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
Optical interconnect in high-speed memory systems
Peer-to-peer, internet protocol telephone system with proxy interface for configuration data
Waterproof wound protector
Methods of forming semiconductor devices having diffusion regions of reduced width
Catecholic butanes and use thereof for cancer therapy
High throughput thin film characterization and defect detection
Prevention and reduction of blood loss
  Randomly Featured Patents
Gearbox assembly
Fan with reduced noise generation
Automotive parts cleaning device with asbestos residue compartment
Assembler for enchilada shells
Suction device and supporting device having the same
Online taxonomy for constructing customer service queries
Arc welding robot control system and method thereof
Mutant E. coli strain with increased succinic acid production
Method and system for improving the locality of memory references during execution of a computer program