Hinges and other mechanisms that relate to the movement of objects back and forth relative to one another are often manually actuated, e.g. doors, windows, lids, etc. However, in some industries, there is significant utility to providing automation. Thus, many technologies exist that utilize actuators to drive hinges and other mechanisms, e.g., rotational, telescoping, etc. Examples include hinges to drive doors, lids, covers, etc. Many actuator driven hinges or similar devices use electrical or other types of motors to provide back and forth actuation, for example. However, these types of actuated hinges can have several drawbacks, particularly when used in certain industries, such as aerospace, nuclear, chemical, etc. For example, motors can have some issues related to lack of covertness, contamination control, thermal control, solar protection, inconvenient failures, etc. As such, it would be desirable to provide an actuator that is highly reliable even in harsh environments and can provide for at least bi-directional movement of articles relative to one another.
In accordance with the present disclosure, a multi-spring-loaded actuator can include a rotatable axis arranged to rotate relative to a fixed frame, a first loaded spring having a first rotational potential attached to the rotatable axis to cause the rotatable axis to rotate in a first direction when the first rotational potential of the first loaded spring is released, and a first one-time release mechanism coupled to the first loaded spring to retain the first loaded spring at the first potential until the first one-time release mechanism is spent causing the first loaded spring to release. In further detail, the multi-spring-loaded actuator can include a second loaded spring having a second rotational potential attached to the rotatable axis to cause the rotatable axis to rotate in a second direction opposite the first direction when a second rotational potential of the second loaded spring is released subsequent to release of the first loaded spring, and a second one-time release mechanism coupled to the second loaded spring to retain the second loaded spring at the second rotational potential until the second one-time release mechanism is spent causing the second loaded spring to release and rotate the rotatable axis in the second direction opposite the first direction.
Regarding certain additional example details of the multi-spring-loaded actuator, the actuator can include, for example, a third loaded spring having a third rotational potential attached to the rotatable axis to cause the rotatable axis to rotate in the first direction when a third rotational potential of the third loaded spring is released subsequent to release of the first loaded spring and the second loaded spring, and a third one-time release mechanism coupled to the third loaded spring to retain the third loaded spring at the third rotational potential until the third one-time release mechanism is spent causing the third loaded spring to release and rotate the rotatable axis in the first direction. In further detail, the multi-spring-loaded actuator may include a fourth loaded spring having a fourth rotational potential attached to the rotatable axis to cause the rotatable axis to rotate in the second direction when a fourth rotational potential of the fourth loaded spring is released subsequent to release of the first loaded spring, the second loaded spring, and the third loaded spring, and a fourth one-time release mechanism coupled to the fourth loaded spring to retain the fourth loaded spring at the fourth rotational potential until the fourth one-time release mechanism is spent causing the fourth loaded spring to release and rotate the rotatable axis in the second direction. In some examples, the fixed frame can be attached to a first article, and the rotatable axis is attached to a second article, wherein rotation of the rotatable axis in the first direction causes a first motion of the second article relative to the first article and rotation of the rotatable axis in the second direction causes a second motion of the second article relative to the first article. The first article, for example, can be a housing and the second article can be a cover for the housing. Upon the first motion and the second motion of the cover, the cover opens then closes or the cover closes then opens relative to the housing. In other examples, the second article may include a solar panel, a calibration source, etc. The first one-time-release mechanism, the second one-time-release mechanism, or both, can include, for example, one or more of a frangible, an explosive, or an electromagnet. In some examples, the multi-spring-loaded actuator can be in the form of a bi-directional hinge actuator, a bi-directional telescoping actuator, or a bi-directional rotational actuator.
In another example, a multi-spring-loaded actuator system can include a first article attached to a fixed frame that supports a rotatable axis that rotates relative to the fixed frame, and a second article operationally associated for movement relative to the first article. The multi-spring-loaded actuator system can further include a first loaded spring having a first rotational potential attached to the rotatable axis to cause the rotatable axis to rotate in a first direction when the first rotational potential of the first loaded spring is released, and an off-actuator one-time release mechanism coupled to the second article to retain the first loaded spring at the first potential until the off-actuator one-time release mechanism is spent causing the first loaded spring to release. Furthermore, the multi-spring-actuator system can include a second loaded spring having a second rotational potential attached to the rotatable axis to cause the rotatable axis to rotate in a second direction opposite the first direction when a second rotational potential of the second loaded spring is released subsequent to release of the first loaded spring, and a second one-time release mechanism coupled to the second loaded spring to retain the second loaded spring at the second rotational potential until the second one-time release mechanism is spent causing the second loaded spring to release and rotate the rotatable axis in the second direction opposite the first direction.
