US1473842A - Structural element - Google Patents

Structural element Download PDF

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Publication number
US1473842A
US1473842A US244196A US24419618A US1473842A US 1473842 A US1473842 A US 1473842A US 244196 A US244196 A US 244196A US 24419618 A US24419618 A US 24419618A US 1473842 A US1473842 A US 1473842A
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Prior art keywords
mold
structural element
structural elements
impregnated
elements
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US244196A
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Louis T Frederick
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CBS Corp
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Westinghouse Electric and Manufacturing Co
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Priority to US244196A priority Critical patent/US1473842A/en
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    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/28Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces of materials not covered by groups E04C3/04 - E04C3/20

Description

L. T. FREDERICK Filed July l0, 1918 Nov. 13 1923.
` a M my ma m W 6 9 u f 4%/ www f f mf N/// @ffm A@ wm/Hw. Uw/m a? Patented Nov. 13, 1923.
UNITED STATES LOUIS T. FREDERICK, 0F WILKINSBURG,
PENNSYLVANIA. ASSIGNOR TO WESTING- HOUSE ELECTRIC & MANUFACTURING COMPANY, A CORPORATION 0F PENNSYL- VANIA..
STRUCTURAL ELEMENT.
Application led July 10, 1918. Serial No. 244,196.
To all whom it may concern:
Be it known that I, Louis T. FREDERICK, a citizen of the United States, and a resident of Wilkinsbur inthe county of Allegheny and State of ennsylvania, have invented a new and nseful Improvement in Structural Elements, of which the following is a speciiication. l
My invention relates to structural elements, and it has for its primary object the construction of structural elements, composed of impregnated fibrous material, by a method which will insure a strong and uniform product.
Structural elements, such as I-beams, T- beams and the like, consisting of impregnated sheet material molded to compact and harden the material, are lighter in weight than metal as well as being mechanically strong and are unaffected by temperature changes and by oils and weak acids. For lthis reason, one object of'my invention is to construct beams of the above described character which may be utilized in airplane con struction.'
Another object of my invention is to provide structural elements which will be noninflammable and which will offer great resistance to bullet penetration.
A still further object of my invention is to construct structural elements having reinforcing portions formed integrally with the structural elements, at desired places.
With these and other objects in view, my invention will be more fully described, illustrated in the drawings, in the several views of which corresponding numerals indicate like parts, and then particularly pointed out in the appended claims.
In the drawings, Figs. 1 to 4 inclusive are end views of various structural elements, illustrating diagrammatically the disposition of the material employed in their construction, the laminated structural feature being greatly exaggerated to bring out more clearly the method of formino' the structural elements. Fig. 5 is a side e ovation, parts being broken away, of an I-beam embodying my invention, showing the I-beam with reinforced portions; Fig. 6 is a fragmentary plan view of the beam shown in Fig. 5; Fig.
is a sectional view, taken on the line VII-VII of Fig. 6, of the reinforced I- beam enclosed in a mold, embodying my invention, which is also shown in a similar section; Fig. 8 is a vertical sectional view of a mold embodying'my invention and a T-beam also in section enclosed therein; Fig. 9 is a view similar to Fig. 8 showing a slightly modified form of a mold embodying my invention adapted to mold U-beams formed as hereinafter described.
In practising my invention, I employ impregnated sheets of material which may be properly shaped to preform the structural element of which they are to be a part. The impregnated sheet material, after being formed and stacked in a suitable manner, is surrounded by the pressure members of the mold and subjected to heat and pressure in the mold to compact the preformed material and harden the binder, the manner of shaping and stacking the material depending upon thenature of the structural element desired. It is necessary, however, to determine the thickness of the stacked material required before subjecting it to pressure and heat in order to have the necessary thickness of material when it is compacted. Structural elements which are to be pierced or drilled at certain portions to provide open ings for bolts or the like may be reinforced at these portions by placing a predetermined amount of material at these places after the structural element has been otherwise completel assembled. When the structural element iaving such additional material at certain portions is subjected to pressure and heat in the mold, the material thus added will be molded integrally with the other material employed in forming the main part of the structure.
In Fig. 1 is shown an I-beam preformed reparatory to molding, the web being ormed by placing layers of impregnated sheet material bent to form channel or U- shaped elements l back to back so that their flanges 2 extend in opposite directions. Flat longitudinal strips 3 of the same material may be stacked against the oppostely extending flanges 2 to thicken and strengthen them.
