Patents Represented by Attorney Morris A. Case
  • Patent number: 4706797
    Abstract: A first unit positions and then rotates an apple with a randomly oriented core. Rotation is stopped when any one of a series of aligned probes enters into one of the indents in the core of the apple. A second unit with axis of rotation at 90 degrees from the axis of rotation of the first unit takes and holds the positioned apple, and then rotates it. Rotation is stopped when a positioned probe enters into the indent in the core to align the core of the apple in the desired position to provide apple core alignment.
    Type: Grant
    Filed: March 11, 1986
    Date of Patent: November 17, 1987
    Inventor: Richard L. Carlson
  • Patent number: 4662587
    Abstract: A pair of specially reinforced skin-spar joints in combination with a honeycomb core are used to build up a wing spar for a composite airplane wing. A series of contoured mandrels with a covering of fuel resistant material and a wrapped reinforced plastic are aligned one above the other. The wing spar materials are placed between the mandrels, honeycomb core is located alongside as well as wing skins to form a wing buildup. The buildup is placed in a mold, pressure applied to each mandrel forcing all the parts together, and the buildup heated to cure the resins and form a composite wing structure.
    Type: Grant
    Filed: June 10, 1985
    Date of Patent: May 5, 1987
    Assignee: The Boeing Company
    Inventor: Philip C. Whitener
  • Patent number: 4569158
    Abstract: A pair of support members are slideably inserted into a rectangular shaped open ended housing from opposite ends of the housing. Each support member has a downwardly extending projection to form facing cutting surfaces. A resilient member presses the support members toward each other forming a ski sharpener. When the sharpener is placed against and moved along a ski the cutting surfaces sharpen the sides of the ski.
    Type: Grant
    Filed: September 16, 1983
    Date of Patent: February 11, 1986
    Inventor: David M. Curmi
  • Patent number: 4568045
    Abstract: A shaped support beam is joined to and extends laterally across a landing gear door to provide support and to hold a retracted airplane landing gear in position when the landing gear door is closed. Pivotable linkage, extending between airplane structure and the shaped support beam, press against the landing gear to hold the gear in the retracted position with the door latched, and to be pressed against to move an unlatched door aside to permit extension of the landing gear into operating position.
    Type: Grant
    Filed: August 17, 1983
    Date of Patent: February 4, 1986
    Assignee: The Boeing Company
    Inventor: John D. Mayer
  • Patent number: 4565595
    Abstract: A pair of specially reinforced skin-spar joints in combination with a honeycomb core are used to build up a wing spar for a composite airplane wing. A series of contoured mandrels with a covering of fuel resistant material and a wrapped reinforced plastic are aligned one above the other. The wing spar materials are placed between the mandrels, honeycomb core is located alongside as well as wing skins to form a wing buildup. The buildup is placed in a mold, pressure applied to each mandrel forcing all the parts together, and the buildup heated to cure the resins and form a composite wing structure.
    Type: Grant
    Filed: June 6, 1983
    Date of Patent: January 21, 1986
    Assignee: The Boeing Company
    Inventor: Philip C. Whitener
  • Patent number: 4560123
    Abstract: A four bar linkage, between a hinge carriage segment and a translating door segment, of an outward opening overhead rotation plug type aircraft door, defines the relative movement between the two segments. A door handle actuates linkages that extend between the two segments to power the relative movement. When the handle is in either the down and the door locked position, or in the up and unlocked ready for outward rotation position, the linkage is overcenter so that the handle remains in position. A safety link extends between the two segments to provide fail safe locking at either handle position.
    Type: Grant
    Filed: September 30, 1982
    Date of Patent: December 24, 1985
    Assignee: The Boeing Company
    Inventors: Francis Sealey, Richard H. Weiland
  • Patent number: 4557442
    Abstract: A high strength braided thermosetting resin cord acts as a core for an escape line. A series of knobs of a foamed resin are threaded onto the core at spaced intervals with a second series of smaller knobs of a foamed resin located between each adjacent larger knobs. Each of the knobs are bonded with a thermosetting resin to the core. A high strength thermosetting resin is braided over the knobs and core, and one end of the cord is secured to a support member of an airplane to provide an escape line.
    Type: Grant
    Filed: September 14, 1983
    Date of Patent: December 10, 1985
    Assignee: The Boeing Company
    Inventors: John E. Krezak, Michael F. Lamb
  • Patent number: 4557401
    Abstract: A control unit for a squeeze type fluid container is attached to a tube extending from inside the container to the outside. The control unit has a check valve resiliently held to open in response to pressure inside the container; which permits fluid to flow through the control unit and out the tube. The control valve has a second check valve positioned inside the first check valve casing, and resiliently held to open in response to a negative pressure inside the container to permit fluid to flow from the tube through the control unit and back into the container.
    Type: Grant
    Filed: December 1, 1983
    Date of Patent: December 10, 1985
    Assignee: The Boeing Company
    Inventor: John G. Hodge
  • Patent number: 4551918
    Abstract: A set of two cutting units are located on the end of a tool to be rotated. The cutting units are radially aligned and on a bevel. Each blade on each cutting unit has a radial rake of at least 60 degrees, a clearance angle, and serrations cut at an angle normal to the cutting edge to provide a series of points extending along that cutting edge.
    Type: Grant
    Filed: March 26, 1984
    Date of Patent: November 12, 1985
    Assignee: The Boeing Company
    Inventor: Dudley G. Smithberg
  • Patent number: 4545102
    Abstract: An index bar is secured to a machined and leveled surface of a base. One side of the bar is machined to be contacted and to act as a buttock plane. The bar has a series of in line holes positioned for lengthwise indexing. A second index bar, secured to the base, has a series of matching holes and the bar is positioned parallel to the buttock plane. The index bars are used for alignment for scribing header locations on the base. Headers, contoured with respect to the base surface and with respect to the buttock plane, are formed and while on the scribed line and while contacting the base and the buttock plane surface, are secured to the base. The secured headers are vertically aligned and held in that position to provide the critical lines for forming a master model.
