ANISOTROPICALLY FLEXIBLE VIBRATION ISOLATING COUPLING MECHANISM
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United States of America Patent
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Issued Date -
Jan 11, 2024
app pub date -
Sep 21, 2023
filing date -
Apr 22, 2020
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Abstract
A flexible coupling mechanism may be used to suspend a structural component, such as a propulsion pod, from a support member, such as a strut of a hydrofoil watercraft. The flexible coupling mechanism may include multiple vibration isolating mounts configured to extend through the support member to suspend the structural component. The vibration isolating mounts may include a plurality of elastomeric bushings configured to prevent direct contact between a component rigidly coupled to the support member and a component rigidly coupled to the structural component. The elastomeric bushings may include a tapered outer profile configured to provide a nonlinear force feedback profile in response to rotation of the support member relative to the structural component.
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