Patent 10364827 was granted and assigned to MTU Aero Engines on July, 2019 by the United States Patent and Trademark Office.
An adjustable guide vane ring of a turbomachine having an inner ring, the guide vanes of which each have a radially inner vane disk with disk thickness increasing in the direction of flow and acting as a bearing pin; a guide vane, as well as an inner ring for such a guide vane ring, as well as a turbomachine are disclosed.