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
Oil extractor and the preparation method thereof
Mobile communication device and method for providing positioning information
In-vehicle communication system and method of operation
Methods of packaging imager devices and optics modules, and resulting assemblies
Data encoding and decoding apparatus and method thereof for verifying data integrity
Signal processing apparatus and methods
Image signal processing apparatus and image signal processing method
  Randomly Featured Patents
Modular fuel nozzle and method of making
Surface pattern for sheet goods
Dynamically generated schema representing multiple hierarchies of inter-object relationships
Active matrix type flat-panel display device
Controlled inventory device and method using pressure transducer
Refrigerating device with cooling of circulating air
Electrodeionization apparatus with resilient endblock
Rapid access tool
Top loading vertical axis washing/drying machine
Hunting retention system and method