Processing

Please wait...

PATENTSCOPE will be unavailable a few hours for maintenance reason on Tuesday 25.01.2022 at 12:00 PM CET
Settings

Settings

Goto Application

1. WO2021236190 - ANGLE OF ATTACK SENSOR WITH SLOPED FACEPLATE

Publication Number WO/2021/236190
Publication Date 25.11.2021
International Application No. PCT/US2021/019630
International Filing Date 25.02.2021
IPC
G01P 13/02 2006.1
GPHYSICS
01MEASURING; TESTING
PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION OR SHOCK; INDICATING PRESENCE OR ABSENCE OF MOVEMENT;  INDICATING DIRECTION OF MOVEMENT 
13Indicating or recording presence or absence of movement; Indicating or recording of direction of movement
02Indicating direction only, e.g. by weather vane
B64D 15/00 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
15De-icing or preventing icing on exterior surfaces of aircraft
B64D 43/00 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
43Arrangements or adaptations of instruments
B64D 43/02 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
43Arrangements or adaptations of instruments
02for indicating aircraft speed or stalling conditions
B64D 45/00 2006.1
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
45Aircraft indicators or protectors not otherwise provided for
CPC
B64D 43/02
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
43Arrangements or adaptations of instruments
02for indicating aircraft speed or stalling conditions
G01C 21/00
GPHYSICS
01MEASURING; TESTING
CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
21Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
G01P 13/02
GPHYSICS
01MEASURING; TESTING
PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
13Indicating or recording presence, absence, or direction, of movement
02Indicating direction only, e.g. by weather vane
Applicants
  • ROSEMOUNT AEROSPACE INC. [US]/[US]
Inventors
  • WHALEN, Mackenzie
  • CUSHER, Aaron, A.
  • VALDES CHAVEZ, Armando
  • HANSON, Daniel
  • SCHWARTZ, Richard, Alan
  • JOHNSON, Wallace
  • KRUEGER, William, B.
  • ANDERSON, Kaleb
Agents
  • FAIRBAIRN, David, R.
  • KOENCK, Alan, M.
  • WRIGHT, Erik
Priority Data
62/981,25625.02.2020US
Publication Language English (en)
Filing Language English (EN)
Designated States
Title
(EN) ANGLE OF ATTACK SENSOR WITH SLOPED FACEPLATE
(FR) CAPTEUR D'ANGLE D'ATTAQUE À PLAQUE FRONTALE INCLINÉE
Abstract
(EN) An angle of attack sensor includes a housing having an open end and a closed end, a faceplate positioned on the open end of the housing, the faceplate comprising a periphery at an outer edge of the faceplate, a central opening, and an exterior surface extending from the periphery to the central opening, and a vane assembly extending through the central opening of the faceplate. The exterior surface of the faceplate has a sloped profile from the periphery to the central opening.
(FR) Un capteur d'angle d'attaque comprend un boîtier ayant une extrémité ouverte et une extrémité fermée, une plaque frontale positionnée sur l'extrémité ouverte du boîtier, la plaque avant comprenant une périphérie au niveau d'un bord externe de la plaque avant, une ouverture centrale, et une surface extérieure s'étendant de la périphérie à l'ouverture centrale, et un ensemble aube s'étendant à travers l'ouverture centrale de la plaque frontale. La surface extérieure de la plaque frontale a un profil incliné de la périphérie à l'ouverture centrale.
Latest bibliographic data on file with the International Bureau