Flush-mount combined static pressure and temperature probe
AssigneeRosemount Aerospace Inc.
InventorLisa Graham
Life of this patent
Estimating the term…
Loading patent…
AssigneeRosemount Aerospace Inc.
InventorLisa Graham
Estimating the term…
A pressure and temperature probe includes a probe head, a probe tip extending from the probe head and ending with a sensor face, a pressure channel extending into the probe tip through the sensor face, and a temperature channel extending into the probe tip through the sensor face. A pressure sensor is in fluid communication with a pressure channel and a temperature sensor in fluid communication with the temperature channel. The temperature channel extends parallel to the pressure channel, and the temperature channel is fluidly separate from the pressure channel. The sensor face can be configured to minimally intrude the flowpath of a working fluid, thereby minimizing disruption of the flowpath. The probe can be configured on a gas turbine engine.
A gas turbine engine extending along an axis comprising:
A probe comprising:
A gas turbine engine extending along an axis comprising:
Dependencies are inferred from the claim text.