The I-beam shown in Fig. 2 is preformed in substantially the same manner and its web 4 may be thickened by inter osing strips 5, of the same material as is used in forming its U-shaped elements 1. between the U- or channel-shaped elements 1.
The T-beam shown in Fig. 3. may be formed by placing layers of impregnated `lclamping plate 20, a bottom sheet material bent to form L-shaped elements 6 so that the engaging portion 7 forni the stem and the oppositely extending portions 8 form the head. lIhe head may be thickened and strengthened by stacking tlat strips 9 upon it, as in performing the I- beams. The stem may also be thiclnieed by interposing strips 10 between the L-shapcd elements. The channel or U-beam 11 shown in Fig. :t may be formed by stacking a plurality of sheets of treated material bent into proper form.
The material which may be employed in the construction of structural elements in accordance with my invention may be a fibrous sheet material, such as paper, duck or muslin, impregnated with a suitable binder, such as a phenolic condensation product. The sheet material so impregnated will have sufficient rigidity of form to permit shaping the sheets in order that they may be stacked to the form of the structural element desired.
In Figs. 5 and 6 is shown an I-beam 12 embodying my invention which has reinforcing portions 13 in the regions where it may be necessary to employ bolts 14. The reinforcing portions 13 may be inserts of stacked sheet material, of the same nature as that forming the rest of the structure, cut so that they may be put in place and molded integrally with the beam. The reinforcing por tions 13 are shown as employed with an I- beam but they may also be inserted in any structural element, regardless of its shape.
The mold 15 shown in Fig. 7 is adapted to mold I-beams which embody my invention, in such manner that the pressure may be exerted from all four sides, thus assuring a uniform structure. The section of the I- beam in the mold is taken in such a manner as to show the reinforcing insert 13 at one side of the beam but not at the other, the splits 16 and 17 of this mold having offsets in those regions where it is desirable to add the renforcin material. Inmoldin an I- beam, the pre ormed structure may e disposed between splits 16 and 17, which have suitable recesses to receive the reinforcin portions 13 and the preformed structure and splits may then be slipped between the side plates 18 and 19, of the mold 15, which rest upon, and are held in place by, the bottom ormin plate 21 being previously disposed upon t e bottom clamping plate 20. The splits 16 and 17 and the top forming plate 22 may then be pressed down betweenthe side plates 18 and 19 sufficiently to allow a top clamping plate 23 to,he Jositioned with its flanges engaging the si e plates 18 and 19. Pressure may then be exerted against the top plate 23 to force the inner mold sections into their final positions, as shown in Fi 7.
'Ihe mold 24 shown in Fig. 8 may be employed for molding' T-beams and differs from the mold above described in that the splits 25 and 26 are so shaped that the bottom forming plate 21 is unnecessary. The molding operation may be performed in the same manner as for an I-beam. The mold 27 shown in Fig. 9 differs from the mold shown in Fig. 7 only in the shape of the splits 28 and 29, the bottom forming plate 2l being necessary in this case.
Heat may be applied during the molding operation or after the pressure members have been forced into their final positions, as seems most desirable. Although I have indicated and described the construction of structural elements by employing impregnated sheet material, 1t is obvious tliatmaterial other than sheet materia] may be employed. The performing operation is not necessary but facilitates the placing of the material in the mold previous to the application of pressure.
Although I have specifically described and illustrated several modifications of my method and of the apparatus for `forming structural elements, it is obvious that minor changes may be made both in the material and treatment thereof and in the shape of the mold elements I desire, therefore, that no limitations shall be imposed except such as are indicated in the appended claims.
I claim as my invention: I
1. In I-beam, U-beam,` T-beam or the like comprising a fibrous sheet material impregnated with a hardened phenolic condensation product as a binder.
2. A structural element comprisin an impregnated material molded integra y with reinforcing portions of similar materlal disposed at intervals along'the structural element.
In testimony whereof, I have hereunto subcribed my name this 22nd day of June, '191 LOUIS T. FREDERICK.
Certiicate of Correction.
It is hereb certified that in Letters Patent No. 1,473,842, granted November 13, 1923, upont e application of Louis T. Frederick, of Vl'lkinsburg, Pennsylvania` for an improvement in Structural Elements, an error appears in the printed specification requrin correction as follows: Page 2, line 99, claim 1, for the word In read A molde and that the said Letters Patent should be read with this correction therein that the same may conform to the record of the case in the Patent Oce.
Signed and sealed this 92d day of January. A. 1)., 1924.
[mn] KARL FENNING,
.10M-ng l 'om-mixxz'om'r of Palams.
US244196A 1918-07-10 1918-07-10 Structural element Expired - Lifetime US1473842A (en)

