Patents Represented by Attorney Robert L. Broad
  • Patent number: 5329089
    Abstract: A welding torch for plasma arc welding apparatus has a transparent shield cup disposed about the constricting nozzle, the cup including a small outwardly extending polished lip. A guide tube extends externally of the torch and has a free end adjacent the lip. First and second optical fiber bundle assemblies are supported within the guide tube. Light from a strobe light is transmitted along one of the assemblies to the free end and through the lip onto the weld site. A lens is positioned in the guide tube adjacent the second assembly and focuses images of the weld site onto the end of the fiber bundle of the second assembly and these images are transmitted along the second assembly to a video camera so that the weld site may be viewed continuously for monitoring the welding process.
    Type: Grant
    Filed: July 29, 1993
    Date of Patent: July 12, 1994
    Assignee: The United States of America as represented by the United States National Aeronautics and Space Administration
    Inventors: William F. McGee, Daniel J. Rybicki
  • Patent number: 5314500
    Abstract: An artificial manually positionable elbow joint for use in an upper extremity, above-elbow, prosthetic which provides a locking feature that is easily controlled by the wearer. The instant elbow joint is very strong and durable to withstand the repeated heavy loadings encountered by a wearer who works in an industrial, construction, farming or similar environment. The elbow joint of the present invention comprises a turntable, a frame, a forearm and a locking assembly. The frame generally includes a housing for the locking assembly and two protruding ears. The forearm includes an elongated beam having a cup-shaped cylindrical member at one end and a locking wheel having a plurality of holes along a circular arc on its other end with a central bore for pivotal attachment to the protruding ears of the frame.
    Type: Grant
    Filed: July 8, 1992
    Date of Patent: May 24, 1994
    Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space Administration
    Inventor: Bruce C. Weddendorf
  • Patent number: 5302805
    Abstract: The present invention relates to a device which is used to monitor the position of a filler wire relative to a base material being welded as the filler wire is added to a welding pool. The device is applicable to automated welding systems wherein nonconsumable electrode arc welding processes are utilized in conjunction with a filler wire which is added to a weld pool created by the electrode arc. The invention senses pressure deviations from a predetermined pressure between the filler wire and the base material, and provides electrical signals responsive to the deviations for actuating control mechanisms in an automatic welding apparatus so as to minimize the pressure deviation and to prevent disengagement of the contact between the filler wire and the base material.
    Type: Grant
    Filed: May 27, 1993
    Date of Patent: April 12, 1994
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Timothy B. Morris, Peter F. Milly, Sr., J. Kevin White
  • Patent number: 5302804
    Abstract: A welding torch for plasma arc welding apparatus has an inert gas applied circumferentially about the arc column externally of the constricting nozzle so as to apply a constricting force on the arc after it has exited the nozzle orifice and downstream of the auxiliary shielding gas. The constricting inert gas is supplied to a plenum chamber about the body of the torch and exits through a series of circumferentially disposed orifices in an annular wall forming a closure at the forward end of the constricting gas plenum chamber. The constricting force of the circumferential gas flow about the arc concentrates and focuses the arc column into a more narrow and dense column of energy after exiting the nozzle orifice so that the arc better retains its energy density prior to contacting the workpiece.
    Type: Grant
    Filed: June 25, 1993
    Date of Patent: April 12, 1994
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: William F. McGee, Daniel J. Rybicki
  • Patent number: 5281042
    Abstract: A saddle clamp assembly includes a hollow cylindrical body centered about a longitudinal axis and being diametrically split into semicircular top and bottom sections each having a pair of radially outwardly projecting connection flanges at their opposite ends. A pair of bolts are captively retained on the top section flanges and are threadable into nuts captively retained on the bottom section flanges. A base member is anchored to a central underside portion of the bottom clamp body section and has a pair of connection tabs positioned beneath the bottom clamp body section connection flanges on opposite sides of the clamp axis. A pair of bolts are captively retained on the base member connection tabs and are threadable into a pair of nuts captively retainable on a support structure. The connection tab and connection flanges on each side of the clamp body are axially offset in a manner permitting downward installation/removal tool access to the lower bolts past the connection flanges.
