Resources Contact Us Home
Browse by: INVENTOR PATENT HOLDER PATENT NUMBER DATE
 
 
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
Nuclear fuel assembly bottom nozzle
Systems and methods for mitigating spectral regrowth from non-linear systems
Method of making an array of nucleic acid colonies
Power management method for reducing power of host when turning off main monitor and computer system applying the same
Pre-fetching map data using variable map tile radius
Mixed reactant flow-by fuel cell
Case for camera
  Randomly Featured Patents
Traction control system using torque sensor for adaptive engine throttle control
Snare removing device for a drum
Door frame construction
Speaker grill
Process for extracting bitumen from tar sands
Apparatus for feeding sheets and method of determining the vertical position of stacked sheets
Trap and drain flush out kit
Dot recording method and dot recording apparatus
Direct preparation of pyrrolo[3,4-c]pyrroles
System and method for a reactive and personalized exposure of mobile end-user context to a third party