Search Images Maps Play YouTube News Gmail Drive More »
Sign in
Screen reader users: click this link for accessible mode. Accessible mode has the same essential features but works better with your reader.

Patents

  1. Advanced Patent Search
Publication numberUS2682491 A
Publication typeGrant
Publication dateJun 29, 1954
Filing dateFeb 23, 1952
Priority dateFeb 23, 1952
Publication numberUS 2682491 A, US 2682491A, US-A-2682491, US2682491 A, US2682491A
InventorsHahn Stuart H
Original AssigneeDalmo Victor Company
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Skin for doubly curved sandwichtype panels
US 2682491 A
Images(1)
Previous page
Next page
Description  (OCR text may contain errors)

June 29, 1954 S. H. HAHN SKIN FOR DOUBLY CURVED SANDWICH-TYPE PANELS Filed Feb. 23. 1952 IN V EN TOR. Stuart H Hahn ATTORA/E YS Patented June 29, 1954 S KIN FOR DOUBLY CURVED SANDWICH- TYPE PANELS Stuart H. Hahn, Los Gatos, Calif., assignor to Dalmo Victor Company, San Carlos, Calif., a corporation of California Application February 23, 1952, Serial No. 272,951

3 Claims.

This invention relates to a doubly curved product and to a method of forming the same.

There is very little difficulty encountered in producing a so-called singly curved product, such as a segment of a cylinder, since a laminated article can be readily fabricated by providing a suitable core and facing the same with a sheet on either side thereof. It is obvious that a flat thin sheet readily conforms to a cylindrical shape. However, when producing a doublycurved product, such as a segment of a sphere or a paraboloid etc, difficulties are immediately encountered in trying to provide the doubly curved facings or skins, since it is equally apparent that a flat sheet does not readily con-form to a spherical or other doubly curved surface.

In an attempt to circumvent the problem of providing doubly curved skins, some doubly curved articles have been cast. These cast articles have been satisfactory where weight is not a problem and Where a high stiffness to weight ratio is not required. However, certain doubly curved articles, such as doubly curved radar reflectors, must be both light in weight and havev a high stiffness to weight ratio. In an attempt to lighten cast articles. they have been perforated but unfortunately this produces a relatively flexible product. Flexing of these reflectors during use obviously distorts the beam transmitted and the signals received by these reflectors.

In order to provide a light stiff doubly curved reflector, it has been the ractice in the prior art to form a" laminated or sandwich-type article having a cellular core and-front and back sheet metal skins. However, unless the core material has a varying thickness from the center outwardly, it is necessary to use two sets of very expensive die equipment to accurately form the concave and convex skins, it being obvious that both skins cannot be formed by the same die equipment. If the core is made of variable thickness so that the front and rear skins can be formed by the same die equipment, the die equipment requirements are reduced .but a high cost is encountered in forming such a variable thickness core.

. It is therefore a main object of the present invention to provide a doubly curved sandwiched article, particularly one having a metallic sur- I face for use as a radar reflector, which article,

although being very light in weight, has a high stiffness to weight ratio.

Another main object of the present invention is to provide a method for forming an article having a doubly curved surface, which method is simple and does not necessitate the use of expensive and complex equipment.

Another object of the present invention is .to provide a simple and improved metal faced radar dish having accuracy of contour and a high stiffness to weight ratio.

Various other objects of the invention will be apparent from the following description taken in connection with the accompanying drawings wherein:

Fig. 1 is a three-dimensional view of a radar dish or reflector embodying the concepts of the present invention.

Fig. 2 is a front elevational view of the dish disclosed in Fig. 1. i

Fig. 3 is an enlarged cross-sectional view'of the dish taken on line 33 of Fig. 2.

Referring to the accompanying drawings wherein similar reference characters indicate similar parts throughout, the radar dish or reflector shown and representing one embodiment of my invention comprises a doubly curved cellular core 9 having a front facing or skin H secured to the concave side thereof and a rear facing or skin l3 secured to the convex side thereof. Since the facings are identical in construction, only the front facing ll need be described in detail.

Front facing ll comprises two layers [5 and l1 joined together by an adhesive material, such material throughout the construction being generally entitled l9. Each of the layers [5 andl1 comprises a plurality of narrow metallic foil strips 2! arranged and adhesively secured in overlapping or shingled relation to one another. Layer I! is adhesively secured to the front concave surface of the cellular core 9 and layers 15 and I? are adhesively secured to one another.

As is apparent from Fig. 2, the strips of one layer of facing I l are arranged at an angle, preferably 90, to the otherlayer of the facing to achieve a maximum amount of strength and stiffness. The strips 2| of rear facing i 3 are similarly arranged and adhesively secured in place to the rear convex surf-ace of cellular core 9.

