Invention Grant
- Patent Title: Adjustable aft pivot assembly release component
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Application No.: US17732817Application Date: 2022-04-29
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Publication No.: US11878801B2Publication Date: 2024-01-23
- Inventor: Benjamin Hetrick , Matthew Bangerter , Christopher K. Solecki , Zachary Scott Zutavern , Scott E. Herrmann
- Applicant: Raytheon Company
- Applicant Address: US MA Waltham
- Assignee: Raytheon Company
- Current Assignee: Raytheon Company
- Current Assignee Address: US MA Tewksbury
- Agency: Renner, Otto, Boisselle & Sklar LLP
- Main IPC: B64D1/02
- IPC: B64D1/02 ; B64D37/12

Abstract:
An aft pivot assembly includes a height adjustment mechanism integrated into a device for mounting a payload, to enable release of the payload. The aft pivot assembly releasably secures an aft portion of the payload, such a pod, store, ordinance, or fuel tank. The aft pivot assembly includes a shaft operable with the mount device and a release component, the shaft being rotatable about multiple shaft axes relative to the mount device so as to either minimize or eliminate carriage loads about the aft portion, while reacting jettison loads during a jettison event or phase. The rotation of the shaft about its shaft axes can further be limited via a limit device. As the payload transitions from a carriage phase to a jettison phase, the shaft moves in multiple degrees of freedom and in multiple axes relative to the mount device.
Public/Granted literature
- US20230025482A1 ADJUSTABLE AFT PIVOT ASSEMBLY RELEASE COMPONENT Public/Granted day:2023-01-26
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