US2796157A - Structural panel construction - Google Patents

Structural panel construction Download PDF

Info

Publication number
US2796157A
US2796157A US585822A US58582256A US2796157A US 2796157 A US2796157 A US 2796157A US 585822 A US585822 A US 585822A US 58582256 A US58582256 A US 58582256A US 2796157 A US2796157 A US 2796157A
Authority
US
United States
Prior art keywords
ribbon
ribbons
unit
core
panel construction
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US585822A
Inventor
Charles R Ginsburg
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US585822A priority Critical patent/US2796157A/en
Application granted granted Critical
Publication of US2796157A publication Critical patent/US2796157A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C2/00Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels
    • E04C2/30Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure
    • E04C2/34Building elements of relatively thin form for the construction of parts of buildings, e.g. sheet materials, slabs, or panels characterised by the shape or structure composed of two or more spaced sheet-like parts
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49826Assembling or joining
    • Y10T29/49879Spaced wall tube or receptacle
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628Nonplanar uniform thickness material
    • Y10T428/24661Forming, or cooperating to form cells
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628Nonplanar uniform thickness material
    • Y10T428/24669Aligned or parallel nonplanarities
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24628Nonplanar uniform thickness material
    • Y10T428/24669Aligned or parallel nonplanarities
    • Y10T428/24686Pleats or otherwise parallel adjacent folds

Definitions

  • This invention is particularly concerned with structural units which in one embodiment may constitute the spacing and reinforcing elements adapted to serve as the body portion of a structural element. Devices of this nature have a low weight-to-strength ratio and are desirable as a strain resisting member. These structures are adapted for use as floor panels, for aircraft and building industry as well as a variety of other places.
  • An object is to produce a new and improved structural unit provided with a plurality of cone-like cells having a high degree of strength and stiffness in combination with lightness of weight and which may be formed of metallic or non-metallic material or combinations thereof.
  • Another object is to produce a simple and efiicient structural unit which has the important and unique features of construction and assembly hereinafter described.
  • Figure l is a perspective view, partly broken away, illustrating a composite structural member and showing one of the structural units partly unfolded;
  • Figure 2 is an enlarged perspective view of a structural unit showing the manner in which it is formed from two ribbons of bendable sheet material, such as aluminum;
  • Figure 3 is an enlarged fragmentary elevation of one of the ribbons after being folded or braided.
  • the illustrated embodiment of the invention comprises a pair of spaced panels and 11 between which are interposed a plurality of closely spaced parallely arranged core units 12 which are adhesively secured in place by a suitable adhesive, such for example as a thermo setting synthetic resin.
  • a suitable adhesive such for example as a thermo setting synthetic resin.
  • Suitable resins are phenol formaldehyde or polymerized phenol formaldehyde.
  • a modifier may be added for reducing brittleness in the form of alcohol soluble polyamid or neoprene.
  • Each core unit 12 is formed from a pair of ribbons 14 and 15 preferably of light gauge sheet aluminum.
  • Figure 2 illustrates the manner in which the ribbons are folded to form a unit. It will be observed that the two ribbons are first disposed at right angles to each other with a portion of the ends lapped. Then successively the ribbons are folded over upon each other, allowing a slight spacing between a bend of one ribbon and the adjacent edge of the other ribbon. First one ribbon is folded at right angles upon the other ribbon, then the latter ribbon is folded in the opposite direction at right angles upon the first ribbon. The folds in each instance are loose to enable subsequent twisting action. This folding is carried out until the desired length of core unit is obtained.
  • the structure so formed is extended longitudinally and twisted to oppose the tendency of the structure to unfold, so that each of the sides of the unit is parallel to the opposite side, forming a' generally rectangular structure in cross-section.
  • An alternate method of forming a core unit consists in effecting a twist as the ribbons are interlaced and at the same time providing the desired spacing of the bent portions of one ribbon from the other. This may be achieved by making the folds over a suitable forming tool.
  • each cell 16 being generally V-shaped with opposite side walls 17 and 18 and a closed apical wall 19.
  • the wall 18 at the front ( Figure 2) is relatively long and of S shape, and the rear edge is substantially straight up and down.
  • the lower portion of the front edge portion, as indicated at 20 snugly engaging the other ribbon out at the top, as indicated at 21, there is somewhat more material, the ribbon curving gently over and downwardly as shown.
  • conical cells are formed so that relatively great weight can be supported without danger of buckling.
  • a cone-like support is provided as distinguished from a less substantial cylindrical support.
  • the cells are alternately arranged; that is one opens to one side of the unit and the next adjacent cell opens in the opposite direction. Thus throughout the length of each unit, the cells are alternately arranged and alternately face in opposite directions. This arrangement obtains, regardless of which of the four sides of the unit is viewed.
  • the core units 16 can be varied as desired, this depending upon the length of the ribbons employed to form the individual core units.
  • the core units can be made of any suitable length and width and then severed to the length that is desired for a particular panel structure.
  • the necessity of making the core units or the core specific in size for a definite panel is not necessary and consequently quantity production can be carried out more efliciently and economically.
  • the manner in which the core units are assembled is also of importance from an economic standpoint since they can be placed in sandwich form and adhesively united to the opposite panels quickly and efiiciently.
  • a structural member comprising a surface panel formed of a pair of relatively thin sheets of material disposed in spaced parallel planes with opposed inner sides, and a core between said sheets, said core comprising a plurality of core units arranged in juxtaposed parallel relation, each unit comprising a pair of ribbons of sheet material, said ribbons being undulant, each with a series of successively oppositely bent portions and being successively oppositely twisted between the bent portions providing a series of alternately facing cone-shaped cells, the ribbons of each pair being disposed with the surfaces thereof generally at right angles and loosely interlacing with one another, each bent portion of one ribbon passing over .an edge between the bent portions of the other ribbon, thereby providing alternate sharp and bent edge portions along each side of each unit, said units having opposite References Cited in the file of this patent UNITED STATES PATENTS Yarrington Jan. 31, 1893 Pajak Sept. 2, 1952

