# US 11,441,963 B1 · Aircraft pressure measurement device including an enhanced cleaning system > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 11,441,963 B1 - Document ID: US11441963B1 - Status: Granted - Kind: B1 - Application number: 17/302,436 - Filed: 2021-05-03 - Granted: 2022-09-13 - Earliest claimed: 2021-05-03 - Assignees: Rosemount Aerospace Inc. - Applicants: Rosemount Aerospace Inc. - Inventors: Michael Robert Daup; Brian Brent Naslund - Web page: https://patentgrep.com/patent/US11441963B1 ## CPC - G01L 19/0627: {Protection against aggressive medium in general} - G01P 5/14: by measuring differences of pressure in the fluid - B64F 5/60: Testing or inspecting aircraft components or systems - G01L 27/007: {Malfunction diagnosis, i.e. diagnosing a sensor defect} - G01P 5/165: Arrangements or constructions of Pitot tubes - G01L: MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE (weighing G01G) - G01P: MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT (measuring or recording blood flow A61B5/02, A61B8/06; monitoring speed or deceleration of electrically-propelled vehicles B60L3/00; vehicle lighting systems adapted to indicate speed B60Q1/54; determining position or course in navigation, measuring ground distance in geodesy or surveying G01C; combined measuring devices for measuring two or more variables of movement G01C23/00; measuring velocity of sound G01H; measuring velocity of light G01J7/00; measuring direction or velocity of solid objects by reception or emission of radiowaves or other waves and based on propagation effects, e.g. Doppler effect, propagation time, direction of propagation, G01S; measuring speed of nuclear radiation G01T; measuring acceleration of gravity G01V; {measuring or recording the speed of trains B61L23/00; speed indicators incorporated in motor vehicles B60K35/00; measuring frequency or phase G01R; traffic control G08G}) - B64F: GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR ## Abstract An aircraft pressure measurement device includes a pressure sensor, a pressure measurement path, a valve, and a fluid port. The pressure measurement path extends between an aircraft skin and the pressure sensor, and the valve is positioned within the pressure measurement path between the aircraft skin and the pressure sensor. The valve is configured to regulate airflow through the pressure measurement path, and the fluid port is configured to allow a pressurized fluid into the pressure measurement path to clear the pressure measurement path of debris. The improved pressure measurement device allows the aircraft to automatically clear debris from the pressure measurement path both during flight and while on the ground, removing the need for manual cleaning processes. ## Claims ### Claim 1 A pressure measurement device for use on an aircraft, the pressure measurement device comprising: a pressure sensor positioned within the aircraft; a pressure measurement path extending between the pressure sensor and an air inlet situated at a skin of the aircraft, wherein the pressure measurement path allows air to flow from outside the skin of the aircraft to the pressure sensor; a valve fluidly coupled to the pressure measurement path between the skin of the aircraft and the pressure sensor; and a fluid port configured to supply a clearing fluid, and selectively fluidly coupled to the pressure measurement path via the valve, wherein the valve is actuatable between at least two states: a closed state wherein the fluid port is fluidly isolated from the pressure measurement path, and an open state wherein the fluid port is fluidly connected to the pressure measurement path. ### Claim 2 (depends on 1) The pressure measurement device of claim 1, further comprising a maintenance port extending through the skin of the aircraft, wherein the maintenance port is fluidly coupled via a clearing fluid line to the fluid port as a source of the clearing fluid. ### Claim 3 (depends on 1) The pressure measurement device of claim 1, further comprising a fluid reservoir positioned within the aircraft, wherein: the fluid reservoir is configured to store the clearing fluid; the fluid reservoir is fluidly coupled to the pressure fluid port via a clearing fluid line; and the fluid reservoir is configured to supply the fluid into the pressure measurement path to clear debris from the pressure measurement path. ### Claim 4 (depends on 3) The pressure measurement device of claim 3, wherein the fluid reservoir is a compressed air tank configured to store compressed air as the clearing fluid. ### Claim 