The present invention relates to force control mechanisms, and in an embodiment, but not by way of limitation, a mechanism to control a linearly decreasing force.
In the testing of certain devices and apparatuses, the test requires the application or provision of a linearly increasing force. In many of these circumstances, a simple compression coil spring or a spring-loaded test device can be used to provide such a linearly increasing force. However, in other situations, such as in the testing of pyro cartridges or the matching of an aerodynamic loading condition, testing requires a linearly decreasing force. Such a linearly decreasing force cannot be provided by a simple spring. The art is therefore in need of a test apparatus that can supply a linearly decreasing force.
In the following detailed description, reference is made to the accompanying drawings that show, by way of illustration, specific embodiments in which the invention may be practiced. These embodiments are described in sufficient detail to enable those skilled in the art to practice the invention. It is to be understood that the various embodiments of the invention, although different, are not necessarily mutually exclusive. For example, a particular feature, structure, or characteristic described herein in connection with one embodiment may be implemented within other embodiments without departing from the scope of the invention. In addition, it is to be understood that the location or arrangement of individual elements within each disclosed embodiment may be modified without departing from the scope of the invention. The following detailed description is, therefore, not to be taken in a limiting sense, and the scope of the present invention is defined only by the appended claims, appropriately interpreted, along with the full range of equivalents to which the claims are entitled. In the drawings, like numerals refer to the same or similar functionality throughout the several views.
The swing links 105a-d, spring seat links 125a,b, fixed link 115, and input/output link 110, when a force F1 is applied to the input/output link 110 of the apparatus 100 via the load bearing assembly 140, as illustrated in
In the foregoing detailed description of embodiments of the invention, various features are grouped together in one or more embodiments for the purpose of streamlining the disclosure. This method of disclosure is not to be interpreted as reflecting an intention that the claimed embodiments of the invention require more features than are expressly recited in each claim. Rather, as the following claims reflect, inventive subject matter lies in less than all features of a single disclosed embodiment. Thus the following claims are hereby incorporated into the detailed description of embodiments of the invention, with each claim standing on its own as a separate embodiment. It is understood that the above description is intended to be illustrative, and not restrictive. It is intended to cover all alternatives, modifications and equivalents as may be included within the scope of the invention as defined in the appended claims. Many other embodiments will be apparent to those of skill in the art upon reviewing the above description. The scope of the invention should, therefore, be determined with reference to the appended claims, along with the full scope of equivalents to which such claims are entitled. In the appended claims, the terms “including” and “in which” are used as the plain-English equivalents of the respective terms “comprising” and “wherein,” respectively. Moreover, the terms “first,” “second,” and “third,” etc., are used merely as labels, and are not intended to impose numerical requirements on their objects.
The abstract is provided to comply with 37 C.F.R. 1.72(b) to allow a reader to quickly ascertain the nature and gist of the technical disclosure. The Abstract is submitted with the understanding that it will not be used to interpret or limit the scope or meaning of the claims.
This invention was made with United States Government support under contract number F34601-02-C-0090 with the Department of the Air Force. The United States government has certain rights in this invention.
Number | Name | Date | Kind |
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3263511 | Wellstein | Aug 1966 | A |
4265141 | Bowman | May 1981 | A |
5433656 | Cloutier et al. | Jul 1995 | A |
7143850 | Takenaka et al. | Dec 2006 | B2 |
7540799 | Trojan | Jun 2009 | B1 |
Number | Date | Country | |
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20100083734 A1 | Apr 2010 | US |