|Publication number||US3108924 A|
|Publication date||Oct 29, 1963|
|Filing date||Apr 7, 1960|
|Priority date||Apr 14, 1959|
|Publication number||US 3108924 A, US 3108924A, US-A-3108924, US3108924 A, US3108924A|
|Inventors||Mountford Adie George|
|Original Assignee||Mountford Adie George|
|Export Citation||BiBTeX, EndNote, RefMan|
|Patent Citations (13), Referenced by (38), Classifications (14)|
|External Links: USPTO, USPTO Assignment, Espacenet|
Oct. 29, 1963 G. M. ADlE STRUCTURAL ELEMENT 2 Sheets-Sheet 1 Filed April '7. 1960 Oct. 29, 1963 G. M. ADlE STRUCTURAL ELEMENT 2 Sheets-Sheet 2 Filed April 7. 1960 '1 I lnve flor C K B W W ttarneys United States Patent 3,1ll8fi24 STRUCTURAL ELEMENT George lt lountford Ailie, '7 Carlos Place, London, England: Filed Apr. '7, I966 Ser. No. 26,672 Claims priority, appli-catien Great Eritain Apr. 14,1959 '7 illaims. (Cl. 16l127) This invention relates to materials and elements for use in building constructions and the like and is an improvement in or modification of prior materials or clements consisting of a slab, panel, block or the like of cellular material in which the density of the material is graded so as to be a maximum in the neighbourhood of one or both of its faces and a minimum in the neighbourhood of the opposite face or the median plane as the case may be. Such prior material or elements have been formed by the juxtaposition of thin sheets of mouldable material, such as a thermoplastic, lhaving dimples or cups formed in them, the open sides of the dimples being brought opposite each other to provide cells which were spherical in shape. The cells were so arranged that the density of the material was a maximum in the neighbourhood of both of its faces and a minimum in the neighbourhood of the median plane or" the material. Each outer load-bearing face was bounded by a skin of non-cellular material.
According to the present invention, a cellular slab, panel, block or like element is formed of a number of juxtaposed sheets having dimples formed therein of square, circular, hexagonal or other polygonal cross section. The size of the dimples in the sheets decreases from sheet to sheet away from the median plane of the element or from one of its faces to the other and the sheets are disposed so that the apex of the dimples in each intermediate sheet being nested with a dimple in an adjacent intermediate sheet and in contact with the apex of the dimples with which they are nested, the depth of the dimples in the sheets decreasing in amount by a factor of two from sheet to sheet from one side to the other of the slab, and all of the apices lying substantially within the same plane.
The dimples may for example be pyramidal or coni cal in shape or some may be pyramidal and some. conical. The sheets are preferably of mouldable material such as thermoplastic or thermosetting plastic, metal, such as mild steel or any other suitable substance. One very suitable material for all the sheets is pressed fibre because of its cheapness, ease of moulding and lightness. When pressed fibre sheets are used throughout the element then two identical centre sheets are used so that the element is balanced to counteract any variation which may occur due to the variation in a sheet of pressed fibre of one of its surfaces as compared with the other surface. When pressed fibre, thermoplastic or other suitable material is used for the sheets then they can be riveted together as well as or instead of being stuck with adhesive.
The pyramidal dimples are preferably truncated so that the apices of the dimples in all the sheets are flat surfaces all of the same size subject to the necessary allowance for the thickness of the sheet material. The pitch of the pyramidal dimples in the various sheets is preferably doubled from sheet to sheet from the outermost dimpled sheet where the density of the element is to be greatest to the middle sheet or the opposite outermost dimpled sheet where the density is to be least. The word pitc wherever used herein is intended to refer to the distance between the apices of the dimples, or in other Words, the number of dimples occupying a given area. Thus the depth of the pyramids in any relatively outer sheet is approximately half that of the depth of the pyramids in the next relatively inner sheet. This leads to the production of an element having a system of voids constituting a two-dimensional rectangular or triangular grid of which the grid lines are channels of triangular cross section.
