Patents Assigned to Avco Lycoming
  • Patent number: 4896815
    Abstract: A combination of unique properties of (i) high strength and stiffness at temperatures up to about 1500.degree. F., (ii) good room temperature mechanical properties including good ductility and (iii) improved resistance to matrix cracking is achieved in a titanium structure by forming a hybrid titanium alloy matrix composite in which the matrix consists of layers of at least two alloys, i.e. a high temperature-resistant titanium aluminide alloy and a ductile, lower modulus titanium alloy, that are bonded metallurgically to each other in various embodiments. A reinforcing material in the form of filaments, fibers or whiskers, e.g. silicon carbide, can be embedded within either or both types of the titanium layers.
    Type: Grant
    Filed: August 4, 1988
    Date of Patent: January 30, 1990
    Assignee: Avco Lycoming
    Inventors: Dan G. Rosenthal, Joseph A. Goebel
  • Patent number: 4832999
    Abstract: Honeycomb structure assemblies comprising walled structures which admit fluid such as air for purposes of cooling or heating the walls thereof or for other purposes. The assemblies comprise spaced inner and outer walls united by means of an internal honeycomb structure comprising aligned cells having opposed interior and exterior gaps open to adjacent cells, which causes the admitted fluid to undulate through said gaps into contact with both of the walls, such as for uniform cooling or heating. The honeycomb structure contains flanges which are secured to one or both walls for uniform strength and resistance to separation under the stress of use.
    Type: Grant
    Filed: October 27, 1987
    Date of Patent: May 23, 1989
    Assignee: Avco Lycoming/Textron
    Inventor: E. Jack Sweet
  • Patent number: 4816347
    Abstract: A combination of unique properties of (i) high strength and stiffness at temperatures up to about of 1500.degree. F., (ii) good room temperature mechanical properties including good ductility and (iii) improved resistance to matrix cracking is achieved in a titanium structure by forming a hybrid titanium alloy matrix composite in which the matrix consists of layers of at least two alloys, i.e. a high temperature-resistant titanium aluminide alloy and a ductile, lower modulus titanium alloy, that are bonded metallurgically to each other in various embodiments. A reinforcing material in the form of filaments, fibers or wiskers, e.g. silicon carbide, can be embedded within either or both types of the titanium layers.
    Type: Grant
    Filed: May 29, 1987
    Date of Patent: March 28, 1989
    Assignee: Avco Lycoming/Subsidiary of Textron, Inc.
    Inventors: Dan G. Rosenthal, Joseph A. Goebel