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
Receiving security risk feedback from linked contacts due to a user's system actions and behaviors
Pull through coronary sinus pacing lead
Broadband optical network apparatus and method
Post-processing including median filtering of noise suppression gains
Flat panel display device and stereoscopic display device
Stable aqueous composite compositions
Storage basket with lid
  Randomly Featured Patents
Herbicidal trans-2-[(3-chloroallyloxyimino)alkyl]-5-(substitutedsulfinylalkyl)-cycl ohexane-1,3-diones and derivatives thereof
Bonding structure for manifold assemblies
Secure communication system and method for exchanging data units
Liquid crystal compounds having a terminal alkoxy propenyl group
Contact lens cleaning composition containing lipid solvent and method of using
Temperature indicating paint
Method for producing viral vaccines
System and method for data mining of contextual conversations
Memory cartridge having a multi-memory controller with memory bank switching capabilities and data processing apparatus
Tumor therapy with high affinity laminin receptor-targeted vectors