Description

June 18, 1957 INVENTOR.
CHARLES R. GINSBURG ATTORNEY STRUCTURAL PANEL CONSTRUCTION Charles R. Ginsburg, Toledo, Ohio Application May 18, 1956, Serial No. 585,822
1 Claim. (Cl. 189-34) This invention is particularly concerned with structural units which in one embodiment may constitute the spacing and reinforcing elements adapted to serve as the body portion of a structural element. Devices of this nature have a low weight-to-strength ratio and are desirable as a strain resisting member. These structures are adapted for use as floor panels, for aircraft and building industry as well as a variety of other places.
An object is to produce a new and improved structural unit provided with a plurality of cone-like cells having a high degree of strength and stiffness in combination with lightness of weight and which may be formed of metallic or non-metallic material or combinations thereof.
Another object is to produce a simple and efiicient structural unit which has the important and unique features of construction and assembly hereinafter described.
Other objects and advantages will appear more fully hereinafter and for purposes of illustration but not of limitation, an embodiment of the invention is shown on the accompanying drawings in which Figure l is a perspective view, partly broken away, illustrating a composite structural member and showing one of the structural units partly unfolded;
Figure 2 is an enlarged perspective view of a structural unit showing the manner in which it is formed from two ribbons of bendable sheet material, such as aluminum; and
Figure 3 is an enlarged fragmentary elevation of one of the ribbons after being folded or braided.
The illustrated embodiment of the invention, as shown on Figure 1, comprises a pair of spaced panels and 11 between which are interposed a plurality of closely spaced parallely arranged core units 12 which are adhesively secured in place by a suitable adhesive, such for example as a thermo setting synthetic resin. Suitable resins are phenol formaldehyde or polymerized phenol formaldehyde. A modifier may be added for reducing brittleness in the form of alcohol soluble polyamid or neoprene.
Each core unit 12 is formed from a pair of ribbons 14 and 15 preferably of light gauge sheet aluminum. Figure 2 illustrates the manner in which the ribbons are folded to form a unit. It will be observed that the two ribbons are first disposed at right angles to each other with a portion of the ends lapped. Then successively the ribbons are folded over upon each other, allowing a slight spacing between a bend of one ribbon and the adjacent edge of the other ribbon. First one ribbon is folded at right angles upon the other ribbon, then the latter ribbon is folded in the opposite direction at right angles upon the first ribbon. The folds in each instance are loose to enable subsequent twisting action. This folding is carried out until the desired length of core unit is obtained. After the desired length or predetermined length has been obtained by the alternate folding of one ribbon upon the other, then the structure so formed is extended longitudinally and twisted to oppose the tendency of the structure to unfold, so that each of the sides of the unit is parallel to the opposite side, forming a' generally rectangular structure in cross-section.
An alternate method of forming a core unit consists in effecting a twist as the ribbons are interlaced and at the same time providing the desired spacing of the bent portions of one ribbon from the other. This may be achieved by making the folds over a suitable forming tool.