Embodiments of the invention are illustrated in the drawing accompanying the provisional specification in which:
FIGURE 1 is an exploded view showing nine sheets which can be assembled together to make an element of which FIGURE 2 is a cross sectional view, and in the accompanying drawing in which:
FIGURE 3 is an isometric view of a modified centre sheet, and
FIGURE 4 is a section of a part of a slab incorporating the centre sheet shown in FIGURE 3.
The element shown in FIGURES l and 2 comprises a centre sheet ill, three intermediate sheets .12, 13 and 14 on each side of the centre sheet and an outer slain or sheet 15 which forms a flat face on each side of the element. The centre and each of the intermediate sheets is formed with a series of dimples in the form of hollow truncated pyramids.
The centre sheet 10 is formed with two series of identical pyramidal dimples 16 extending in opposite directions so that the bases of the pyramids occupy the whole of the projected area of the sheet.
Each of the two intermediate sheets 1-2 which are identical is dimpled with identical truncated pyramids 18 which, however, extend all in the same direction from the sheet. The pitch of the dimples 18 is half that of the dimples 16 on one side of the centre sheet 1G and their bases occupy the whole of the projected area of the sheet. The next pair of intermediate sheets 13 are also dimpled, the pitch of the dimples 20 in them being one half of that of the dimples 18. The sheets 14 are formed with still smaller dimples 22 at one half the pitch of the dimples 20.
The flat surface at the truncated apex of each pyramidal dimple is the same size and shape for each pyramid on each sheet allowing, of course, for the thickness of the sheet material and the slope of the sides of each pyramid is the same so that they can be fitted together one over the other.
The outermost sheets 15 shown in FIGURE 1 are plane.
The nine sheets shown in FIGURE 1 can be assembled to produce a slab having the cross section shown in FIG- URE 2. Alternate pyramidal dimples in the sheets 12 are engaged over the apices of the pyramidal dimples extending to one side or the other of the centre sheet 163; alternate dimples in the sheets 13 are engaged over the apices of the dimples in the sheets 12, alternate dimples in the sheets 14 are engaged over the apices of the dimples in the sheets 13, and the plane sheets 15 lie in contact with the apices of the dimples of the sheet 14. It
will be clear from an inspection of FIGURE 2 that the density of the material forming the element shown therein is greatest in the region of the outside and decreases progressively towards the inside so that material can be saved and the slab have a high strength to weight ratio. By sticking or welding the sheets together where they are in contact with each other, a block will be formed which will be of extremely light weight, which will be highly resistant to penetration and which will have a good load bearing capacity even though the load is applied over only a small area.
The truncation of the pyramidal dimples is advantageous as it facilitates construction of the dimpled sheets and also in the case of the outermost dimpled sheet which receives the finishing skin provides a good area of contact between the dimples and the outer skin.
A cross section taken at right angles to that shown in FIGURE 2 will be identical with FIGURE 2. Therefore, the system of voids defined by the sheets will consist of (i) two series of passages of approximately triangular section B, C, D, intersecting each other at right angles and forming two-dimensional grids, '(ii) the hollow interiors E, F, G of the alternate pyramidal dimples 18, 20, 22, and (iii) the interior A and H of dimples 16.
The intermediate sheets 12, 13 and 14 serve to reinforce not only the outer portions of the element but also the sloping sides of the centre sheet and enable the element to withstand highly concentrated loads at points along its length. Such an element may be weakest at its median plane where there is only one thickness of material to resist the load and therefore it may be advantageous to use a central sheet 10 of a material more highly resistant or stronger than adjacent sheets or to provide a double centre sheet. For example, the centre sheet may be of steel while the outer sheets of the composite element could be of thermoplastic material. Owing to the thickness of the material of the sheets a small web equal in width to the sheet thickness is left between the dimples. Thus the sheets in each side of the central sheet are not in line and the centre sheet is subjected to shear force when the slab 'is loaded. In order to minimize this shear force the centre sheet or sheets may be formed with a dog leg, Where it passes between the dimples in the sheets on each side of it. The dog leg has a width equal to that of the webs between the dimples or in other words equal to the thickness of the material. Thus the webs of the dimples in the sheet on one side of the centre sheet lie immediately in line with the corresponding webs in the sheet on the other side of the centre sheet, separated only by the dog leg portion of the centre sheet. In this way stresses are transmitted from one sheet to the other without subjecting the centre sheet to any substantial shear force.
