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
Transaction cost recovery queue management
Image heating apparatus
Graphical user interface for interpreting the results of image analysis
Error detection and recovery tool for logical volume management in a data storage system
Adaptive take-off strips for smoothing ink consumption
Processing biomass
Activated carbon cryogels and related methods
  Randomly Featured Patents
Disc data storage apparatus with structure for preventing cracked disc from jetting out
Beverage dispensing system
Archery bow sight
Certain-phenoxy-phenoxy-alkylene-oxy-pyrimidines or symmetrical triazines, thio-analogues thereof, having insecticidal activity
Process and apparatus for generating a pesticidal gas
Method and system for announcing traffic engineering parameters of composite transport groups
Winged arrow rest
Toy mouse
Method and materials for conferring tripsacum genes in maize
Mass spectrometer