Resources Contact Us Home
Gas turbine engine and composite parts

Image Number 8 for United States Patent #4738902.

High strength, fracture tough, high temperature oxidatively stable, gas turbine engine core engine components are described made of silicon carbide fiber reinforced ceramic matrix or silicon carbide fiber reinforced glass matrix material. A gas turbine engine containing core engine components as above described is also disclosed.

  Recently Added Patents
High power fiber amplifier with stable output
Apparatus and methods for providing efficient space-time structures for preambles, pilots and data for multi-input, multi-output communications systems
Encoder that detects positional information of a moving body generating interference fringes that move in opposite directions
.beta.-2 microglobulin as a biomarker for peripheral artery disease
IR(voltage) drop analysis in integrated circuit timing
Playback device for stereoscopic viewing, integrated circuit, and program
Sample analysis and/or sample processing system
  Randomly Featured Patents
Solution warming unit
Fishing lure retriever
Highly thermostable fluorescent proteins
NMR analyzers for clinical evaluation of biosamples
Planters having light-transmitting enclosures
Non-metallic anti-knock fuel additive
Electromechanical filling indicator for pattern-controlled weaving loom
Reversing ratchet
Interrupt and status reporting structure and method for a timeslot bus