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 Manageability tools for lossless networks Housing structure for a slide type mobile communication terminal Creation of user digital certificate for portable consumer payment device Light emitting diode lamp TCP-aware power control in wireless networks Power sequence control circuit, and gate driver and LCD panel having the same Secure folder with double binder   Randomly Featured Patents Light modulating microdevice and method Refrigerant recovery machine Regenerative braking system and method using air conditioning system of electric vehicle Process for polymerizing 1-butene Surface acoustic wave element, method of producing the same, and method of changing resonation frequency of the same Golf accessory clip Remover for injection-molded article Method and device for manufacturing a double-walled, thermoplastic tube with a connecting sleeve Method and apparatus for determining flow rates of well fluid constituents Kitchen utensil having a length adjusting device © 2006-2008 PatentGenius. All Rights Reserved.