Honeywell G.m.b.h.

Other

Jeffrey W Hegg

Wayne E Lance

William W Gregory

Larry James Yount

William F Potter

A dynamic gas-flow wound dressing assembly and method for enhancing the effect of generated gas flow across a wound creates spacing between a medical dressing cover and the wound to enhance ventilation. The assembly provides a medical dressing cover that covers a wound. The medical dressing couples to a gas flow framing structure having a gas inlet and enclosed gas outlets. A high rate gas flow is introduced through gas flow framing structure. The gas discharges to cross the wound. A scaffolding partition member serves as a resilient spacer between the gas flow framing structure and wound, enhancing ventilation by forces on the skin and directing gas flow. The scaffolding includes intake ports and outlet ports in fluid communication with inlets and outlets of gas flow framing structure. The scaffolding carries generated gas flow from the gas flow framing structure to wound, covering a larger gas flow volume across wound.

Dynamic gas-flow wound dressing assembly and method for enhancing the effect of generated gas flow across a wound

A medical gauze and gas flow assembly and method of applying a medical gauze with gas flow over a wound, provides a medical dressing cover that couples to a gas flow framing structure. The gas flow framing structure provides a flow of gas over a wound. A medical grade gauze material adheres to the lower surface of the medical dressing cover, so as to create spacing between the medical grade gauze material and the wound treatment area. The gas flow is directed between the medical grade gauze material and the wound treatment area. The gas flow vents to ambient though the gas permeable medical dressing cover. When degraded, the assembly is replaced or only the medical dressing cover and medical grade gauze material is replaced. The synergistic combination of a medical grade gauze material that is a gas permeable, with a gas flow structure that discharges gas over the wound enhances healing the wound.

Medical gauze and gas flow assembly and method of applying a medical gauze with gas flow on a wound

A hand controller system which provides the proper feel of the hand controller during aircraft operation. In both non-redundant and redundant embodiments, torque, and position measurements are made from the hand controller movements and processed to provide a feedback to a control motor in mechanical connection with the hand controller. The system includes self-monitoring of the motor, as well as the signals provided by the position, and torque sensors. Connections are provided from the hand controller system so that cross-coupling may be provided between the pilot's and copilot's hand controllers.

Active hand controller redundancy and architecture

A redundant active hand controller system has first and second motors connected to a common shaft. A compensator which differentiates a motor command signal from a first proportional and integral controller, differentiates a motor command signal from a second proportional and integral controller and subtracts the first differentiated motor command signal from the second differentiated motor command signal to provide a correction signal. The correction signal is summed with the error signal into the first proportional and integral controller to correct for slight differences in the integral control function of the first and second proportional and integral controllers.

Integrator management for redundant active hand controllers

An active hand controller system includes a moment cell for generating a signal representative of the force or torque applied to the stick of the hand controller by a user. The moment cell has an internal center of rotation and distributed masses are used to counterbalance the effect of inertial forces on the stick of the hand controller.

Moment cell counterbalance for active hand controller

Conventional column controls for aircraft flight control systems are replaced by active sidesticks which are connected to port and starboard aircraft mechanical, electrical or hydraulic systems by means of servo motors and cables. Movement of the active sidestick handles is detected and a signal generated to drive a servo motor in manner corresponding thereto, which in turn will drive cable assemblies which control aircraft flight control surfaces. Two sidesticks are provided, preferably with an electrical cross-cockpit interconnect to cause movement of one sidestick to result in a signal being transmitted to a second sidestick to cause the motor thereof to force the sidestick to track the movement of the first sidestick. In an alternative implementation, the sidesticks are employed in a fly-by-wire system with a conventional cable system as backup. The cable system is disengaged from the sidesticks by means of a disengage clutch whereupon failure of the fly-by-wire system, the clutch will engage the cable system and provide a mechanical backup to the fly-by-wire system in the event of failure thereof.

