Invention Publication
- Patent Title: Tow Line Tension Management Systems for Aircraft
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Application No.: US17885053Application Date: 2022-08-10
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Publication No.: US20240051661A1Publication Date: 2024-02-15
- Inventor: Russell C. Peters , John Robert Wittmaak, JR. , Alyssa Berta Armendariz , Christopher John Stroncek
- Applicant: Textron Innovations Inc.
- Applicant Address: US RI Providence
- Assignee: Textron Innovations Inc.
- Current Assignee: Textron Innovations Inc.
- Current Assignee Address: US RI Providence
- Main IPC: B64C29/00
- IPC: B64C29/00 ; B64D3/00

Abstract:
A tailsitter aircraft for deploying a tow line includes an airframe having wings with pylons extending therebetween and a thrust array attached to the airframe, the thrust array including propulsion assemblies configured to transition the airframe between a forward flight orientation and a VTOL orientation. The tailsitter aircraft includes an attenuation spool coupled to the airframe and an attenuation cable having a first end coupled to the attenuation spool and a second end coupled to the tow line, the attenuation cable partially or fully wound around the attenuation spool. The tailsitter aircraft also includes a spool sensor to detect movement of the attenuation spool and a flight control system implementing a tow line tension monitoring module in communication with the spool sensor to determine a tow line tension parameter and a tow line tension reaction module to initiate an aircraft response based on the tow line tension parameter.
Public/Granted literature
- US11987351B2 Tow line tension management systems for aircraft Public/Granted day:2024-05-21
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