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公开(公告)号：US20250153856A1
公开(公告)日：2025-05-15
申请号：US18507774
申请日：2023-11-13
Applicant: Bell Textron Inc.
Inventor： Austin Thomas MCINTIRE , Brian Joseph Roppolo , Eric Stephen Olson
Abstract: A rotorcraft propulsion system includes a mast coupled to a rotor assembly, a gear coupled to the mast, the gear during use producing an axial reaction force, a flexure shaft extending from the gear, where the flexure shaft does not rotate with the gear and the flexure shaft flexes in response to radial loads from the gear, and a load cell on the flexure shaft to measure the axial reaction force.
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