    Type: Grant
    Filed: November 17, 1992
    Date of Patent: January 25, 1994
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Adminstration
    Inventor: Charles R. Belrose
  • Patent number: 5279092
    Abstract: A rigid patch body for placing over and around a damaged portion (hole) of the external wall of a pressurized vessel, such as a space vehicle or habitat. The rigid patch body allows a person such as an astronaut to make temporary repairs to the pressurized vessel from the exterior of the vessel to enable more permanent repairs to be made from the interior of the vessel. The pressure wall patch of the present invention includes a floor surrounded by four side members. Each side member includes a threaded screw for anchoring the patch body to the external wall of the pressurized vessel and a recess in its lower surface for supporting an inflatable bladder for surrounding the damaged portion (hole) of the external wall to seal the area surrounding the damaged portion to allow the vessel to be repressurized. The floor of the rigid patch body supports a source of gas in communication with a gas supply valve and a gas supply gauge in communication with the gas supply valve and the inflatable bladder.
    Type: Grant
    Filed: October 15, 1992
    Date of Patent: January 18, 1994
    Assignee: The United States of America as represented by the Administrator, National Aeronautics and Space Administration
    Inventors: Joel E. Williamsen, Bruce C. Weddendorf
  • Patent number: 5267950
    Abstract: An articulated tang in clevis joint for incorporation in newly manufactured conventional strap-on orthotic knee devices or for replacing such joints in conventional strap-on orthotic knee devices. The instant tang in clevis joint allows the user the freedom to extend and bend the knee normally when no load (weight) is applied to the knee and to automatically lock the knee when the user transfers weight (load) to the knee, thus preventing a damaged knee from bending uncontrollably when weight (load) is applied to the knee.The tang in clevis joint of the present invention includes first and second clevis plates, a tang assembly and a spacer plate sandwiched and secured between the clevis plates. Each clevis plate includes a bevelled serrated upper section. A bevelled shoe is secured to the tang in close proximity to the bevelled serrated upper section of the clevis plates.
    Type: Grant
    Filed: December 26, 1991
    Date of Patent: December 7, 1993
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Bruce C. Weddendorf
  • Patent number: 5265994
    Abstract: In the space shuttle, a cargo bay storage rack was required which was to be manufactured from a metal-plastic composite and bolted to a cargo structure. Following completion, utilization of the rack was disallowed due to tolerances, that is, the size differences between the outside bolt diameter and the inside hole diameter. In addition to the space shuttle problem there are other close tolerance requirements for bolts. Such environments often benefit from close tolerance bolting. Frequently such fabrication is not cost effective. Consequently there is a need for means of achieving close tolerances between bolts and bolt holes. Such means are provided herein. After compressing the elements together a strong rigid plastic, ceramic, or ceramic plastic fluid is forced into a channel extending through the bolt.
    Type: Grant
    Filed: January 27, 1993
    Date of Patent: November 30, 1993
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: David L. Johnston, Phillip G. Bryant
  • Patent number: 5265415
    Abstract: Thrust chambers for liquid propellant rocket engines include three principal components. One of these components is an injector which contains a plurality of injection elements to meter the flow of propellants at a predetermined rate, and fuel to oxidizer mixture ratio, to introduce the mixture into the combustion chamber, and to cause them to be atomized within the combustion chamber so that even combustion takes place. Evolving from these injectors are tube injectors. These tube injectors have injection elements for injecting the oxidizer into the combustion chamber. The oxidizer and fuel must be metered at predetermined rates and mixture ratios in order to mix them within the combustion chamber so that combustion takes place smoothly and completely. Hence tube injectors are subject to improvement.
    Type: Grant
    Filed: January 27, 1993
    Date of Patent: November 30, 1993
    Assignee: The United States of America as represented by the administrator of the National Aeronautics and Space Administration
    Inventor: George B. Cox, Jr.
  • Patent number: 5256241
    Abstract: A method for controlling the crystallization of protein by solvent evaporation including placing a drop of protein solution between and in contact with a pair of parallel plates and driving one of the plates toward and away from the other plate in a controlled manner to adjust the spacing between the plates. The drop of solution forms a liquid cylinder having a height dependent upon the plate spacing thereby effecting the surface area available for solvent evaporation. When the spacing is close, evaporation is slow. Evaporation is increased by increasing the spacing between the plates until the breaking point of the liquid cylinder. One plate is mounted upon a fixed post while the other plate is carried by a receptacle movable relative to the post and driven by a belt driven screw drive. The temperature and humidity of the drop of protein solution are controlled by sealing the drop within the receptacle and mounting a heater and dessicant within the receptacle.