An example of a slab incorporating such a dog legged centre sheet is shown in FIGURE 4. This figure shows the width of the webs 30, 32 between the dimples 18 of the sheets much exaggereated to show the construction clearly. In fact the width and that of the dog leg 34 is only equal to that of the thickness of the material of the sheet. The small webs between the dimples of one sheet lie immediately above the corresponding webs 32 between the dimples of the sheet on the other side of the centre sheet the webs 30, 32 being separated only by the dog leg portion 34 of the centre sheet. When the webs 30, 32 and dog leg portion 34 of the centre have their correct widths, equal to the thickness of the sheets, then the sides of the pyramidal dimples of one sheet will be in line with the sides of the pyramidal dimples of the sheet on the other side of the centre sheet.
Instead of the centre sheet 10 being formed with pyramidal dimples on both of its faces, two sheets having dimples formed only on one of their faces can be secured together with their open faces next to each other to provide a layer having dimples on each side. The pyramids on one sheet can be either staggered with respect to those on the other sheet, can be opposite them or can be diagonally disposed one to another. Further layers are then built up on the same manner as in the elements described above.
Alternatively a plane centre sheet may be used or indeed no centre sheet at all. In these cases a series of closed cells will be provided in the centre of the slab.
If the sheets are made of thermoplastic they will conveniently have a thickness of the order of four thousanths of an inch. This results in an element of very low weight, for example, a square foot of the seven sheet element without the outside sheets as described above and stuck together weighs approximately 7 ozs. and has a resistance to collapse exceeding a quarter of a ton per square foot.
If it is desired that the element have some particular properties such for example as acoustic or insulating properties than a sheet or blanket of material having such a property or properties may be included in the element. Such a blanket if it is very thin say only a few thousandths of an inch thick, could be placed between each of any two dimpled sheets but if it is of greater thickness then it is preferably placed between the two centre sheets.
The blanket could act as an adhesive, a hardener, a heating element, a heat containing or reflecting element, a weather-proofing or fire-proofing element or as a strengthening sheet. If desired it can be arranged to isolate all the grids of ducts between the dimples on one side of the central sheet from the grids of ducts between the dimples on the other side on the central sheet.
1. A building slab or element comprising a number of superimposed relatively thin sheets consisting of spaced outermost sheets and at least three intermediate sheets, the intermediate sheets having a regular series of truncated dimples formed therein arranged on a rectangular grid, said dimples having their sides all disposed at the same slope, the said sheets being disposed in juxtaposition, the apex of the dimples in each said intermediate sheet being nested with a dimple in an adjacent intermediate sheet and in contact with the apex of the dimples with which they are nested, the depth of the dimples in the sheets decreasing in amount by a factor of two from sheet to sheet from one side to the other of the slab, and all of the apices lying substantially within the same plane.
2. A building element as claimed in claim 1 in which the dimples are pyramidal in shape.
3. A slab comprising a number of relatively thin superimposed sheets consisting of spaced outermost sheets and at least three intermediate sheets and including a center sheet, said center sheet being formed with two regular series of dimples extending in opposite directions, the other intermediate sheets being formed with only one regular series of dimples extending in one direction, all of said dimples being arranged on rectangular grids with their sides all disposed at the same slope and having truncated apices, the said sheets being disposed in juxtaposition, the apex of the dimples in each said intermediate sheet being nested with a dimple in an adjacent intermediate sheet and in contact with the apex of the dimples with which they are nested, the depth of the dimples in the sheets decreasing in amount by a factor of'two from sheet to sheet away from the median plane of the slab, all of the apices on one side of the median plane of the slab lying substantially within a single plane, and all of the apices on the other side of the median plane lying substantially within another single plane.
