Other

Fci Americas Technology Inc.

Go, Inc.

Surfdash

Robert Jonathan Carr

James Michael Higgins

S Jerrold Kaplan

Jennifer Kelly

David R Low

Michael Ouye

Raymond Kelly

Todd Agulnick

Seyed Safakish

Tony Hoeber

A method and system for providing a secure network. The system can have a URL programming interface, a server, and a database connected to the server. The server can be configured to receive requests from the URL programming interface. The server can include a file manager, an authentication server, a resource server, and a collaboration server.

System and method for providing a secure network

Aircraft design

A die storing and organizing system includes a holder for storing and organizing crimp dies, the holder having a first side and a second, opposite side. The system further includes a plurality of apertures in the holder, each aperture extending from the first side to the second, opposite side; wherein each aperture is adapted to receive a die pin.

Die storing and organizing system

An aircraft designed with three wings located on either side of the fuselage. The forward wing has a downward angle with a curved top and bottom surface. The upper wing is located towards the rear of the aircraft and above the forward wing. The lower wing is located below the upper wing and slightly forward. It is also located to the rear and below of the forward wing. The outer ends of all three wings come into contact at one point. The forward wing uses the Coanda effect to increase the airflow across the top surface of the bottom wing. The aircraft can be designed so that it is large enough to carry people and/or cargo, or to be small enough to be flown as a toy aircraft. The like design can use any type of aircraft engine commonly used today. One embodiment of the aircraft has two turbines, shaft-coupled to a power source, located on either side of the forward end of the fuselage. Each engine has part of its thrust diverted through and directed by a plenum disposed internal of the coanda toward both sides of the fuselage so that an equal amount of thrust flows through the duct and over the wings on either side of the fuselage. This ensures equal lift on the coanda and both wings on either side of the fuselage in the event that one engine malfunctions.

Aircraft internal wing and design

The present invention provides an improved lift system for an aerial crane incorporating a wing, coanda and curved surface. The arrangement of the wing, coanda and curved surface use and induce airflow to create additional lift through an increase in airflow mass, density and velocity. A different configuration of the wing, coanda and curved surface can be used to propel a vehicle.

Lift system for an aerial crane and propulsion system for a vehicle

A notebook computer which is controlled by a stylus executing gestures on the computer screen. The stylus and the computer include complementary electronic circuitry by which the proximity of the stylus tip to the computer is sensed. The proximity sensing is used to detect to approach of the stylus tip to the computer screen, and gestural commands are then entered on the screen by moving the stylus. The entry of a command is terminated by removing the stylus tip from proximity with the screen, which is detected by the computer, which then implements the command. Alternative methods of implementing the commands include time-outs and command termination buttons.

Control of a computer through a position-sensed stylus

An aircraft having a fuselage provided with an internal duct extending longitudinally therethrough to provide an internal wing for the craft, the internal duct having the forward end open for receiving an air stream therethrough and the aft end thereof open for discharge of the air stream therefrom, the internal contour of the duct being alterable in accordance with required operational conditions for the flight of the craft, and a plurality of control flaps and/or vanes provided at the aft end of the duct for proving operational controls for the craft in the manner of a more conventional external wing craft.

Internal wing aircraft

Lift for an aircraft is provided by forming a longitudinal lifting duct therethrough, said lifting duct having a substantially planar roof and a longitudinally cambered floor. When the aircraft is driven forwardly, a stream of air enters and passes through the lifting duct and the contouring of the floor of the lifting duct give rise to a pressure gradient in the air stream which result in a higher pressure on the roof of the lifting duct than on the floor thereof so that the pressure difference provides lift for the aircraft.

Growing community of inventors

Yukon, OK, United States of America

Robert Jonathan Carr