    Type: Grant
    Filed: May 23, 1983
    Date of Patent: October 8, 1985
    Assignee: The Boeing Company
    Inventor: Fred F. Grabos
  • Patent number: 4541137
    Abstract: An elongated flat arm is joined at one end to the outer side of one of a pair of spaced apart legs, with that leg extending at about 90 degrees to the arm. The legs are joined together at one end, and are open ended at the other end. Inwardly directed cooperating projections are located adjacent the open end. A latch having a knobbed end is joined intermediate the length of the joined leg, and that latch extends towards and works in combination with an opening through the opposite leg to hold the legs together.
    Type: Grant
    Filed: November 28, 1983
    Date of Patent: September 17, 1985
    Inventor: Lester K. Murray
  • Patent number: 4526641
    Abstract: A laminate of a plurality of thermosetting resin films are joined together with a thermosetting resin to impart a peel strength between films of about 1 to 3 pounds per inch of width.
    Type: Grant
    Filed: September 6, 1983
    Date of Patent: July 2, 1985
    Assignee: The Boeing Company
    Inventors: Matthias P. Schriever, Chun-Ming Wong
  • Patent number: 4515260
    Abstract: A guide bar reciprocally movable at an inclined angle accepts a fastener in an upper leg of the guide bar when in a retracted position, moves that fastener past a stationary member and drops it onto a lower leg of the guide bar when in the extended position. A movable pin contacts the lower end of the fastener and acts as a reference when that pin is in the extended position. The guide bar when it is retracted is at a distance less than the length of the fastener from the reference point. If the fastener, which has a shallow recess on one end and a deep recess on the other end, has the shallow recessed end down that end will drop down when the pin is retracted. If the deep recessed end is down the fastener will rotate around the pin and drop the shallow recessed end down.
    Type: Grant
    Filed: March 28, 1983
    Date of Patent: May 7, 1985
    Assignee: The Boeing Company
    Inventor: David L. Wagner
  • Patent number: 4515152
    Abstract: A pair of boots each having an outer shell and an inner resilient liner are each contoured to fit at the juncture between a person's foot and leg. The shell and liner of each contoured boot have extended ends that are folded over each other, and secured in the folded position to the person's leg. A support member, attached to the front of the shell, in turn provides for inverted suspension of the person from an independent support member, and a loop attached to the front of the shell extends to contact the back of the person's leg to give torque free suspension to a person wearing the boots.
    Type: Grant
    Filed: May 17, 1982
    Date of Patent: May 7, 1985
    Inventor: Roger C. Teeter
  • Patent number: 4515044
    Abstract: A cylinder is rotatably located in a head of a wrench. Ratchet teeth located in a groove around the periphery of the cylinder acts in conjunction with a pawl to secure the cylinder in position and to provide ratchet action. An insert with axially located socket rotates with the cylinder to act on a fastener.
    Type: Grant
    Filed: October 23, 1980
    Date of Patent: May 7, 1985
    Inventor: Larry V. Harstad
  • Patent number: 4485709
    Abstract: A sliding block with a female die acts in conjunction with a four bar linkage mounted block with a male die to punch indexing holes in a moving metal strip. The block with male die continually seeks to rotate, but is held in position by the sliding block. The sliding block is programmed to periodically move forward at the speed of the moving metal strip and to return to starting position. This frees the male die to rotate to punch out the hole, and to continue to rotate back into the starting position to be held by the returned sliding block.
    Type: Grant
    Filed: May 20, 1982
    Date of Patent: December 4, 1984
    Assignee: The Boeing Company
    Inventors: Doyle W. Huber, Richard H. Smith, Robert L. Strong
  • Patent number: 4477044
    Abstract: A constant force mechanical spring and a varying force hydraulic actuator combine to provide feel to a pilot of his movement of an airplane's elevators. A constant force bias spring works against the hydraulic actuator to reduce the actuators effectiveness to nearly zero at minimum feel force conditions.
    Type: Grant
    Filed: January 17, 1983
    Date of Patent: October 16, 1984
    Assignee: The Boeing Company
    Inventors: Kevin A. Darcy, Terence F. H. Faithfull
  • Patent number: 4470312
    Abstract: A torque measuring device has a torsion bar with effective length adjustable to show different energy absorption capability. One end of the torsion bar's effective length is held stationary while a torque from a torque controlled winding tool is applied to the other end through a one direction of rotation clutch. The actual torque applied to the torsion bar is measured after which the torque on the bar is released.
    Type: Grant
    Filed: September 29, 1982
    Date of Patent: September 11, 1984
    Assignee: The Boeing Company
    Inventor: Douglas Thompson
  • Patent number: 4460657
    Abstract: Flat metal stock is contoured into a shaped blank prior to being superplastically formed into a finished part. The stock is shaped in steps.
    Type: Grant
    Filed: March 20, 1981
    Date of Patent: July 17, 1984
    Assignee: The Boeing Company
    Inventors: Samuel D. Elrod, DeVere V. Lindh
  • Patent number: 4450661
    Abstract: A composite structure window belt has a roll of the lined reinforced plastic window frames set between honeycomb core and covered top and bottom with a reinforced plastic cover. The window frames have built-in reinforcements to accept fasteners for securing windows within the diamond-shaped openings.
    Type: Grant
    Filed: September 30, 1981
    Date of Patent: May 29, 1984
    Assignee: The Boeing Company
    Inventor: Philip C. Whitener