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
Laser protection polymeric materials
Method and system for providing complete internet anywhere with partial server processing
Semiconductor device with hetero-junction bodies
Computer device with digitizer calibration system and method
Locking flange
Circuit breakers
Method of operating an electromechanical converter, a controller and a computer program product
  Randomly Featured Patents
Carbonation device
Sheet feeding device, sheet treating device and image reading apparatus using the same
Intermediate memory array with a parallel port and a buffered serial port
Loading system
Document processing system capable of simultaneously displaying two continuous document pages in accordance with a selected binding position
Broom with adjustable handle
Method and system for power control in wireless networks using interference prediction with an error margin
Low CO cigarette
Burner control apparatus