210; 310) includes a first printed wiring board (28; 128; 228; 328) with a first receiving feature (38; 138; 238; 338) and a trace (12; 112; 212; 312) attached to the first printed wiring board (28; 128; 228; 328). The three dimensional trace (12; 112; 212; 312) is formed by layer-by-layer additive manufacturing. The three dimensional trace (12; 112; 212; 312) includes first (14; 114; 214; 314) and second ends. The first end (14; 114; 214; 314) of the three dimensional trace (12; 112; 212; 312) engages with the first receiving feature (38; 138; 238; 338) of the first printed wiring board (28; 128; 228; 328). The second end of the three dimensional trace (12; 112; 212; 312) is configured to engage with a second printed wiring board (40; 140; 240; 340).

公开(公告)号：EP4389324A1

公开(公告)日：2024-06-26

申请号：EP23215364.3

申请日：2023-12-08

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： LOPAC, Mark S. ,  FEIST, Dale

IPC: B22F10/31 ,  B22F10/39 ,  B22F10/62 ,  B22F10/66 ,  B22F12/30 ,  B22F12/33 ,  B22F12/37 ,  B22F12/86 ,  B29C64/176 ,  B29C64/182 ,  B29C64/188 ,  B29C64/245 ,  B33Y10/00 ,  B33Y40/20 ,  B22F10/28 ,  B29C64/153 ,  B33Y30/00

CPC classification number: B22F12/30 ,  B22F12/33 ,  B22F12/37 ,  B22F10/31 ,  B22F10/39 ,  B22F12/86 ,  B22F10/28 ,  B22F10/66 ,  B22F10/62 ,  B29C64/153 ,  B29C64/245 ,  B29C64/188 ,  B33Y10/00 ,  B33Y40/20 ,  B33Y30/00

Abstract: A method of making an object (42) includes partially additively manufacturing the object (42) onto a removable platen (40) using an additive manufacturing system, removing the platen (40) with the object (42) from a base (38) of the additive manufacturing system, processing the object (42) on the platen (40), inserting the platen (40) with the object (42) that has been processed into the additive manufacturing system or a different system, mating the platen (40) with the object (42) that has been processed to the base (38) of the additive manufacturing system or a base (38) of the different system using a registration feature, and manufacturing a layer onto the object (42) that has been processed.