A mounting system (10) for attaching a structural monument in a desired position in an aircraft cabin comprises a support element (12) that is connectable to a base body (14) of the structural monument in a pedestal area of the structural monument. The mounting system (10) further comprises a receiving device (50) that is attachable in an area of a floor of the aircraft cabin, and a first coupling element (38) attached to the support element (12), designed for connecting the supporting element (12) to the receiving device (50) that is attachable in an area of a floor of the aircraft cabin. Finally, the mounting system (10) comprises a retaining element (76) that is connectable to the base body (14) of the structural monument in a ceiling area of the structural monument, and a second coupling element (86) attached to the retaining element (76), designed for connecting the retaining element (76) to a structurally solid component of the aircraft.
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 >