公开(公告)号：US20220185477A1

公开(公告)日：2022-06-16

申请号：US17644653

申请日：2021-12-16

申请人： Dash Systems, Inc.

发明人： Joel Ifill ,  Zach Taylor ,  Jason Litzinger ,  Phil Stahlhuth ,  Marc Berte

IPC分类号： B64D1/14 ,  B64C27/02 ,  B64C39/02 ,  G05D1/10

摘要： A payload delivery device configured to deliver an aircraft deployed payload along a flight path to a predetermined landing destination includes a support member configured to be removably attached to the payload, a flight control and navigation system module configured to control orientation of the plurality of control surfaces while the payload is travelling along the flight path to the predetermined landing destination, a control surface assembly module including a plurality of control surfaces, a rotor assembly including a plurality of rotor blades having a central axis of rotation, and a collective control assembly module including at least one collective servomotor configured to control a plurality of control linkages connected to the plurality of rotor blades.

公开(公告)号：US20220185478A1

公开(公告)日：2022-06-16

申请号：US17644657

申请日：2021-12-16

申请人： Dash Systems, Inc.

发明人： Joel Ifill ,  Zach Taylor ,  Jason Litzinger ,  Phil Stahlhuth ,  Marc Berte

IPC分类号： B64D1/14 ,  B64C39/02 ,  B64C27/02 ,  B64F5/10

摘要： A method of assembling a delivery payload assembly configured to be deployed from an aircraft and travel along a flight path to a predetermined landing destination includes attaching a tail-kit assembly to a first end of a payload, the tail-kit assembly including a rotor blade assembly including a plurality of rotor blades having a central axis of rotation, and a flight control and navigation system configured to control a collective pitch angle of each of the plurality of rotor blades of the rotor blade assembly, configured to control an axial thrust force of the rotor blade assembly, the axial thrust force being at an angle with respect to the central axis of rotation of the rotor blade assembly, and configured to navigate the delivery payload assembly along the flight path to the predetermined landing destination. The method further includes removing the tail-kit assembly from the payload after the payload is delivered to the predetermined landing destination.