It is pointed out that by making the strips 2| thin and relatively narrow, the amount of wrinkling of the strips is kept to a minimum. These strips can be built up on the core without any appreciable wrinkling if at least two of their I dimensions are small in comparison to the curvature of the cellular core. The two dimensions selected are the thickness of the strip and its width. Although, of course, some wrinkling'does occur, the extent thereof is not suflicient to detrimentally efiect the transmission of signals from or the reception of signals by the dish, since it is the general con-tour of the dish (apart from severe wrinkling) that determines to a large degree whether reception and transmission of radio frequency energy by the radarrefiector will be distorted or not.

By using thin foil-like forms of light metals, such as aluminum, maximum advantage can be taken of the hardness and strength which are inherent in severely cold-worked metal, whereas a comparable single-ply sheet of metal would necessarily be much softer and weaker.

A novel and inexpensive manner of forming a doubly-curved article as above described comprises the steps of forming a mal form havin a doubly curved convex workin surface conforming to the curvature desired of the concave side of the final product. Such a form can be inexpensively constructed of wood. After the provision of such a form, strips 2| of layer I5 are then laid on the form and overlapped in a shingle fashion, it being preferable that the overlap be approximately 50 per cent of the width of a strip so that each layer has in effect an even two-pl thickness, therebydistinctly lessening the irregularities on the faces of the dish which would otherwise be produced with a lesser or greater amount of overlapping at the overlapped joints of the strips of the two layers. Concurrent with the laying of. the strips, a suitable adhesive material is applied to th strips so that the strips are secured to one another. A suitable adhesive for this purpose is a phenolic thermo-setting resin or an epichlorhydrin polymer, commercially given the name of Epon VI. The latter adhesive has a low curing temperature and low shrinking characteristics upon polymerization. A primary advantage of such an adhesive is that all differential expansion difficulties inherent. in the use of the usual adhesives, which have high curing temperatures, is avoided.

Strips 2| of layer I! are next applied or built upon the wooden form on top of layer i5 and adhesively secured thereto and. are adhesively secured to one another in shingled fashion and arranged at an angle, preferably 90, to the strips of layer [5 to achieve maximum strength from the strip construction. Next, a cellular core of uniform or non-uniform thickness, which may be previously formed doubly curved, by any simple process, is applied and adhesively secured to layer i l, the adhesive. material assuring good conformity of the core to the layer. Such a core can be readily formed from a fiberglass honeycombed panel by a simple heating step or, if the cellular core is to be a metallic honeycombed panel, such can be made up of triangular se ments bent to a doubly curved configuration.

Finally, the two layers of facing I3 are laid and adhesively secured to one another and to the core 0. The adhesive material is then allowed to dry or polymerize. However, it may be desired to insure an accurate conformity of the built-up structure to the form and this can be readily accomplished and insured by enclosing the built-up structure and the form in a bag and then evacuating the air from the bag to apply atmospheric pressure to the laminated or sandwiched product and force it against the curvature of the form.

It is preferable that a separant such as a soap, grease or a commercial mold lubricant be applied to the form prior to building up the layers therethe resulting article being from on to enable eas removal of the completed product.

In the above-described process and in the previously described product, only two cross layers per facing were described, but it is obvious that as many layers as desired can be added. In fact, it is contemplated that a multiplicity of plied-up layers of strips will be utilized in forming the usual product.

By way of example and not by way of limitation, foil used in the above process for producing a dish 6 feet in diameter had a thickness of from .0005 inch to .005 inch and a width approximately 4 inches, the overall thickness of A2 inch to 3 inches thick, Ordinarily, at least two layers per facing will be used so that one layer can cross the other layer. However, in special circumstances, it is contemplated that only one layer might be used although it is obvious that a twolayer facing will have considerably more strength than a single layer even taken in proportion to the thickness of the two facings.

Although the building up process. has been described with reference to the use of strips, it is contemplated that such a construction couldbe built up by the use of individual shingles or fishscale-like pieces, although it is believed that the strip formation is less expensive and more readily carried out than a fishscale-type construction.

It is additionally pointed out that metallic bonding of the individual foil strips to one another is found unnecessary in the case of radar reflectors becauseof the inherent high capacitative coupling of the closely adjacent foil pieces which are separated by a few thousandths of an inch or less by the adhesive bonding material which is normally a dielectric. However, conducting or semi-conducting adhesives may be used as well.

By the present invention a doubly curved sandwich-type article has been provided having an extremely high stiffness to Weight ratio and which can be easily fabricated w th a minimum use of equipment and time, yet which article can be produced having an accurate contour suitable for use as a radar reflector. Obviously, the invention has wide application in the construction of a Wide range of doubly curved articles, both metal faced and otherwise, and that the reference to a radar reflector merely illustrates a practical application of the concepts of the present invention.

While I have shown the preferred form of my invention, it is to be understood that various changes may be made in its construction by those skilled in the art without departing from the spirit of the invention as defined in the appended claims.

Having thus described my invention, what I claim and desire to secure by Letters Patent is:

1. A doubly curved article having a doubly curved honeycomb core with a facing on each of its opposite sides, each facing having a first and second layer, each layer including a plurality of thin strips arranged and secured in shingled fashion to one another with a constant width of exposed surface throughout the length of each strip, the innermost layers of the facings being secured to the honeycomb core, the strips of each layer running at an angle to the strips of the immediately adjacent layer.