Regarding additional details related to the multi-spring-loaded actuator system, the system may include a third loaded spring having a third rotational potential attached to the rotatable axis to cause the rotatable axis to rotate in the first direction when a third rotational potential of the third loaded spring is released subsequent to release of the first loaded spring and the second loaded spring, and a third one-time release mechanism coupled to the third loaded spring to retain the third loaded spring at the third rotational potential until the third one-time release mechanism is spent causing the third loaded spring to release and rotate the rotatable axis in the first direction. In a more detailed example, the multi-spring-loaded actuator system can further include a fourth loaded spring having a fourth rotational potential attached to the rotatable axis to cause the rotatable axis to rotate in the second direction when a fourth rotational potential of the fourth loaded spring is released subsequent to release of the first loaded spring, the second loaded spring, and the third loaded spring, and a fourth one-time release mechanism coupled to the fourth loaded spring to retain the fourth loaded spring at the fourth rotational potential until the fourth one-time release mechanism is spent causing the fourth loaded spring to release and rotate the rotatable axis in the second direction. In some examples, the fixed frame can be attached to a first article, and the rotatable axis can be attached to a second article. Rotation of the rotatable axis in the first direction causes a first motion of the second article relative to the first article and rotation of the rotatable axis in the second direction causes a second motion of the second article relative to the first article. In additional examples, the first article can be a housing and the second article can be a cover for the housing. In this example, upon the first motion and the second motion of the cover, the cover opens then closes or the cover closes then opens relative to the housing.
In another example, a method of bi-directionally moving a second article relative to a first article can include discharging a first one-time-release mechanism to cause a first loaded spring attached to a rotatable axis to unload and rotate the rotatable axis in a first direction, and discharging a second one-time-release mechanism after discharging the first one-time-release mechanism to cause a second loaded spring attached to a rotatable axis to unload and rotate the rotatable axis in a second direction opposite the first direction. In this example, rotation in the first direction causes a first motion of a second article relative to a first article, and rotation in the second direction causes a second motion of the second article relative to a first article.
In additional detail regarding the methods herein, the first one-time release mechanism, for example, can be located on the second article, and the rotatable axis, the first loaded spring, the second one-time release mechanism, and the second loaded spring can be part of a multi-spring-loaded actuator located on the first article. In other examples, the rotatable axis, the first one-time release mechanism, the first loaded spring, the second one-time release mechanism, and the second loaded spring can be part of a multi-spring-loaded actuator located on the first article. In other examples, discharging the first one-time-release mechanism, the second one-time-release mechanism, or both includes discharging one or more of a frangible, an explosive, or an electromagnet. Furthermore, the multi-spring-loaded actuator can in some instances be in the form of a bi-directional hinge actuator, a bi-directional telescoping actuator, or a bi-directional rotational actuator.
As a note, with respect to the multi-spring-loaded actuators, the multi-spring-loaded actuator systems, and the methods of bi-directionally moving a second article relative to a first article, specific descriptions with respect to one example can be considered applicable to other examples whether or not they are explicitly discussed in the context of that example. Thus, for instance, in discussing a first loaded spring related to the multi-spring-loaded actuators, such disclosure is also relevant to and directly supported in context of the systems and methods also described herein, and vice versa.
The terms used herein will have their ordinary meaning in the relevant technical field unless specified otherwise. Some terms are specifically defined herein that pertain to the present disclosure and appended claims and should be understood herein as specifically defined, taken in context with the plain meaning of those defined terms.
The term “multi-spring-loaded actuator” refers to actuators, as exemplified herein, that include at least two loaded springs that are pre-set to actuate articles in different directions, respectively, when the actuator is installed on one or both of the articles. The multiple loaded springs are configured to be sequentially unloaded through the sequential decoupling or firing of multiple one-time release mechanisms. In operation, the multi-spring-loaded actuator can be configured to move a first article relative to a second article, move a second article relative to a first article, or move a first article and a second article relative to one another. Example structures of multi-spring-loaded actuator configurations can include a hinge assembly for opening and shutting a second article relative to a first article (e.g., opening and shutting a lid relative to the housing or a door relative to a frame), a rotational assembly for rotating a second article such as a rotational stage relative to a first article about an axis (e.g., bi-directional rotation of a calibration source), a telescoping assembly (e.g., bi-directional in and out movement of a mechanism, such as a shutter, within a telescope housing), or the like.
The term “multi-spring-loaded actuator system” refers to assemblies including a multi-spring-loaded actuator, but the actuator is assembled as part of a system, e.g., attached to a first article and a second article that are actuated relative to one another. In some examples, the multiple loaded springs can be released sequentially by one-time release mechanisms present on the multi-spring-loaded actuator, or alternatively, one or more of the one-time release mechanisms may be present “off-actuator,” (e.g., present on a hinged article, an article of a rotational stage, a telescoping article, etc.). The off-actuator one-time release mechanism may still be mechanically associated with one or more of the loaded springs so that when the off-actuator one-time release mechanism is fired (e.g., explosive or frangible mechanism) or decoupled (e.g., electromagnetic release mechanism), the loaded springs are unloaded causing the multi-spring-loaded actuator to rotationally turn and then turn back in the opposite direction, respectively.