4. The slab of claim 3, wherein the truncated apices of the dimples are all substantially of the same size.
5. The slab of claim 3 wherein the distance between the truncated apices of the dimples in each intermediate sheet is halved from sheet to sheet away from the median plane of the slab.
6. The slab of claim 3 wherein the bases of the dimples in the center sheet occupy the whole of the area of the center sheet.
7. The slab of claim 3 wherein the center sheet is formed with a dog-leg between the bases of the oppositely extending dimples.
References Cited in the file of this patent UNITED STATES PATENTS E1113 Sept. 4, 1934 M011 Apr. 28, 1931 Williams Aug. 30, 1932 Greulich Aug. 10, 1937 10
|Cited Patent||Filing date||Publication date||Applicant||Title|
|US1802522 *||Dec 20, 1927||Apr 28, 1931||Jacob Moll||Corrugated cardboard|
|US1875188 *||Jan 27, 1932||Aug 30, 1932||Sherman Products Corp||Unit formed of sheet material|
|US2089893 *||Aug 26, 1936||Aug 10, 1937||Greulich Gerald G||Hollow steel building structure|
|US2157374 *||Sep 28, 1936||May 9, 1939||Johns Manville||Trussed plate structure|
|US2333343 *||Jan 16, 1940||Nov 2, 1943||Armzen Company||Method of making structural materials|
|US2481046 *||Nov 13, 1947||Sep 6, 1949||Western Engineering Associates||Panel structure|
|US2549189 *||Feb 7, 1947||Apr 17, 1951||Naum Gabo||Building construction unit|
|US2809908 *||Dec 28, 1953||Oct 15, 1957||Keyes Fibre Co||Construction panel|
|US3013641 *||Apr 29, 1957||Dec 19, 1961||Thompson Ramo Wooldridge Inc||Structural element|
|USRE19301 *||Dec 19, 1930||Sep 4, 1934||Indented paper|
|FR1002117A *||Title not available|
|FR1024889A *||Title not available|
|FR1047151A *||Title not available|
|Citing Patent||Filing date||Publication date||Applicant||Title|
|US3402700 *||Jul 22, 1966||Sep 24, 1968||Sulzer Ag||Structural panel for a steam generator|
|US3461632 *||Oct 18, 1965||Aug 19, 1969||Robert G Kuhne||Lightweight cellular structural material|
|US3501878 *||May 22, 1967||Mar 24, 1970||Segal Charles||Sound and heat insulating panels|
|US3607604 *||Nov 19, 1969||Sep 21, 1971||Nava Robert D||Flame arrester and pressure relief|
|US3619340 *||Jan 21, 1969||Nov 9, 1971||Peter Jones||Multilayered thermal insulation material|
|US3642566 *||May 20, 1970||Feb 15, 1972||Irving E Figge||Quasi-isotropic sandwich core|
|US3802145 *||May 25, 1972||Apr 9, 1974||Rohr Corp||Mechanism and method for providing intra-cell thermal resistance in honeycomb panel cores|
|US3834487 *||Mar 8, 1973||Sep 10, 1974||Hale J||Sandwich core panel with structural decoupling between the outer face sheets thereof|
|US3849237 *||Apr 8, 1971||Nov 19, 1974||L Zetlin||Structural member of sheet material|
|US3894374 *||Oct 1, 1973||Jul 15, 1975||Fresa Ets||Set of elements for the construction of buildings|
|US3899805 *||Jul 13, 1973||Aug 19, 1975||Dow Chemical Co||Indented sheet|
|US3906571 *||May 30, 1974||Sep 23, 1975||Lev Zetlin||Structural member of sheet material|
|US4134243 *||Aug 25, 1977||Jan 16, 1979||Fries Donald J||Structural panels|