It will be found that the completed structure has a series of cells 16, each cell being generally V-shaped with opposite side walls 17 and 18 and a closed apical wall 19. It should be observed that in each cell 16 the wall 18 at the front (Figure 2) is relatively long and of S shape, and the rear edge is substantially straight up and down. The lower portion of the front edge portion, as indicated at 20, snugly engaging the other ribbon out at the top, as indicated at 21, there is somewhat more material, the ribbon curving gently over and downwardly as shown. As a result conical cells are formed so that relatively great weight can be supported without danger of buckling. Thus a cone-like support is provided as distinguished from a less substantial cylindrical support.
The cells are alternately arranged; that is one opens to one side of the unit and the next adjacent cell opens in the opposite direction. Thus throughout the length of each unit, the cells are alternately arranged and alternately face in opposite directions. This arrangement obtains, regardless of which of the four sides of the unit is viewed.
When several of the units are arranged in side by side relation, such as indicated on Figure 1 and adhesively secured to the panels 10 and 11, an exceedingly sturdy structure is obtained and one which can withstand very great weights without collapsing. The arrangement of the core units and their inherent form provide a barrier against the flow of air from one side to the other. The various cells trap air and thus form a very satisfactory insulation. In the event that it is desired to permit air circulation between the panels 10 and 11, perforations (not shown) can be formed in the walls of the core units for this purpose.
From the above, it will be manifest that panels of any desired size can be readily made since the length of the core units 16 can be varied as desired, this depending upon the length of the ribbons employed to form the individual core units. Thus from a quantity production standpoint it will be manifest that the core units can be made of any suitable length and width and then severed to the length that is desired for a particular panel structure. The necessity of making the core units or the core specific in size for a definite panel is not necessary and consequently quantity production can be carried out more efliciently and economically. The manner in which the core units are assembled is also of importance from an economic standpoint since they can be placed in sandwich form and adhesively united to the opposite panels quickly and efiiciently.
This application constitutes a continuation-in-part of my application, Serial No. 504,241, filed April 27, 1955 and entitled Structural Unit.
Numerous changes in details of construction, arrangement and operation and choice of materials may be effected without departing from the spirit of the invention, especially as defined in the appended claim.
What I claim is:
A structural member comprising a surface panel formed of a pair of relatively thin sheets of material disposed in spaced parallel planes with opposed inner sides, and a core between said sheets, said core comprising a plurality of core units arranged in juxtaposed parallel relation, each unit comprising a pair of ribbons of sheet material, said ribbons being undulant, each with a series of successively oppositely bent portions and being successively oppositely twisted between the bent portions providing a series of alternately facing cone-shaped cells, the ribbons of each pair being disposed with the surfaces thereof generally at right angles and loosely interlacing with one another, each bent portion of one ribbon passing over .an edge between the bent portions of the other ribbon, thereby providing alternate sharp and bent edge portions along each side of each unit, said units having opposite References Cited in the file of this patent UNITED STATES PATENTS Yarrington Jan. 31, 1893 Pajak Sept. 2, 1952
US585822A 1956-05-18 1956-05-18 Structural panel construction Expired - Lifetime US2796157A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US585822A US2796157A (en) 1956-05-18 1956-05-18 Structural panel construction

