Rapid product design of improved ballistic articles
11194311 · 2021-12-07
Assignee
Inventors
Cpc classification
F41H5/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B2571/02
PERFORMING OPERATIONS; TRANSPORTING
G01N9/00
PHYSICS
B32B5/26
PERFORMING OPERATIONS; TRANSPORTING
F41H5/0485
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B9/007
PERFORMING OPERATIONS; TRANSPORTING
B32B2260/04
PERFORMING OPERATIONS; TRANSPORTING
B32B2255/02
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/10
PERFORMING OPERATIONS; TRANSPORTING
F41J13/00
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B3/06
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/54
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/762
PERFORMING OPERATIONS; TRANSPORTING
G01N3/00
PHYSICS
G05B19/4099
PHYSICS
Y02P90/02
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B32B2250/42
PERFORMING OPERATIONS; TRANSPORTING
F41J11/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B32B2260/021
PERFORMING OPERATIONS; TRANSPORTING
B32B2307/546
PERFORMING OPERATIONS; TRANSPORTING
International classification
F41H5/02
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
G01N9/00
PHYSICS
G05B19/4099
PHYSICS
Abstract
A method for the design and development of new ballistic resistant articles is provided. Improved ballistic articles are formed of polyethylene-based composite laminated structures having unique material properties including material density, Poisson's ratio, and modulus of elasticity (Young's modulus). Cycle time for completing design and development is less than 30 calendar days.
Claims
1. A method for a rapid design of improved ballistic articles comprising, in combination: identifying new armor products or existing armor products to be improved upon; creating a 3D engineering model utilizing ballistics failure analyses with a CAE (Computer Aided Engineering) program utilizing an anti-ballistic material comprising: interlineated layers of modified polyethylene materials; and layers of carbon nanotubes between adjacent modified polyethylene materials layers, wherein each said interlineated layer of modified polyethylene material is formed having a molecularly oriented layer of material; iteratively testing said 3D engineering model until a suggested design is achieved to meet a selected specification; creating a physical prototype of said suggested design; and destructively testing said physical prototype to confirm if the selected specification is achieved; wherein the CAE (Computer Aided Engineering) program is utilized with the 3D engineering model imported into a stand-alone simulation application for said iterative testing of the 3D engineering model to modify material properties selected from a group comprising: material density; Poisson's ratio; and modulus of elasticity (Young's modulus).
2. A method for the rapid design of improved ballistic articles comprising, in combination: identifying new armor products or existing armor products to be improved upon; creating a 3D engineering model utilizing ballistics failure analyses with a CAE (Computer Aided Engineering) program utilizing an anti-ballistic material comprising: interlineated layers of modified polyethylene materials; and layers of carbon nanotubes between adjacent modified polyethylene materials layers, wherein each said interlineated layer of modified polyethylene material is formed having a molecularly oriented layer of material; iteratively testing said 3D engineering model until a suggested design is achieved to meet a selected specification; creating a physical prototype of said suggested design; and destructively testing said physical prototype to confirm if are the selected specification is achieved; wherein a cycle time for completing said combination is less than 30 calendar days; wherein prior art specimens are utilized as a starting point for design development, dimensions and features emulated as closely as possible; and wherein the commercial CAE (Computer Aided Engineering) program is utilized with the 3D engineering model imported into a stand-alone simulation application for said iterative testing of the 3D engineering model to modify material properties selected from a group comprising: material density; Poisson's ratio; and modulus of elasticity (Young's modulus).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The advantages and features of the present invention will become better understood with reference to the following more detailed description and claims taken in conjunction with the accompanying drawings, in which like elements are identified with like symbols, and in which:
(2)
(3)
(4)
DESCRIPTION OF THE PREFERRED EMBODIMENTS
(5) It should also be understood that, unless a term is expressly defined in this patent there is no intent to limit the meaning of that term, either expressly or by implication, beyond its plain or ordinary meaning, and such term should not be interpreted to be limited in scope based on any statement made in any section of this patent (other than the language of the claims). To the extent that any term recited in the claims at the end of this patent is referred to in this patent in a manner consistent with a single meaning, that is done for sake of clarity only so as to not confuse the reader, and it is not intended that such claim term by limited, by implication or otherwise, to that single meaning. Finally, unless a claim element is defined by reciting the word “means” and a function without the recital of any structure, it is not intended that the scope of any claim element be interpreted based on the application of 35 U.S.C. § 112(f).
(6) The best mode for carrying out the invention is presented in terms of its preferred embodiment, herein depicted within the Figures.
1. Detailed Description of the Figures
(7) Referring now to
(8) If CAE testing appears to fail the performance specification, the design in successively improved and reiterated 24. If the CAE test in appears to meet performance specifications, a physical prototype is destructively tested 26, with failures reiterated back to the CAE program. Passage of the destructive testing results in a completed design.
(9) Referring now to
(10) Referring now to
(11) An initial performance simulation 110 is performed within the CAE program, with failing virtual results leading to virtual design iteration and passing virtual results leading to the creating of a physical prototype for destructive testing 112. Subsequent destructive testing 112 results in failing designs leading to reiteration, with passing results leading to a completed design 120.
2. Operation of the Preferred Embodiment
(12) In operation, the present method of rapid new product development is provided for anti-ballistic articles according to the preferred embodiment of the present invention. New armored products, or newly designed and improved armor products, can hereby be developed with significant decrease of the time for development of improved ballistic resistant articles. Using such methods maximize the benefits polyethylene-based composite laminated structures for new armored products in such a manner as to provide for complete ideation, development, experimentation, testing and finalization in short overall window, such as, inter Alia, within a 30 day project window.
(13) The foregoing descriptions of specific embodiments of the present invention are presented for purposes of illustration and description. The Title, Background, Summary, Brief Description of the Drawings and Abstract of the disclosure are hereby incorporated into the disclosure and are provided as illustrative examples of the disclosure, not as restrictive descriptions. It is submitted with the understanding that they will not be used to limit the scope or meaning of the claims. In addition, in the Detailed Description, it can be seen that the description provides illustrative examples and the various features are grouped together in various embodiments for the purpose of streamlining the disclosure. This method of disclosure is not to be interpreted as reflecting an intention that the claimed subject matter requires 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 configuration or operation. The following claims are hereby incorporated into the Detailed Description, with each claim standing on its own as a separately claimed subject matter. Further, the scope of the invention is in no way to be limited only by any adverse inference under the rulings of Warner-Jenkinson Company, v. Hilton Davis Chemical, 520 US 17 (1997) or Festo Corp. v. Shoketsu Kinzoku Kogyo Kabushiki Co., 535 U.S. 722 (2002), or other similar caselaw or subsequent precedent should not be made if any future claims are added or amended subsequent to this Patent Application.