Gimbal having parallel stability mechanism
First Claim
1. A gimbal mechanism for providing movement of a payload about at least two degrees of freedom, the gimbal mechanism comprising:
- a first actuator providing rotation about a first actuator axis;
a second actuator providing rotation about a second actuator axis different from the first actuator axis;
a first coupler operatively coupling the first actuator and the payload, the first coupler being configured to affect rotation of the payload about the first actuator axis; and
a second coupler operatively coupling the second actuator and the payload, the second coupler being configured to affect rotation of the payload about the second actuator axis and comprising;
a joint member configured to be coupled to the payload; and
a cantilever member coupled to the second actuator and configured to translate a torque generated by the second actuator to the payload via the joint member, the cantilever member comprising a first cantilever component and a second cantilever component movably coupled to each other via a hinge, and the hinge being configured to provide free rotation of the second cantilever component about a hinge axis;
wherein the first actuator and the second actuator are fixed in position and orientation relative to one another and relative to a support structure, the support structure being configured to support at least one of the first actuator or the second actuator.
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Accused Products
Abstract
A gimbal mechanism includes a first actuator providing rotation about a first actuator axis, a second actuator providing rotation about a second actuator axis different from the first actuator axis, a first coupler operatively coupling the first actuator and a payload and being configured to affect rotation of the payload about the first actuator axis, and a second coupler operatively coupling the second actuator and the payload and being configured to affect rotation of the payload about the second actuator axis. The first actuator and the second actuator are fixed in position and orientation relative to one another and relative to a support structure. The support structure is configured to support at least one of the first actuator or the second actuator.
19 Citations
19 Claims
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1. A gimbal mechanism for providing movement of a payload about at least two degrees of freedom, the gimbal mechanism comprising:
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a first actuator providing rotation about a first actuator axis; a second actuator providing rotation about a second actuator axis different from the first actuator axis; a first coupler operatively coupling the first actuator and the payload, the first coupler being configured to affect rotation of the payload about the first actuator axis; and a second coupler operatively coupling the second actuator and the payload, the second coupler being configured to affect rotation of the payload about the second actuator axis and comprising; a joint member configured to be coupled to the payload; and a cantilever member coupled to the second actuator and configured to translate a torque generated by the second actuator to the payload via the joint member, the cantilever member comprising a first cantilever component and a second cantilever component movably coupled to each other via a hinge, and the hinge being configured to provide free rotation of the second cantilever component about a hinge axis; wherein the first actuator and the second actuator are fixed in position and orientation relative to one another and relative to a support structure, the support structure being configured to support at least one of the first actuator or the second actuator. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19)
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Specification