A surface-mounted fuselage skin applique panel having an aperture to a reference static air input port is rugged, replaceable, and independently calibratable. The static port skin applique generally conforms to the fuselage surface, and is held in place either with adhesive or with a mounting frame. The applique size enables airflow in the vicinity of the static port to be substantially uniform. Because the applique is not part of the fuselage structure, distorting stress loads are avoided. The applique material resists scratches and bumps that can distort flow. A static port skin applique and its mounting provisions can be made using a range of materials, and can receive finishes to meet user preferences.
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.
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