Resources Contact Us Home
Thermocouple probe

Image Number 3 for United States Patent #5678926.

A thermocouple probe 10 suitable for use in a gas turbine engine comprises a thermocouple element 12 which is coaxially arranged inside a protective sheath 16. The thermocouple element 12 is resiliently supported by a helical member 18 which insulates the element 12 from deleterious vibrations induced in the sheath 16. In use, the thermocouple probe 10 projects through an aperture 30 in the casing 32 of a gas chamber 34. Vibrations in the probe 10 are further reduced by ensuring that the longitudinal axis AA of the probe is angularly offset from the central axis BB of the aperture 30, such that the outer periphery of the sheath 16 is in contact with the inner periphery of the aperture 30 in two diametrically opposite and axially offset locations.

  Recently Added Patents
Mobile browser context switching
Proximity search methods using tiles to represent geographical zones
Touch panel structure and manufacturing method thereof
Color imaging device
Invisible fence battery charger
Method of producing probabilities of being a template shape
Providing policy-based operating system services in an operating system on a computing system
  Randomly Featured Patents
On-chip circuit to compensate output drive strength across process corners
Needle capture mechanisms
Method system and program for determining a test case selection for a software application
Method and kit having layered device for detecting biological component by interference color
Aerospace vehicle
Method of fabricating a thin-film magnetic recording medium and thin-film magnetic recording medium
Wiring board with conductive wirings and protrusion electrodes
Air bag for air bag apparatus
Indexing hinge