Invention Application
- Patent Title: APPARATUS AND METHOD FOR DIRECTING THRUST FROM TILTING CROSS-FLOW FAN WINGS ON AN AIRCRAFT
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Application No.: US15483602Application Date: 2017-04-10
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Publication No.: US20180044013A1Publication Date: 2018-02-15
- Inventor: Kirk L. Groninga , Daniel B. Robertson , Matthew E. Louis
- Applicant: Bell Helicopter Textron Inc.
- Applicant Address: US TX Fort Worth
- Assignee: Bell Helicopter Textron Inc.
- Current Assignee: Bell Helicopter Textron Inc.
- Current Assignee Address: US TX Fort Worth
- Main IPC: B64C29/00
- IPC: B64C29/00 ; B64C15/12 ; B64C3/32 ; B64D27/24 ; F04D17/04 ; F04D29/28

Abstract:
A variable thrust cross-flow fan system for an aircraft including a rotatable wing member having a first housing member; an actuator assembly operably coupled to the first housing member; and a variable thrust cross-flow fan assembly including a first and second driver plates having a plurality of blades rotatably mounted therebetween. The plurality of blades has a circular path of travel when rotating and includes a control assembly coupled to the plurality of blades to generate a variable thrust force. The control assembly includes a control cam that is substantially non-rotatable relative to the first and second driver plates and a hinge member that is fixedly connected to the control cam and to the first housing member at a hinge axis. Rotation of the first housing member by the actuator assembly imparts rotation of the control cam about the hinge axis, thereby changing the direction of the variable thrust force.
Public/Granted literature
- US10377480B2 Apparatus and method for directing thrust from tilting cross-flow fan wings on an aircraft Public/Granted day:2019-08-13
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