|Publication number||USH1481 H|
|Application number||US 08/082,069|
|Publication date||Sep 5, 1995|
|Filing date||Jun 23, 1993|
|Priority date||Jun 23, 1993|
|Publication number||08082069, 082069, US H1481 H, US H1481H, US-H-H1481, USH1481 H, USH1481H|
|Original Assignee||The United States Of America As Represented By The Secretary Of The Navy|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (6), Referenced by (24), Classifications (8), Legal Events (1)|
|External Links: USPTO, USPTO Assignment, Espacenet|
The invention described herein may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
The present invention relates generally to sandwich constructions suitable for use in structural and non-structural members, and more particularly to sandwich constructions of low-density cores bonded between thin-gauge, high-strength face sheds for use in a wide range of military, industrial and commercial components.
Sandwich constructions are finding broad application as structural and non-structural members in boats, aircraft, furniture, appliances, and other items requiring high strength, light-weight materials. They typically include face sheets bonded to either side of a low density core and can be made of such materials as metals, plastics or composite fiberglass laminates for rigidity and strength. Among the various core materials are rigid plastic foams, honeycombs, truss-core corrugations and an arrangement of adjacent, inclined rectangular-shaped facets connected by intermediate rows of adjoining parallelagram-shaped facets.
In aircraft design the need for weight efficiency and aerodynamically smooth surfaces under high stress levels has stimulated use of sandwich construction as a possible substitute for the conventional sheet-stringer construction. Notwithstanding the superior weight-efficiency of the sandwich constructions, their general acceptance for critical applications has lagged behind theoretical development primarily because of maintenance problems experienced in service. Honeycomb core sandwich constructions, for instance, are considered to be among the most weight-efficient but, due to their tendency to retain moisture which may become entrapped due to ineffective edge seals or unbonding of face sheets from the core. This may degrade the structural integrity and lead to extensive corrosion and premature failure of components. Experience has shown a significant frequency of repairs on replacements which are very time-consuming and expensive.
Accordingly, an object of the present invention is to provide a sandwich construction having a high strength-to-weight efficiency suitable for a broad variety of military, industrial and commercial applications.
Another object is to provide a low-density core sandwich construction in which corrosion and degradation of structural integrity due to retention of moisture is substantially eliminated.
Another object is to provide a sandwich construction in which unbonding of face sheets from the core is substantially reduced or eliminated when heat, pressure or vacuum is applied for purposes of repair.
Still another object is to provide a sandwich construction having a flexible core with structural discontinuities for improved tolerance for damage.
These and other objects of the invention are achieved in a sandwich construction comprising strips of corrugations arranged adjacent one another and alternately offset so that a series of peaks is next to a series of troughs, and vice versa, and contained between upper and lower face sheets. By arranging the strips in this alternating fashion, a plurality of passage-ways from cell to cell is provided. The outer face sheets and the strips are cocured in one operation without any secondary bonding.
The novel features which are believed to be characteristics of the invention, both as to its organization and methods of operation, together with further objects and advantages thereof, will be better understood from the following descriptions in connection with the accompanying drawings in which the presently preferred embodiments of the invention are illlustrated by way of examples. It is to be expressly understood, however, that the drawings are for purposes of illustration and description only and are not intended as a definition of the limits of the invention.
FIG. 1 shows a partially cutaway, perspective view of a prior art corrugated sandwich construction;
FIG. 2 shows a similar view of the instant invention, showing offset corrugationns that provide moisture pathways and also showing a series of shape-mandrels, extended from inside the corrugations, that can be used to form the offset pattern;
FIG. 3 shows a front elevation of the offset corrugation construction;
FIG. 4 shows a top view, with the upper face sheet partially cut away of the offset corrugations; and
FIG. 5 shows a cross-sectional view of the offset corrugations, taken along lines V-V of FIG. 3.
Referring now to the drawings wherein like referenced characters designate like or corresponding components throughout the several views, there is shown in FIG. 1 a typical prior art corrugated sandwich construction 20 having open cells 23a,b and c alternately adjacent open cells 24a,b, contained between face sheets 21a and b. The only difference between the cells being that cells 23a,b and c have a flat roof section 26 adjacent face sheet 21a and cells 24a,b have a flat roof section 27 adjacent face sheet 21b. Cells 23 and 24 are formed by corrugations, consisting of peaks and troughs, in a core material, which can be various metals, plastics, composites or non-composites, and face sheets 21a and b are bonded to appropriate roof sections 26 and 27, respectively. Under stress, the face sheets may crack or separate from the cells, permitting moisture to accumulate therein, and with time, cause the core material to increase in weight and corrode. The usual procedure for repair entails cleaning out any damage and resealing the face sheets by applying heat and pressure (or vacuum) thereto. This is unreliable and sometimes causes further problems with the face sheets.
Referring now to the inventive embodiment of FIGS. 2 through 5, there is shown a sandwich construction 35 comprising corrugated strips 41 and 43, each having peaks 45 and troughs 47, offset, or out of phase by a predetermined amount, contained between upper and lower face sheets 51a and b, respectively. This offset corrugated construction provides hexagonally shaped cells 55 surrounded on either side by individual triangular cells 58. The material used for a particular core is separated into strips 41, of approximately one-half inch in width and wrapped around a set of mandrels 60,61, as shown in FIG. 2. Strips 41 can be of any suitable size and can depend on the overall size and strength of the sandwich construction. Mandrels 60,61 maintain the desired shape and spacing during attachment of face sheets 51a and b, but are then removed after the cocuring operation. This design allows pathways for any moisture that may find its way into the core. Mandrels 60,61 can be any solid type material, such as TFE or other similar materials, to facilitate removal after curing.
Experimental work with a test sample constructed with this offset corrugated core, as compared to a sample constructed using a prior art design, shows a 56% increase in transverse shear stiffness in the weaker direction (in the direction of corrugation). A comparison of bending stiffness shows no measurable difference between the two.
Finally, while the offset corrugated core sandwich construction has been described with reference to a particular embodiment, it should be understood that the embodiment is merely illustrative as there are numerous variations and modifications which may be made by those skilled in the art. Thus, the invention is to be construed as being limited only by the spirit and scope of the appended claims.
|Cited Patent||Filing date||Publication date||Applicant||Title|
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|US3574103 *||Sep 6, 1968||Apr 6, 1971||Atomic Energy Commission||Laminated cellular material form|
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|U.S. Classification||428/98, 428/114|
|International Classification||B32B3/28, B31D3/00|
|Cooperative Classification||B32B3/28, B31D3/005|
|European Classification||B32B3/28, B31D3/00C|
|Jun 23, 1993||AS||Assignment|
Owner name: UNITED STATES OF AMERICA, THE, AS REPRESENTED BY T
Effective date: 19930622
Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:RAY, HEMEN;REEL/FRAME:006603/0951