2. A doubly curved radar reflector comprising a central honeycombed core, and interior and exterior metallic skins covering said core, each of 5 said skins having a first layer of thin foil strips adhesively secured to said core, said strips being adhesively secured to one another in overlapping shingled relation with a constant width of exposed surface throughout the length of each strip, a second layer of thin foil strips adhesively secured to each first layer and arranged at an angle to the strips of the first layer, the strips of each second layer being adhesively secured to one another in overlapping shingled relation with a constant width of exposed surface throughout the length of each strip.

3. The method of making a doubly curved article comprising providing a male form having a doubly curved convex working surface; laying a layer of strips of constant width across the convex surface, arranging and securing the strips to one another in overlapping shingled fashion with a constant degree of overlap; laying a second layer of strips of constant width across the first layer of strips, adhesively securing the strips of the second layer to the first layer at an angle to the strips of the first layer, arranging the strips of the second layer and securing them to one another in overlapping shingled fashion with a constant degree of overlap, laying a honeycombed cellular core onto the second layer and securing the core to said second layer, laying a third layer of strips of constant width onto the cellular core with the strips being arranged and secured to one another in overlapping shingled relation with a constant degree of overlap, and laying a fourth layer of strips of constant width across the third layer of strips with the strips of the fourth layer being adhesively secured to the third layer at an angle to the strips of the third layer, arranging the strips of the fourth layer in parallel relation and securing them to one another in overlapping shingled fashion with a constant degree of overlap.

References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 2,448,114 Olson et al. Aug. 31, 1948 2,578,781 Brundige Dec. 18, 1951 2,592,080 Thompson Apr. 8, 1952 OTHER REFERENCES 30 Foot Tower, Modern Plastics, December 1950, page 138.

Honeycomb Sandwich Construction, Plastics (London), October 1949, pages 64-66.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US2448114 *May 18, 1943Aug 31, 1948Goodrich Co B FMethod for making heat-molded articles containing fabric reinforcements
US2578781 *Jan 18, 1945Dec 18, 1951Samuel Brundige RoyManufacture of plywood
US2592080 *Jun 6, 1947Apr 8, 1952Weavewood IncMethod of molding dishlike articles
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2742387 *Sep 28, 1953Apr 17, 1956Lavoie Lab IncReflector for electromagnetic radiations and method of making same
US2747180 *Jun 20, 1952May 22, 1956Zenith Plastics CompanyRadar reflector
US2777790 *Oct 1, 1953Jan 15, 1957Steven P KishMethod of making reproduction fixtures
US2804909 *Jun 23, 1954Sep 3, 1957Hammer SamuelMethod for forming sheet material
US3119109 *Dec 31, 1958Jan 21, 1964Raytheon CoPolarization filter antenna utilizing reflector consisting of parallel separated metal strips mounted on low loss dish
US3137602 *Aug 21, 1959Jun 16, 1964Continental Can CoCeramic honeycomb
US3150026 *Apr 22, 1960Sep 22, 1964Ferro CorpApparatus for placing and bonding weft strands to continuous warp strands
US3200026 *Apr 21, 1960Aug 10, 1965Brown Arthur TMethod of producing a shell roof structure
US3372075 *Mar 6, 1964Mar 5, 1968Amercoat CorpMethod of making an insulated storage tank
US3459617 *Feb 23, 1965Aug 5, 1969Ernest B Dane JrMethod for constructing a boat hull
US3483614 *May 26, 1967Dec 16, 1969Hexcel Products IncMethod for making dimpled honeycomb sandwich
US4188358 *Mar 14, 1977Feb 12, 1980U.S. Philips CorporationFlamespraying thermohardening resin saturated fibrous layer
US4463055 *Apr 27, 1983Jul 31, 1984Hodges Marvin PReflective film and method of applying same
US4575726 *Aug 16, 1982Mar 11, 1986Rca CorporationAntenna construction including two superimposed polarized parabolic reflectors
US4635071 *Aug 10, 1983Jan 6, 1987Rca CorporationElectromagnetic radiation reflector structure
US5333003 *Jan 21, 1992Jul 26, 1994Trw Inc.Laminated composite shell structure having improved thermoplastic properties and method for its fabrication
US7907081 *Dec 25, 2006Mar 15, 2011Rafael - Armament Development Authority Ltd.Millimeter wave imaging system
DE1013722B *Oct 13, 1955Aug 14, 1957Marconi Wireless Telegraph CoRichtantenne fuer sehr kurze elektromagnetische Wellen nach Art einer reflektierenden Flaeche oder einer Linse
DE3333951A1 *Sep 20, 1983Mar 22, 1984Rca CorpAntennenhalterung
Classifications
U.S. Classification343/912, 342/5, 156/197, 156/297, 428/116, 156/224, 244/126, 428/109, 428/64.1
International ClassificationH01Q15/14, B32B15/08
Cooperative ClassificationB32B15/08, H01Q15/144
European ClassificationB32B15/08, H01Q15/14B1B