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US585822A US2796157A (en) 1956-05-18 1956-05-18 Structural panel construction

Publications (1)

Publication Number Publication Date
US2796157A true US2796157A (en) 1957-06-18

Family

ID=24343097

Family Applications (1)

Application Number Title Priority Date Filing Date
US585822A Expired - Lifetime US2796157A (en) 1956-05-18 1956-05-18 Structural panel construction

Country Status (1)

Country Link
US (1) US2796157A (en)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2982846A (en) * 1958-08-05 1961-05-02 Poly Ind Inc Laminated structure and method of fabricating the same
US3017971A (en) * 1958-03-24 1962-01-23 Formacel Inc Cellular cored panels and continuous process for manufacturing same
US3057057A (en) * 1958-10-01 1962-10-09 Engelhard Ind Inc Method of making a honeycomb sandwich structure
US3068565A (en) * 1958-10-16 1962-12-18 Nat Distillers Chem Corp Method of making honeycomb laminate
US3114612A (en) * 1959-05-15 1963-12-17 Eugene W Friedrich Composite structure
US3884646A (en) * 1972-12-05 1975-05-20 James T Kenney Structural panel and method of fabrication thereof
US4414257A (en) * 1981-07-09 1983-11-08 Mitsubishi Denki Kabushiki Kaisha Elevator panel
US5535912A (en) * 1994-03-17 1996-07-16 A. O. Smith Corporation Metal liner for a fiber-reinforced plastic tank
US20080020188A1 (en) * 2006-07-24 2008-01-24 Tessellated Group Three-dimensional support structure
US20110042035A1 (en) * 2009-08-19 2011-02-24 Alstom Technology Ltd Heat transfer element for a rotary regenerative heat exchanger
US10094626B2 (en) 2015-10-07 2018-10-09 Arvos Ljungstrom Llc Alternating notch configuration for spacing heat transfer sheets
US10175006B2 (en) 2013-11-25 2019-01-08 Arvos Ljungstrom Llc Heat transfer elements for a closed channel rotary regenerative air preheater
US10197337B2 (en) 2009-05-08 2019-02-05 Arvos Ljungstrom Llc Heat transfer sheet for rotary regenerative heat exchanger
US10378829B2 (en) 2012-08-23 2019-08-13 Arvos Ljungstrom Llc Heat transfer assembly for rotary regenerative preheater
US10914527B2 (en) 2006-01-23 2021-02-09 Arvos Gmbh Tube bundle heat exchanger

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US490938A (en) * 1893-01-31 Spring
US2609068A (en) * 1949-03-11 1952-09-02 Glenn L Martin Co Metal foil honeycomb core

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US490938A (en) * 1893-01-31 Spring
US2609068A (en) * 1949-03-11 1952-09-02 Glenn L Martin Co Metal foil honeycomb core

