The invention relates to a device (9) for taking up thrust forces for an aircraft engine pylon, which includes safety means, associated with each of the two lateral link rods (90) for taking up forces and equipped with first end-stop means (108) fitted to the link rod, as well as second end-stop means (112) fitted to the spreader bar (91), where these end-stop means, once they have come into contact as a result of relative rotation between the spreader bar and the link rod around the axis (93) of a link rod pivot mechanism (92) and in a given direction of rotation, are used to stop the said relative rotation in the given direction of rotation.
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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