The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jun. 17, 2025

Filed:

Sep. 21, 2023
Applicant:

Kai Concepts, Llc, Alameda, CA (US);

Inventors:

Donald Lewis Montague, Paia, HI (US);

Joseph Andrew Brock, Alameda, CA (US);

Tomasz Pawel Bartczak, Toronto, CA;

Matthew Campbell Greaves, Corinda, AU;

Alec Korver, Monument, CO (US);

Jamieson Edward Schulte, Alameda, CA (US);

Dmitri Stepanov, San Francisco, CA (US);

Assignee:

Kai Concepts, LLC, Alameda, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B63B 1/24 (2020.01); B60L 50/50 (2019.01); B63B 32/10 (2020.01); B63H 1/14 (2006.01); B63H 5/125 (2006.01); B63H 21/17 (2006.01);
U.S. Cl.
CPC ...
B63B 1/242 (2013.01); B60L 50/50 (2019.02); B63B 1/246 (2013.01); B63B 1/248 (2013.01); B63B 32/10 (2020.02); B63H 1/14 (2013.01); B63H 5/125 (2013.01); B63H 21/17 (2013.01); B60L 2200/32 (2013.01); B63H 2005/1254 (2013.01);
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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