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3017971A (en) * 1958-03-24 1962-01-23 Formacel Inc Cellular cored panels and continuous process for manufacturing same
US2982846A (en) * 1958-08-05 1961-05-02 Poly Ind Inc Laminated structure and method of fabricating the same
US3057057A (en) * 1958-10-01 1962-10-09 Engelhard Ind Inc Method of making a honeycomb sandwich structure
US3068565A (en) * 1958-10-16 1962-12-18 Nat Distillers Chem Corp Method of making honeycomb laminate
US3114612A (en) * 1959-05-15 1963-12-17 Eugene W Friedrich Composite structure
US3884646A (en) * 1972-12-05 1975-05-20 James T Kenney Structural panel and method of fabrication thereof
US4414257A (en) * 1981-07-09 1983-11-08 Mitsubishi Denki Kabushiki Kaisha Elevator panel
US5535912A (en) * 1994-03-17 1996-07-16 A. O. Smith Corporation Metal liner for a fiber-reinforced plastic tank
US10914527B2 (en) 2006-01-23 2021-02-09 Arvos Gmbh Tube bundle heat exchanger
US20100310832A1 (en) * 2006-07-24 2010-12-09 Tessellated Group, Llc Three dimensional support structure
US7762938B2 (en) * 2006-07-24 2010-07-27 Tessellated Group, Llc Three-dimensional support structure
US8192341B2 (en) 2006-07-24 2012-06-05 Tessellated Group, Llc Pallet and three-dimensional support structure
US8585565B2 (en) 2006-07-24 2013-11-19 Tessellated Group, Llc Method for forming three-dimensional support structure
US20080020188A1 (en) * 2006-07-24 2008-01-24 Tessellated Group Three-dimensional support structure
US10982908B2 (en) 2009-05-08 2021-04-20 Arvos Ljungstrom Llc Heat transfer sheet for rotary regenerative heat exchanger
US10197337B2 (en) 2009-05-08 2019-02-05 Arvos Ljungstrom Llc Heat transfer sheet for rotary regenerative heat exchanger
US20110042035A1 (en) * 2009-08-19 2011-02-24 Alstom Technology Ltd Heat transfer element for a rotary regenerative heat exchanger
US8622115B2 (en) * 2009-08-19 2014-01-07 Alstom Technology Ltd Heat transfer element for a rotary regenerative heat exchanger
US9448015B2 (en) 2009-08-19 2016-09-20 Arvos Technology Limited Heat transfer element for a rotary regenerative heat exchanger
US10378829B2 (en) 2012-08-23 2019-08-13 Arvos Ljungstrom Llc Heat transfer assembly for rotary regenerative preheater
US11092387B2 (en) 2012-08-23 2021-08-17 Arvos Ljungstrom Llc Heat transfer assembly for rotary regenerative preheater
US10175006B2 (en) 2013-11-25 2019-01-08 Arvos Ljungstrom Llc Heat transfer elements for a closed channel rotary regenerative air preheater
US10094626B2 (en) 2015-10-07 2018-10-09 Arvos Ljungstrom Llc Alternating notch configuration for spacing heat transfer sheets

Similar Documents

Publication Publication Date Title
US2796157A (en) Structural panel construction
US1645060A (en) Truss construction
US2160677A (en) Reinforced corrugated sheet
US2221309A (en) Insulating element
US2699599A (en) Structural sheet
US2891491A (en) Building unit
US4020205A (en) Structural cores
DE6944385U (en) TUBULAR REINFORCEMENT BODY.
US3642566A (en) Quasi-isotropic sandwich core
US3527664A (en) Membrane structural module having double ruled quadric surfaces
US1955833A (en) Building material
US1942989A (en) Heat insulating product
US2772757A (en) Structural material
SE437391B (en) PROCEDURE FOR MANUFACTURE OF TREE RULE
US3340023A (en) Cellular structure
EP0797486B1 (en) Grid, in particular flat grid (grating)
US2774386A (en) Profile element for harness frames
US1104475A (en) Metal fabric.
US2336835A (en) Glass run guide
US930350A (en) Expanded-metal fabric.
US3076302A (en) Laminated filter
US3815733A (en) Construction unit assembly
US1080418A (en) Expanded metal.
US1829285A (en) Counter construction
US1046186A (en) Metal reinforcement for concrete structures.