In accordance with the invention, features can be directly imprinted into the surface of a solid substrate. Specifically, a substrate is directly imprinted with a desired pattern by the steps of providing a mold (20) having a molding surface (21) to imprint the pattern, disposing the molding surface adjacent or against the substrate (24) surface (25) to be imprinted, and irradiating the substrate surface with radiation to soften or liquefy the surface. The molding surface is pressed into the softened or liquefied surface to directly imprint the substrate. The substrate can be any one of a wide variety of solid materials such as semiconductors, metals, or polymers. In a preferred embodiment the substrate is silicon, the laser is a UV laser, and the mold is transparent to the UV radiation to permit irradiation of the silicon workpiece through the transparent mold. Using this method, applicants have directly imprinted into silicon large area patterns with sub-10 nanometer resolution in sub-250 nanosecond processing time. The method can also be used with a flat molding surface to planarize the substrate.

Laser assisted direct imprint lithography

In accordance with the invention, an article comprising a nanoscale surface pattern, such as a grating, is provided with a nanoscale patterns of reduced edge and/or sidewall roughness. Smooth featured articles, can be fabricated by nanoimprint lithography using a mold having sloped profile molding features. Another approach uses a mold especially fabricated to provide smooth sidewalls of reduced roughness, and a third approach adds a post-imprint smoothing step. These approaches can be utilized individually or in various combinations to make the novel articles.

Articles Comprising Nanoscale Patterns With Reduced Edge Roughness and Methods of Making Same

The present invention provides an integrated self-contained lighting module which can be used on its own, or in conjunction with other modules to produce white light, or light of any other colour within the colour spectrum. Each module comprises one or more light-emitting elements, a drive and control system, a feedback system, thermal management system, optical system, and optionally a communication system enabling communication between modules and/or other control systems. Depending on the configuration, the lighting module can operate autonomously or its functionality can be determined based on either or both internal signals and externally received signals.

Integrated Modular Light Unit

System and method for selectively applying electrical energy to structures within or on the surface of a patient's body and controlling the flow of an electrically conductive fluid from the application site to provide or maintain a desired operating condition of the electrosurgical device. An electrosurgical probe is in communication with a fluid transport apparatus through a fluid transport lumen having an opening at an end proximate the application site and disposed proximate the electrosurgical probe. A controller in communication with the fluid transport apparatus provides control signals to the fluid transport apparatus in response to at least one operating parameter associated with the system. Based on the received control signals, the fluid transport apparatus adjusts a flow rate of the electrically conductive fluid at the application site through the fluid transport lumen in response to at least one operating parameter associated with the system.

Electrosurgical system with suction control, apparatus, system and method

A solid state sub-nanometer-scale electron beam emitter comprising a multi-layered structure having a nano-tip electron emitter and tunnel emission junction formed on substrate, an initial electron beam extraction electrode, a “nano-sandwich Einzel” electrode, and a topmost protective layer.

Integrated sub-nanometer-scale electron beam systems

A permanent wireless onboard to ground operations communications system is provided for an aircraft equipped with a pilot-controllable drive wheel drive system for autonomous ground movement without reliance on the aircraft's engines or external tow vehicles, including an onboard wireless communications link installed to remain permanently with the aircraft designed to interface wirelessly with ground personnel at any airport, aerodrome, or airfield where the aircraft lands immediately upon landing. The permanent wireless onboard to ground operations communications system provides a substantially instantaneous connection between a pilot and ground personnel to facilitate guidance of pilot-controlled autonomous ground movement during taxi, parking in nose-in and parallel orientations, and pushback without reliance on visual signals. The present communications system establishes and maintains cockpit to ground communications during pilot-controlled autonomous aircraft ground movement to enhance the safety of ramp operations and improve the speed at which ramp operations can be safely conducted.

Permanent wireless communications system for an aircraft equipped with a wheel drive system

A system is provided for maximizing efficient ground travel in wide-body and other aircraft equipped with onboard non-engine drive means for autonomous ground travel. Selective operation of the non-engine drive means and selective operation of the aircraft's engines are integrated to power aircraft movement when different ground travel speeds are required between landing and takeoff, optimizing savings and maximizing the cost/benefit ratio for equipping the aircraft with a non-engine drive means. The non-engine drive means may be designed to move a wide-body aircraft at low speeds required for ground maneuvers in a ramp area to move the aircraft at speeds typically used for pushback, initial forward roll, all start-stop situations, and other low speed ground travel. One or more of the aircraft's engines may be operated to move the aircraft at higher taxi speeds.

Optimizing ground movement in a wide-body aircraft equipped with non-engine drive means

A monitoring system is provided to ensure continued efficient reliable operation of an aircraft drive wheel drive system, preferably an aircraft drive wheel drive system driven by actuating drive system-actuated drive means, designed to drive an aircraft autonomously during ground operations. The monitoring system includes an array of sensor elements capable of obtaining desired information relating to selected drive system operating parameters and performance indicators during aircraft ground operations. The sensor elements are designed to be functionally located externally of drive system components to obtain information during aircraft ground movement under a range of operating conditions. The operating parameters and/or performance indicators to be monitored preferably include at least drive wheel speed and direction, drive means speed, drive means temperature, and drive means clutch engagement. It is contemplated that the monitoring system could be expanded to include sensors for additional drive system parameters and/or performance indicators.

Monitoring System for Aircraft Drive Wheel System

An improved aircraft gate parking and servicing method is provided, wherein an aircraft is maneuvered into an airport terminal gate and parked in an optimum orientation at an angle that facilitates maximum access to aircraft front and rear doors. Boarding bridges are designed to facilitate connection to doors located rear of an aircraft wing without extending over the aircraft wing to maximize efficiency of passenger transfer. Passenger transfer and servicing of the aircraft may occur concurrently before the aircraft is maneuvered out of its optimum orientation in the parking space and driven to a takeoff runway for departure. Required safety margins are maintained at all times during aircraft maneuvers into and out of the optimum parking orientation. Stairs may be provided to simultaneously access aircraft doors not connected to boarding bridges. In a preferred embodiment, aircraft are moved to an optimum parking location by engines-off electric taxi systems.

Aircraft gate parking and servicing method

An apparatus 102 for remotely controlling an aircraft 108 having a self-propelled nosewheel 106, on the ground, comprises parking brakes; an APU on said aircraft; control means for applying and releasing said parking brakes 118; control means for turning on and off said APU 116; transmitting means for transmitting information to said parking brakes and said APU; receiving means for receiving information at said parking brakes; and receiving means for receiving information at said APU The remote control may further comprise means for control the speed of the aircraft, the direction of motion of the aircraft, an emergency stop button and a fire suppression feature

Isaiah W. Cox

Papers

Permanent wireless communications system for an aircraft equipped with a wheel drive system

Optimizing ground movement in a wide-body aircraft equipped with non-engine drive means

Monitoring System for Aircraft Drive Wheel System

Aircraft gate parking and servicing method

Remote control of an aircraft parking brakes and/or APU