Patent 12065947 was granted and assigned to General Electric on August, 2024 by the United States Patent and Trademark Office.
Methods, apparatus, systems and articles of manufacture are disclosed. An inner shroud damper for a gas turbine engine includes: at least one carrier including a joint to couple to an inner shroud, the at least one carrier having a first side and a second side, and at least one mass damper coupled to the at least one carrier.