Mechanically linked active sidesticks

A state detector and loop compensation parameter controller for use with an active hand controller system having a single hand controller or having first and second hand controllers, processing and control means for the hand controllers and a flight control computer. The state detector and loop compensation parameter controller accepts a plurality of inputs and provides a plurality of adjustment signals to the processing and control means to improve the performance of the active hand controller system.

Variable servo loop compensation in an active hand controller

A servo controlled system is provided for electrically coupling the motions and applied forces of pilot and co-pilot control sticks. Servo-coupling between the two control sticks is accomplished by detecting the position of the control sticks of respective controllers and/or detecting torque exerted on the control sticks. The position and torques signals are processed and employed in a feedback loop for each control stick to generate a feedback signal to motors to which the control sticks are mechanically coupled. The motors act on the control stick to simulate the feel of traditional mechanical controllers, and to cause the controllers to track each other's movements.

Servo coupled hand controllers

An active hand controller system is provided wherein a feedback loop detects the position of a control stick to control a motor driving the control stick to thereby provide certain force feel characteristics to the control stick. The feedback loop includes a detector for detecting force exerted for the control stick to generate a signal indicative of the force or torque being applied to the control stick. In a more specific aspect, the invention includes the use of variable reluctance transformers, preferably in a push/pull configuration to detect the forces being exerted on the control stick.

Active hand controller feedback loop

A two-axis hand controller including a human interface to simulate feel parameters for use in a vehicle having a pitch axis and a roll axis. A hollow grip having a base end is connected to a swash plate through a rigid connecting member. A universal joint having a center shaft member rigidly affixed to a first support surface and having roll and pitch pivot axis members is attached within the center of the hollow grip so as to provide dual palm pivot points. The swash plate includes an opening positioned so as to accept the shaft member through the opening and into the hollow grip. The swash plate is also flexibly engaged to the first support surface so as to allow for control of the human interface feel parameters. Apparatus for transducing is attached between the swash plate and the base so as to provide electrical signals responsive to movements in the pitch and roll axes without cross-coupling from one axis to the other. Adding an elongated shaft member attached to a bearing mechanism mounted to a second supporting surface provides a third axis in the yaw direction. The swash plate is flexibly attached to the first support surface by at least four linear bearings wherein two of the linear bearings are disposed along the pitch axis and the other two are disposed along the roll axis, wherein each of the linear bearings is further connected to a flexible coupling which is connected to the transducer apparatus comprising a pick-off device.

Roll and pitch palm pivot hand controller

A hand controller for a control system, such as a flight control system, includes a control grip and an support assembly for supporting an operator's forearm so that the operator's wrist joint and hand extend forwardly of the support assembly and the operator's hand is positioned to grip the control grip. The controller also includes roll, pitch and yaw gimbal components. The roll gimbal component is movable about a fore-and-aft extending roll axis defined along a base line of the operator's forearm. The pitch and yaw gimbal components are movable about respective side-to-side extending pitch and up-and-down extending yaw axes defined through the center of the operator's wrist joint in orthogonal relation to one another and to the roll axis. The roll, pitch and yaw gimbal components are coupled to one another and to the control grip in a given sequence for facilitating pivotal motion of the operator's hand about the roll, pitch and yaw axes to activate hand control functions with minimal forearm movement. Also, the controller includes a plurality of transducers for sensing movement of the roll, pitch and yaw gimbal components and generating control signals in response thereto.

Hand controller having pivot axis for minimizing forearm movement

A float stabilized constant current source uses a floated cylinder with a rotational signal output generator and two torque generators for applying a linear torque and an opposing current squared torque to the floated cylinder, respectively. The current squared torque is balanced against the linear torque by a servo system applying a current to the torque generators in series to create a point of zero net torque on the floated cylinder. The current is obtained from the signal generator representative of a cylinder rotation and is used as a stabilized constant output current, i.e., a precision constant current reference driving an electrical load.

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North Redington Beach, FL, United States of America

Jeffrey W Hegg