5 (depends on 3) The pressure measurement device of claim 3, wherein the fluid reservoir is a liquid tank configured to store a liquid as the clearing fluid. ### Claim 6 (depends on 1) The pressure measurement device of claim 1 and further comprising a pitot probe coupled to an exterior of the skin of the aircraft and fluidly coupled to the pressure measurement path. ### Claim 7 (depends on 1) The pressure measurement device of claim 1, further comprising an air bleed disposed from an engine of the aircraft to supply bleed air as the clearing fluid to the fluid port. ### Claim 8 (depends on 1) The pressure measurement device of claim 1, wherein the inlet includes at least one aperture extending through the skin of the aircraft. ### Claim 9 (depends on 1) The pressure measurement device of claim 1, wherein the inlet further comprises a pressure volume disposed adjacent the aircraft skin, and the at least one aperture comprises a plurality of apertures extending through the skin of the aircraft to the pressure volume. ### Claim 10 (depends on 1) The pressure measurement device of claim 1, wherein the clearing fluid is one or more of a cleaning solution, isopropyl alcohol, water, pressurized air, and pressurized gas. ### Claim 11 (depends on 1) The pressure measurement device of claim 1, wherein the valve interrupts the pressure measurement path, such that the valve fluidly isolates the pressure sensor from the inlet in the open state, and fluidly connects the pressure sensor to the inlet in the closed state. ### Claim 12 (depends on 1) The pressure measurement device of claim 1, wherein the valve is disposed adjacent the pressure measurement path, such that the pressure measurement path is not interrupted by the valve. ### Claim 13 A method of clearing debris from a pressure measurement device positioned adjacent a skin of an aircraft, the pressure measurement device comprising a pressure measurement path connecting an inlet to an inboard pressure sensor, the method comprising: fluidly connecting a source of clearing fluid to the pressure measurement path at a location inboard of the inlet and between the inlet and the pressure sensor; flushing the debris out the inlet by flow of the clearing fluid through the pressure measurement path, toward the inlet; and fluidly decoupling the source of clearing fluid from the pressure measurement path. ### Claim 14 (depends on 13) The method of claim 13, wherein the decoupling is achieved by actuating a valve into a closed state to block the source of clearing fluid from the pressure measurement path. ### Claim 15 (depends on 14) The method of claim 14, wherein the valve is fluidly coupled to the pressure measurement path between the skin of the aircraft and the pressure sensor. ### Claim 16 (depends on 14) The method of claim 14, wherein the valve interrupts the pressure measurement path, such that the valve fluidly isolates the pressure sensor from the inlet in an open state, and fluidly connects the pressure sensor to the inlet in the closed state. ### Claim 17 (depends on 14) The method of claim 14, wherein a controller is operatively coupled to the valve, and wherein the controller is configured to send command signals to the valve to initiate actuating the valve into the closed state. ### Claim 18 (depends on 13) The method of claim 13, further comprising receiving, by a controller, air pressure data from the pressure sensor indicating the presence of debris within the pressure measurement path. ### Claim 19 (depends on 18) The method of claim 18, wherein the pressure sensor indicating the presence of debris within the pressure measurement path of the pressure measurement device comprises: comparing, by the controller, the received air pressure data to a projected air pressure; establishing, by the controller, the received air pressure data deviates from the projected air pressure data by a threshold value; and outputting, by the controller, an indication of the presence of debris within the pressure measurement path. ### Claim 20 (depends on 18) The method of claim 18, wherein the pressure sensor indicating the presence of debris within the pressure measurement path of the pressure measurement device comprises: comparing, by the controller, the received air pressure data to air pressure data received from an adjacent pressure sensor; establishing, by the controller, the air pressure data of adjacent pressure sensors deviates by a threshold value; and outputting, by the controller, an indication of the presence of debris within the pressure measurement path.