|US4223053 *||Aug 7, 1978||Sep 16, 1980||The Boeing Company||Truss core panels|
|US4562979 *||Mar 21, 1983||Jan 7, 1986||Aeritalia||Expandable spacecraft|
|US4875259 *||Mar 24, 1988||Oct 24, 1989||Minnesota Mining And Manufacturing Company||Intermeshable article|
|US5071363 *||Apr 18, 1990||Dec 10, 1991||Minnesota Mining And Manufacturing Company||Miniature multiple conductor electrical connector|
|US5088164 *||Mar 22, 1989||Feb 18, 1992||Minnesota Mining And Manufacturing Company||Container with intermeshable closure members|
|US5113555 *||Nov 26, 1990||May 19, 1992||Minnesota Mining And Manufacturing Company||Container with intermeshable closure members|
|US5176530 *||Sep 25, 1991||Jan 5, 1993||Minnesota Mining And Manufacturing Company||Miniature multiple conductor electrical connector|
|US5201101 *||Apr 28, 1992||Apr 13, 1993||Minnesota Mining And Manufacturing Company||Method of attaching articles and a pair of articles fastened by the method|
|US5360270 *||Apr 28, 1992||Nov 1, 1994||Minnesota Mining And Manufacturing Company||Reusable security enclosure|
|US5390467 *||Mar 14, 1994||Feb 21, 1995||Shuert; Lyle H.||Panel structure and pallet utilizing same|
|US5398889 *||Feb 22, 1994||Mar 21, 1995||Furon Company||Aircraft fuselage lining system|
|US5634245 *||Jul 14, 1995||Jun 3, 1997||Minnesota Mining And Manufacturing Company||Structured surface fastener|
|US7591114||Mar 7, 2006||Sep 22, 2009||Herron Intellectual Property Holdings, Llc||High strength low density multi-purpose panel|
|US8402715 *||Dec 21, 2005||Mar 26, 2013||Fraunhofer-Gesellschaft Zur Forderung Der Angewandten Forschung E.V.||Building panel in particular for wall covering and method for the production thereof|
|US9028020 *||Mar 11, 2011||May 12, 2015||Electrolux Home Products, Inc.||Stabilizing panel|
|US20050223675 *||Mar 8, 2004||Oct 13, 2005||Warren Herron||High strength low density multi-purpose panel|
|US20050279574 *||Jun 17, 2005||Dec 22, 2005||Walter Halterbeck||Sound-absorbing device for a wall covering, ceiling covering, or floor covering|
|US20070119120 *||Mar 7, 2006||May 31, 2007||Herron Warren L Iii||High strength low density multi-purpose panel|
|US20070251170 *||Dec 21, 2005||Nov 1, 2007||Christoph Uhlig||Building Panel in Particular for Wall Covering and Method for the Production Thereof|
|US20110297785 *||Feb 23, 2009||Dec 8, 2011||Eiji Itakura||Airframe position adjusting structure|
|US20120228252 *||Mar 11, 2011||Sep 13, 2012||Electrolux Home Products, Inc.||Stabilizing panel|
|US20130067844 *||Mar 21, 2013||Paul Rivers||Building Panel Assembly|
|US20140060965 *||May 14, 2012||Mar 6, 2014||Yeseco Oy||Acoustic panel|
|US20150068835 *||Sep 9, 2014||Mar 12, 2015||Scambia Holdings Cyprus Limited||Muffler shell for use in the exhaust system of a vehicle|
|WO1995022487A1 *||Feb 15, 1995||Aug 24, 1995||Furon Company||Aircraft fuselage lining system|
|U.S. Classification||428/158, 181/292, 244/133, 244/117.00R, 52/789.1, D25/158, 428/172, 428/603|
|Cooperative Classification||E04C2002/3438, E04C2002/3422, E04C2002/3472, E04C2/3405|