AIRCRAFT WITH TAILPROOFER MOUNTS

MX439092BActive Publication Date: 2026-10-05WISK AERO LLC
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Patent Information

Application Number
MX2026003354
Authority / Receiving Office
MX · MX
Patent Type
Patents
Current Assignee / Owner
Priority Date
2020-01-31
Filing Date
2022-07-28
Publication Date
2026-10-05
Estimated Expiration
2041-01-29

AI Technical Summary

Technical Problem

Current aircraft with vertical takeoff and landing capabilities require separate systems for vertical lift and horizontal thrust, lacking a seamless transition between vertical and horizontal flight modes, which complicates control and efficiency.

Method used

The design incorporates tilting fan assemblies that can switch between a vertical lift position and a forward flight position, enabled by a control system that adjusts the fan assemblies' orientation in response to flight instructions, allowing for both vertical takeoff and landing as well as horizontal cruising.

Benefits of technology

This solution enables a balanced control of vertical and horizontal thrust, facilitating smooth transitions between flight modes, enhancing the aircraft's operational efficiency and versatility.

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Abstract

The models provide an aircraft with one or more tilting propeller assemblies that are configured to tilt between a forward flight position and a vertical lift position. The aircraft may also include a plurality of lift propeller assemblies for vertical movement. The tilting propeller assemblies may be attached to the fuselage or wings of the aircraft by one or more tilting mechanisms. A control system attached to the aircraft may control the one or more tilting mechanisms to move the tilting propeller assemblies between the forward flight position and the vertical lift position. The tilting propeller assemblies may be attached to one or more support structures that are attached to the fuselage or wings of the aircraft.
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