公开(公告)号：EP3739343A1

公开(公告)日：2020-11-18

申请号：EP19214726.2

申请日：2019-12-10

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： SLY, Jamie ,  MILLER, Mark Sherwood

IPC: G01P5/24 ,  G01P5/26 ,  G01P13/02 ,  G01S15/86 ,  G01S17/58 ,  B64D43/02

Abstract: A system includes a laser air data sensor (12) and an acoustic air data sensor (14). The laser air data sensor is configured to emit directional light into airflow about an aircraft exterior and to generate first air data parameter outputs for the aircraft based on returns of the emitted directional light. The acoustic air data sensor is configured to emit acoustic signals into the airflow about the aircraft exterior, sense the acoustic signals, and generate second air data parameter outputs for the aircraft based on the sensed acoustic signals.

公开(公告)号：EP3333577B1

公开(公告)日：2019-11-06

申请号：EP17206457.8

申请日：2017-12-11

Applicant: Rosemount Aerospace Inc.

Inventor： NASLUND, Brian Brent ,  SLY, Jamie

IPC: G01P5/14 ,  G01P13/02 ,  G01P21/02

公开(公告)号：EP3825233A1

公开(公告)日：2021-05-26

申请号：EP20200598.9

申请日：2020-10-07

Applicant: Rosemount Aerospace Inc.

Inventor： HAWLEY, Brian ,  SLY, Jamie ,  MATHEIS, Brian Daniel

IPC: B64D43/02 ,  G01P5/24 ,  G01P13/02

Abstract: Apparatus and associated methods relate to detecting turbulence of an airstream over an airfoil surface of an aircraft (10) using a sequence of acoustic transducers (14A-D) attached to the airfoil surface (18) of the aircraft along a path. Each of the sequence of acoustic transducers is configured to detect acoustic waves indicative of airstream condition proximate the acoustic transducer. A processor (16) is configured to determine, for each of the sequence of acoustic transducers, a level of turbulence of the airstream proximate the acoustic transducer.

公开(公告)号：EP3460488A1

公开(公告)日：2019-03-27

申请号：EP18195815.8

申请日：2018-09-20

Applicant: Rosemount Aerospace Inc.

Inventor： SLY, Jamie ,  MILLER, Mark Sherwood

IPC: G01P5/26 ,  G01S17/58 ,  G01S17/95

Abstract: A laser sensing system (12) includes an emitter configured to emit a laser, and a controller (18). The intensity of the laser is based upon power provided to the laser sensing system (12). The controller (18) is configured to control the power provided to the laser sensing system (12), obtain feedback parameters indicative in part of molecular content of the atmosphere, and control the power provided to the laser sensing system (12) based upon the feedback parameters.

公开(公告)号：EP4235218A2

公开(公告)日：2023-08-30

申请号：EP23168581.9

申请日：2019-12-12

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： SLY, Jamie ,  MILLER, Mark Sherwood

IPC: G01S17/00

Abstract: An air data sensor is described, comprising: an acoustic transmitter (101) configured to output an acoustic signal into an airflow; a plurality of acoustic transducers (105) configured to receive the acoustic signal output by the acoustic transmitter; a light source (107) configured to output a light beam into the airflow; a light receiver (111) configured to receive scattered light from the light beam, wherein the light source (107) and the light receiver (111) are bistatic such that a measurement zone is formed away from the air data sensor (100); a plate body (117); and one or more lenses mounted to the plate body (117) and disposed in optical communication with each the light source (107) and the light receiver (111).

公开(公告)号：EP3333577A1

公开(公告)日：2018-06-13

申请号：EP17206457.8

申请日：2017-12-11

Applicant: Rosemount Aerospace Inc.

Inventor： NASLUND, Brian Brent ,  SLY, Jamie

IPC: G01P5/14 ,  G01P13/02 ,  G01P21/02

Abstract: A first air data system for providing first aircraft air data parameter outputs is formed by a first electronics channel (28) of a first multi-function probe (MFP) (12A) that is electrically coupled with a first static pressure sensor. A second air data system for providing second aircraft air data parameter outputs is formed by a first electronics channel (30) of a second MFP (12B) that is electrically coupled with a second static pressure sensor. A third air data system for providing third aircraft air data parameter outputs is formed by a second electronics channel (30) of the first MFP (12A) that is electrically coupled with a second electronics channel (30) of the first MFP (12A).

公开(公告)号：EP4235218A3

公开(公告)日：2024-01-03

申请号：EP23168581.9

申请日：2019-12-12

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： SLY, Jamie ,  MILLER, Mark Sherwood

IPC: G01P5/24 ,  G01P5/26 ,  G01P13/02 ,  G01S7/521 ,  G01S15/60 ,  G01S15/86 ,  G01S17/00 ,  G01S17/58 ,  B64D43/02 ,  G01S15/00

Abstract: An air data sensor is described, comprising: an acoustic transmitter (101) configured to output an acoustic signal into an airflow; a plurality of acoustic transducers (105) configured to receive the acoustic signal output by the acoustic transmitter; a light source (107) configured to output a light beam into the airflow; a light receiver (111) configured to receive scattered light from the light beam, wherein the light source (107) and the light receiver (111) are bistatic such that a measurement zone is formed away from the air data sensor (100); a plate body (117); and one or more lenses mounted to the plate body (117) and disposed in optical communication with each the light source (107) and the light receiver (111).

公开(公告)号：EP3730947A1

公开(公告)日：2020-10-28

申请号：EP19214956.5

申请日：2019-12-10

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： SLY, Jamie ,  SHANNON, Daniel W. ,  MATHEIS, Brian Daniel ,  ELL, Todd A. ,  KUNIK, William ,  KOUSHIK, Surdarshan N.

IPC: G01P5/24 ,  G01P13/02 ,  B64D43/02

Abstract: An ultrasonic air data system (100) can include a pole (103) having a length (103) longer than a boundary layer thickness (105) of a boundary layer flow (107) such that at least a distal end of the pole is configured to extend outwardly from an aircraft surface to be at least partially outside of the boundary layer flow. The system can include a transmitter (111) disposed on or in the pole at or near the distal end of the pole such that the transmitter is located at least partially outside of the boundary layer flow when in use, wherein the transmitter is configured to output a transmitter signal. The system can include one or more receivers (115) disposed downstream of the pole as defined by the boundary layer flow and configured to receive the transmitter signal.

公开(公告)号：EP3633388A1

公开(公告)日：2020-04-08

申请号：EP19201552.7

申请日：2019-10-04

Applicant: ROSEMOUNT AEROSPACE INC.

Inventor： MATHEIS, Brian Daniel ,  SLY, Jamie ,  EGBERG, James Barron

IPC: G01P5/24 ,  G01P13/02 ,  G01P21/02

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.