Abstract: A customizable length averaging pitot tube (APT) probe for insertion into a confined conduit, such as a process pipe, is disclosed. The APT probe includes a probe portion, configured to be inserted into the confined conduit, which includes longitudinally extending upstream, downstream and middle surfaces to form first and second fluid carrying plenums within the APT probe portion. A plurality of longitudinally arranged openings are disposed along the length of the upstream surface with each opening in fluid communication with the first fluid carrying plenum. A plurality of longitudinally arranged openings are disposed along the length of the downstream surface with each opening in fluid communication with the second fluid carrying plenum. A cap is affixed to an end of the APT probe portion to isolate the first and second fluid carrying plenums at the end of the APT probe portion.
Type:
Application
Filed:
September 17, 2013
Publication date:
March 19, 2015
Applicant:
Dieterich Standard, Inc.
Inventors:
Brian Anthony Fieser, John Everett Garnett
Abstract: An electric pressure probe for an aircraft comprises: a pitot tube assembly for collecting pneumatically air pressure in the vicinity of the assembly; a strut including one end mountable to a surface of the aircraft, the pitot tube assembly being coupled to another end of the strut for being supported away from the aircraft surface; a pressure sensor integral to the strut and pneumatically coupled to the pitot tube assembly for converting the pneumatic pressure collected thereby to an electrical pressure signal; and circuitry integral to the strut and coupled to the pressure sensor for signal conditioning the electrical pressure signal, the circuitry including at least one output lead for conducting the conditioned electrical signal from the probe.