# US 2016/0258792 A1 · Conduit > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 2016/0258792 A1 - Document ID: US20160258792A1 - Status: Published application - Kind: A1 - Application number: 15/035,005 - Filed: 2014-11-03 - Published: 2016-09-08 - Earliest claimed: 2013-11-06 - Assignees: BAE SYSTEMS plc - Applicants: Bae Systems PLC - Inventors: Mark Alfred POTTER - Web page: https://patentgrep.com/patent/US20160258792A1 ## CPC - G01F 1/46: Pitot tubes - G01L 19/0023: {for flowthrough systems having a flexible pressure transmitting element} - G01F: MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME - G01L: MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE (weighing G01G) ## Abstract Disclosed is a conduit (4) comprising a conduit wall defining a flow channel through which a fluid may flow and a plurality of further channels (24) through at least part of the conduit wall. Each further channel (24) comprises a first end (20) and a second end (22). The first ends (20) of the further channels (24) are spaced apart along a length of the conduit (4) and comprise openings in fluid communication with the flow channel of the conduit (4). The second ends (22) of the further channels (24) are located proximate to one another (e.g. substantially collocated) such that the distance between the second ends (22) of any two further channels (24) is smaller than the distance between the first ends (20) of those two further channels (24). Pressure sensors (26) may be coupled to the second ends (22) of the further channels, which may be closed. ## Claims ### Claim 1 A conduit comprising: a conduit wall defining a flow channel through which a fluid may flow; and a plurality of further channels, each of the further channels being formed within the conduit wall; wherein each further channel comprises a first end and a second end opposite to the first end; for each further channel, the first end of that further channel comprises an opening in fluid communication with the flow channel of the conduit; the first ends of the further channels are spaced apart along a length of the conduit; the second ends of the further channels are located proximate to one another such that the distance between the second ends of any two further channels is smaller than the distance between the first ends of those two further channels, and the conduit having been produced using an Additive Manufacturing process. ### Claim 2 (depends on 1) The conduit according to claim 1, wherein at least part of at least one further channel runs longitudinally within the conduit wall along at least part of the length of the conduit wall. ### Claim 3 (depends on 2) The conduit according to claim 2, wherein, for each of the plurality of further channels at least part of that further channel runs longitudinally within the conduit wall along at least part of the length of the conduit wall. ### Claim 4 (depends on 1) The conduit according to claims 1, wherein each part a further channel that runs longitudinally within the conduit wall along at least part of the length of the conduit wall is substantially parallel with the flow channel defined by the conduit wall. ### Claim 5 (depends on 1, 2, 3, 4) The conduit according to any of claim 1 to 4, wherein the opening of one or more of the further channels is arranged such that, when a fluid flows through the flow channel of the conduit, that opening is directed upstream. ### Claim 6 (depends on 1) The conduit according to claim 1, wherein the opening of one or more of the further channels is arranged such that, when a fluid flows through the flow channel of the conduit, that opening is a static port in communication with the fluid in a relatively undisturbed area. ### Claim 7 (depends on 1) The conduit according to claim 1, wherein: the conduit comprises one or more elongate potions extending from an internal surface of the conduit wall into the flow channel of the conduit; and for each elongate portion, an opening of one or more of the further channels is located at or proximate to a distal end of that elongate portion. ### Claim 8 (depends on 7) The conduit according to claim 7, wherein at least one of the elongate members comprises at least two openings at or proximate to its distal end, a first of these openings being arranged such that, when a fluid flows through the flow channel of the conduit, that opening is directed upstream, and a second of these openings being arranged such that, when a fluid flows through the flow channel of the conduit, that opening is a static port in communication with the fluid in a relatively undisturbed area. ### Claim 9 (depends on 1) The conduit according to claim 1, wherein the second ends of the further channels are closed ends. ### Claim 10 (depends on 1) The conduit according to claim 1, wherein the conduit further comprises a plurality of pressure sensors; each pressure sensor is coupled to a respective further channel at the second end of that further channel; and each pressure sensor is configured to measure a pressure in the further channel to which that pressure sensor is coupled. ### Claim 11 (depends on 1) The conduit according to claim 1, wherein the second ends of the further channels are substantially co-located. ### Claim 12 (depends on 1) The conduit according to claim 1, wherein each of the further channels is wholly within the conduit wall. ### Claim 13 (depends on 1) The conduit according to claim 1, the conduit being a single item. ### Claim 14 (depends on 1) An aircraft comprising: a first aircraft system; a second aircraft system; and a conduit according to claim 1; wherein the conduit couples the first aircraft system to the second aircraft system such that a fluid may be caused to flow from the first aircraft system to the second aircraft system through the flow channel of the conduit. ### Claim 15 (depends on 1) A method of measuring fluid pressure comprising: providing a first system; providing a second system; coupling a conduit according to claim 1 between the first system and the second system causing a fluid to flow through the flow channel of the conduit from the first system to the second system; and measuring a pressure within one or more of the further channels. ### Claim 16 (depends on 15) The method according to claim 15, in which the first and second systems are aircraft systems located on board an aircraft. ### Claim 17 (depends on 1) The method of producing a conduit according to claim 1, the method comprising producing a digital model of the conduit, and, using the digital model of the conduit, controlling an Additive Manufacturing apparatus to perform the Additive Manufacturing process to produce the conduit as specified by the digital model.