An input system (2) for a landing flap control of an aircraft. In order to make the input system (2) compact, light and reliable, it is provided with a selector lever (4) mounted pivotably by a shaft unit (10) for the input of a landing flap position, and a sensor arrangement (22) being arranged at one side of the selector lever (4) and having two mutually redundant optoelectronic sensor units (24) each for detecting a position of the selector lever (4), wherein a one-piece shaft element (40) of the shaft unit (10) is passed from the selector lever (4) through the sensor units (24).
This information is part of a study by Oasis Global, Inc. of all space inventions filed at the United States Patent and Trademark Office, and is provided for informational purposes only. It is not an endorsement of any particular assignee, inventor or invention. Although Peter A. Koziol represents inventors and assignees of space inventions he does not represent all of the inventors and assignees listed. The prosecuting attorney agent or firm for each patent is identified by the United States Patent and Trademark Office in the patent specfication, which can be viewed by clicking on the patent image or downloading the patent document. For more information regarding Mr. Koziol's background and experience, or to learn more about space inventions, please contact Mr. Koziol.
Enter your name and phone number, and Peter will call you back as soon as possible.
Disclaimer: The hiring of a lawyer is an important decision that should not be based solely upon advertisements. Before you decide, ask us to send you free written information about our qualifications and experience. Read More >