    Type: Grant
    Filed: August 28, 1992
    Date of Patent: October 26, 1993
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: David A. Noever
  • Patent number: 5254173
    Abstract: In vacuum plasma spraying a turntable must be provided which not only makes it possible to rotate and tilt a heavy workpiece, but to operate at vacuum plasma temperatures to do so. In the vacuum plasma coating of large parts such as combustion chambers of rocket engines the workpiece must not only be rotated, but it must be tilted. Hence the turntable must be capable not only of supporting heavy parts, but of angulating such heavy workpieces. And this must be done without drive means failure due to extremely high temperatures under which the turntable mechanism is operated. Herein a turntable mechanism is provided which is capable of operating under such conditions. For cooling the turntable drive mechanism internal cooling means are included.
    Type: Grant
    Filed: January 31, 1992
    Date of Patent: October 19, 1993
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: William N. Myers
  • Patent number: 5249357
    Abstract: A process for making a combustion chamber for a rocket engine wherein a copper alloy in particle form is injected into a stream of heated carrier gas in plasma form which is then projected onto the inner surface of a hollow metal jacket having the configuration of a rocket engine combustion chamber. The particles are in the plasma stream for a sufficient length of time to heat the particles to a temperature such that the particles will flatten and adhere to previously deposited particles but will not spatter or vaporize. After a layer is formed, cooling channels are cut in the layer, than the channels are filled with a temporary filler and another layer of particles is deposited.
    Type: Grant
    Filed: January 27, 1993
    Date of Patent: October 5, 1993
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Richard R. Holmes, Timothy N. McKechnie, Christopher A. Power, Ronald L. Daniel, Jr., Robert M. Saxelby
  • Patent number: 5248421
    Abstract: A fluid separator for separating particulate matter such as contaminates is provided which includes a series of spiral tubes of progressively decreasing cross sectional area connected in series. Each tube has an outlet on the outer curvature of the spiral. As fluid spirals down a tube, centrifugal force acts to force the heavier particulate matter to the outer wall of the tube, where it exits through the outlet. The remaining, and now cleaner, fluid reaches the next tube, which is smaller in cross sectional area, where the process is repeated. The fluid which comes out the final tube is diminished of particulate matter.
    Type: Grant
    Filed: October 9, 1992
    Date of Patent: September 28, 1993
    Assignee: The United States of America as respresented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Glen A. Robertson
  • Patent number: 5245885
    Abstract: A robotic joint wherein an elongated support member attached at one end to a base has the other end thereof pivotally attached to one end of a lever, the other end of the lever extending away from the support member. A tension strip extends along the support member and over the other end of the lever, the ends of the tension strip being attached to the base on opposite sides of the support member. A pair of bladders positioned between the tension strip and the support member on opposite sides thereof can be inflated to apply a tensile force to the strip and cause the lever to pivot, carring with it a finger which is attached to the lever.
    Type: Grant
    Filed: July 13, 1992
    Date of Patent: September 21, 1993
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Glen A. Robertson
  • Patent number: 5239864
    Abstract: A dynamic tester (10) for testing vibration damping seals and bearings is constructed having a hollow shaft (12) extending through the seal or bearing, with the shaft internally supported at each end by fluid bearings (19, 21) on hollow bosses (18, 20) connected to an interior of an enclosure (11) , with no rolling members connected to the shaft. A high pressure working fluid is forced through the hollow bosses (18, 20) to operate the bearings. Additionally, the shaft (12) is provided with a reaction turbine (32) that angularly vents a portion of the high pressure working fluid in order to rotate the shaft at high speed, up top 40,000 rpm. The seal or bearing (44) is mounted in a bushing (70), in turn supported by rods (80, 82, 86 of FIG. 3, or rods 72, 74 of FIG. 2) coupled by flex hinges (90, 90a of FIG. 3, 76, 76a of FIG. 2) to a shaking device (92 of FIG. 3, or 78 of FIG. 2) that vibrates the seal or bearing as the shaft is rotated.