The term “one-time release mechanism” refers to any structure that can be fired, decoupled, or spent to unload a pre-loaded spring positioned about and mechanically connected to a rotational axis to cause the rotational axis to rotate in a direction, e.g., a first direction or a second (typically opposite) direction. Examples include frangible devices, e.g., frangible bolts; explosive release compositions or devices, e.g. explosive adhesive, blasting caps, etc.; or electromagnets. Electromagnetics are not typically known as having a “one-time release mechanism,” but in the context of the actuators and systems described herein, the spring loaded movement after decoupling would position the electromagnetic too far away for the structure to be reversed from its unloaded spring configuration back to its loaded spring configuration. So, in that sense, electromagnetic when used as described herein is considered to be a one-time release mechanism.
Referring now to
As shown, the one-time release mechanisms 12 and 22, which in this instance are frangibles (sometimes referred to as a frangible nut, a frangible bolt, etc., depending on the arrangement), which are devices used in many industries, including the aerospace industry, to sever mechanical connections. For example, a frangible is commonly described as an explosively-splittable component that can separate upon introduction of an electrical signal. In some instances, one portion may remain intact with one of the structures while the other portion is separate therefrom. One example may include a bolt with a frangible nut that is broken off in one or more parts. Regardless of the structure or arrangement, the frangibles suitable for use can include at least two portions which become separated when electrically energized. For example, when a frangible nut or other structure is separated from a frangible bolt, the bolt may sometimes remain with one of the first article or the second article. The nut itself can be split into two or more parts and can be shed, or can remain with the other of the first article or the second article. Other types of frangibles can likewise be used. Though a frangible is shown in
In additional examples, the first article and/or second article can be a structure other than a housing and a lid, respectively. For example, the first article can include a frame, a support structure, a capsule, etc. The second article can be, for example, a solar panel, a calibration source, etc. To illustrate, the first and second articles can be arranged as part of a multi-spring-loaded actuator system that includes a bi-directional hinge actuator, a bi-directional telescoping actuator, or a bi-directional rotational actuator. In instances where there is an off-actuator one-time release mechanism, that particular one-time release mechanism is not part of the bi-directional hinge actuator, the bi-directional telescoping actuator, or the bi-directional rotational actuator, but rather is an “off-actuator,” working together with the multi-spring loaded actuator to release the first loaded spring. Notably, in other examples, all of the loaded springs may be associated with one-time release mechanisms that are included onboard the multi-spring-loaded actuator.
A detailed front view of an example multi-spring-loaded actuator 100 that can be used in a multi-spring-loaded actuator system is shown in
Regarding the structures shown in
Releasing the potential of the four loaded springs 10, 20, 30, and 40 can occur respectively by sequentially firing or decoupling a corresponding first one-time release mechanism (not shown, as this mechanism is an “off-actuator”), followed by a second one-time release mechanism 22, followed by a third one-time release mechanism 32, and then followed by a fourth one-time release mechanism 42. As shown in
The multi-spring-loaded actuator shown in
Referring now to
Starting with
In operation, the initial configuration of the multi-spring-loaded actuator 100 is shown at
Referring now to
Referring now to
Referring now to
Referring now to
In additional detail regarding the methods herein, the first one-time release mechanism, for example, can be located on the second article, and the rotatable axis, the first loaded spring, the second one-time release mechanism, and the second loaded spring can be part of a multi-spring-loaded actuator located on the first article. In other examples, the rotatable axis, the first one-time release mechanism, the first loaded spring, the second one-time release mechanism, and the second loaded spring can be part of a multi-spring-loaded actuator located on the first article. In other examples, discharging the first one-time-release mechanism, the second one-time-release mechanism, or both, includes discharging one or more of a frangible, an explosive, or an electromagnet. Furthermore, the multi-spring-loaded actuator can in some instances be in the form of a bi-directional hinge actuator, a bi-directional telescoping actuator, or a bi-directional rotational actuator.
In accordance with the present disclosure, it is noted that no specific order is required in the methods disclosed herein, though generally in some examples, method steps can be carried out sequentially. It is also understood that the examples set forth herein are not limited to the particular structures, process steps, or materials disclosed, but are extended to equivalents thereof as would be recognized by those ordinarily skilled in the relevant arts. It should also be understood that terminology employed herein is used for the purpose of describing particular examples only and is not intended to be limiting. Furthermore, the described features, structures, or characteristics may be combined in any suitable manner in one or more examples. In the description, numerous specific details are provided, such as examples of lengths, widths, shapes, etc., to provide a thorough understanding of the technology being described. One skilled in the relevant art will recognize, however, that the disclosure can be practiced without one or more of the specific details, or with other methods, components, materials, etc. In other instances, well-known structures, materials, or operations are not shown or described in detail to avoid obscuring aspects of the disclosure.
While the foregoing examples are illustrative of the principles of the disclosure in one or more particular applications, it will be apparent to those of ordinary skill in the art that numerous modifications in form, usage and details of implementation can be made without the exercise of inventive faculty, and without departing from the principles and concepts described herein. Accordingly, it is not intended that the disclosure be limited, except as by the claims set forth below.
This disclosure was made with Government support. The Government has certain rights to the disclosure.