Patents by Inventor Michel M. A. A. Lechevalier

Michel M. A. A. Lechevalier has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 5611489
    Abstract: An actuating system for a variable area exhaust nozzle is disclosed having inner and outer flaps pivotally connected to an airframe whose positions may be varied by a single set of control cylinders. The control cylinders have a case in which is slidably mounted a pair of pistons, each having piston rods extending from one side, which piston rods extend through one end of the cylinder case. The piston rods may be arranged coaxially to minimize the bulk of the actuating cylinder. One of the piston rods is connected to the inner flaps, while the other of the piston rods is connected to the outer flaps.
    Type: Grant
    Filed: May 18, 1993
    Date of Patent: March 18, 1997
    Assignee: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation S.N.E.C.M.A.
    Inventors: Yves R. J. Berneuil, Christian W. B. Bettremieux, Daniel G. A. Kettler, Michel M. A. A. Lechevalier, Xavier J. Pasquali, Jean-Marie N. Pincemin
  • Patent number: 5578997
    Abstract: An apparatus for detecting fuel vapors in a turbojet engine oil tank is disclosed which incorporates a device in the oil tank which senses the presence of fuel vapors in the oil tank. The device has a housing defining an inner chamber in which a piston is slidably located. An actuating cartridge is also located in the chamber between an end wall of the housing and the piston. The cartridge comprises a material which expands in volume when subjected to heat and one which produces an exothermic reaction in the presence of fuel vapors. The housing defines one or more orifices to enable the atmosphere within the tank to communicate with the actuating cartridge.
    Type: Grant
    Filed: November 2, 1993
    Date of Patent: November 26, 1996
    Assignee: Societe Nationale D'Etude et de Construction de Moteurs D'Aviation S.N.E.C.M.A.
    Inventor: Michel M. A. A. Lechevalier
  • Patent number: 5548959
    Abstract: An adjustment valve is provided with a system able to prevent its piston from jamming. This piston (30) is fitted with a vane wheel (50) placed at its end and receiving a flow of air under pressure. The piston is thus in constant rotation inside the body (20) of the valve. Application is for the injection of fuels in turbojet engines.
    Type: Grant
    Filed: March 29, 1995
    Date of Patent: August 27, 1996
    Assignee: Societe Nationale D'Etude et de Construction de Moteurs D'Aviation "SNECMA"
    Inventor: Michel M. A. A. Lechevalier
  • Patent number: 5419360
    Abstract: A fluid supply system including a casing having at least one duct extending through it for the passage of fluid and a recess in the casing around the duct or ducts, a cover covering the recess and held against a bearing surface on the casing surrounding the recess, the cover carrying a continuation of the or each duct, and a vent in either the casing or the cover communicating the recess with the environment outside the casing, is provided with a leak tell-tale device for indicating passage of fluid along a path, such as the vent, which, in the event of a leakage of fluid from a duct into the recess, would be followed by the leaked fluid.
    Type: Grant
    Filed: December 3, 1993
    Date of Patent: May 30, 1995
    Assignee: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation "S.N.E.C.M.A."
    Inventor: Michel M. A. A. Lechevalier
  • Patent number: 5333644
    Abstract: A valve assembly is disclosed having a valve body with dual valve seats and movable valve member located in the valve body having dual sealing surfaces to bear against the two value seats. One of the valve seats has a sharp-edged configuration which is contacted by a generally frusto-conical sealing surface on a movable primary valve member to crush or break any foreign material in the fluid flow stream. The conical sealing surface and the sharp-edged valve seat also act as a seal to block the fluid flow passageway. A secondary valve member is attached to the primary valve member and has a second sealing surface configured to engage the second valve seat of the valve body. The second valve seat and the second sealing surface may be annular and each have a partially, spherical, cross-sectional configuration. The secondary valve member is connected to the primary valve member such that they may move relatively to each other along their axis of movement.
    Type: Grant
    Filed: January 12, 1994
    Date of Patent: August 2, 1994
    Assignee: Societe Nationale d'Etude et de Construction de Moteurs d'Aviation
    Inventors: Eddy F. M. G. Heyden, Christian LaCour, Michel M. A. A. Lechevalier, Christophe N. Riou