    Type: Grant
    Filed: April 1, 1991
    Date of Patent: August 31, 1993
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: George L. von Pragenau
  • Patent number: 5226447
    Abstract: A detection system is provided for sensing a malfunction of a valve having an outlet connected to an end of a first pipe through which pressurized fluid may be flowed in a downstream direction away from the valve. The system includes a bypass pipe connected at its opposite ends to the first pipe and operative to bypass a portion of the fluid flow therethrough around a predetermined section thereof. A housing is interiorly divided by a flexible diaphragm into first and second opposite chambers which are respectively communicated with the first pipe section and the bypass pipe, the diaphragm being spring-biased toward the second chamber. The diaphragm housing cooperates with check valves and orifices connected in the two pipes to create and maintain a negative pressure in the first pipe section in response to closure of the valve during pressurized flow through the first pipe. A pressure switch senses the negative pressure and transmits a signal indicative thereof to a computer.
    Type: Grant
    Filed: October 7, 1992
    Date of Patent: July 13, 1993
    Assignee: The United States of America as represented by the Administration of the National Aeronautics and Space Administration
    Inventor: Richard K. Burley
  • Patent number: 5226308
    Abstract: A system for testing bearings wherein a pair of spaced bearings provide support for a shaft on which is mounted a bearing to be tested, with a bearing holder spaced from and in alignment with the pair of bearings. The bearing holder is provided with an annular collar positioned in an opening in the bearing holder for holding the bearing to be tested. A screw threaded through the bearing holder into engagement with the collar can be turned to move the collar radially out of alignment with the pair of bearings to apply a radial load to the bearing.
    Type: Grant
    Filed: December 26, 1991
    Date of Patent: July 13, 1993
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: John C. Gibson
  • Patent number: 5212718
    Abstract: A gamma ray collimator including a housing having first and second sections. The first section encloses a first section of depleted uranium which is disposed for receiving and supporting a radiation emitting component such as cobalt 60. The second section encloses a depleted uranium member which is provided with a conical cut-out focusing portion disposed in communication with the radiation emitting element for focusing the emitted radiation to the target.
    Type: Grant
    Filed: August 6, 1991
    Date of Patent: May 18, 1993
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Edgar J. Casanova
  • Patent number: 5211489
    Abstract: An outer race carrier (52) is constructed for receiving an outer race (26) of an antifriction bearing assembly (10). The carrier (52) in turn is slidably fitted in an opening (57) of a support wall to accommodate slight axial movements of a shaft (14). A plurality of longitudinal splines (54) on the carrier are disposed to be fitted into matching slots (56) in the opening (57). A deadband gap (60) is provided between sides of the splines and slots, with a radial gap (62) at ends of the splines and slots and a gap (59) between the splines and slots sized larger than the deadband gap. With this construction, operational distortions (slope) of the support wall are accommodated by the larger radial gaps (62, 59) while the deadband gaps (60) maintain a relatively high springrate of the housing. Additionally, side loads applied to the shaft are distributed between sides of the splines and slots, distributing such loads over a larger surface area than a race carrier (28) of the prior art.
    Type: Grant
    Filed: October 7, 1992
    Date of Patent: May 18, 1993
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventor: Jerry H. Moore
  • Patent number: 5173087
    Abstract: Gravitational phenomena, including convection, sedimentation, and interactions of materials with their containers all affect the crystal growth process. If they are not taken into consideration they can have adverse effects on the quantity and quality of crystals produced. As a practical matter, convection and sedimentation can be completely eliminated only under conditions of low gravity attained during orbital flight. There is, then, an advantage to effecting crystallization in space. But in the absence of of convection in a microgravity environment cooling proceeds by thermal diffusion from the walls to the center of the solution chamber. This renders control of nucleation difficult. Accordingly there is a need for a new and improved nucleation process in space. Herein crystals are nucleated by creating a small localized region of high relative supersaturation in a host solution at a lower degree of supersaturation.
    Type: Grant
    Filed: June 19, 1991
    Date of Patent: December 22, 1992
    Assignee: The United States of America as represented by the Administrator of the National Aeronautics and Space Administration
    Inventors: Roger L. Kroes, Donald A. Reiss, Sandor L. Lehoczky