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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2439115A (en) * 1944-09-02 1948-04-06 Viviano Salvatore Support for drying paste products
US2441548A (en) * 1945-06-07 1948-05-11 Baker Mcmillen Co Mold
US2445290A (en) * 1940-12-24 1948-07-13 Holoplast Ltd Hollow cavitied bodies such as rigid hollow panel structures and method of making the same
US2493255A (en) * 1943-11-08 1950-01-03 Victor Mfg & Gasket Co Fluid seal
US2519036A (en) * 1943-08-11 1950-08-15 Ford Motor Co Method of molding cellular articles
US2542859A (en) * 1945-06-06 1951-02-20 Clements Macmillan Building construction
US2578781A (en) * 1945-01-18 1951-12-18 Brundige Roy Samuel Manufacture of plywood
US2740332A (en) * 1954-07-14 1956-04-03 Appleton Wood Products Co Suction box cover
DE1139703B (en) * 1959-10-15 1962-11-15 Boelkow Entwicklungen Kg Rod-shaped spring element made of glass fiber reinforced plastic
US3238690A (en) * 1960-03-11 1966-03-08 Reinforced Plastic Container C Composite beam
WO1997010394A3 (en) * 1995-09-01 1997-03-20 Juergen Sager Support member in the form of a hollow section for use in construction
US5639535A (en) * 1996-06-06 1997-06-17 The Boeing Company Composite interleaving for composite interfaces
US6391246B2 (en) * 1996-11-15 2002-05-21 Honda Giken Kogyo Kabushiki Kaisha Method for forming fiber-reinforced composite member
WO2017202836A1 (en) * 2016-05-24 2017-11-30 Wood Tube Sweden Ab Studs of lined papers for non-supporting walls
US20220080624A1 (en) * 2019-05-31 2022-03-17 Airbus Operations Gmbh Device and method

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2445290A (en) * 1940-12-24 1948-07-13 Holoplast Ltd Hollow cavitied bodies such as rigid hollow panel structures and method of making the same
US2519036A (en) * 1943-08-11 1950-08-15 Ford Motor Co Method of molding cellular articles
US2493255A (en) * 1943-11-08 1950-01-03 Victor Mfg & Gasket Co Fluid seal
US2439115A (en) * 1944-09-02 1948-04-06 Viviano Salvatore Support for drying paste products
US2578781A (en) * 1945-01-18 1951-12-18 Brundige Roy Samuel Manufacture of plywood
US2542859A (en) * 1945-06-06 1951-02-20 Clements Macmillan Building construction
US2441548A (en) * 1945-06-07 1948-05-11 Baker Mcmillen Co Mold
US2740332A (en) * 1954-07-14 1956-04-03 Appleton Wood Products Co Suction box cover
DE1139703B (en) * 1959-10-15 1962-11-15 Boelkow Entwicklungen Kg Rod-shaped spring element made of glass fiber reinforced plastic
US3238690A (en) * 1960-03-11 1966-03-08 Reinforced Plastic Container C Composite beam
WO1997010394A3 (en) * 1995-09-01 1997-03-20 Juergen Sager Support member in the form of a hollow section for use in construction
WO1997010394A2 (en) * 1995-09-01 1997-03-20 Sager Juergen Support member in the form of a hollow section for use in construction
US5639535A (en) * 1996-06-06 1997-06-17 The Boeing Company Composite interleaving for composite interfaces
US6391246B2 (en) * 1996-11-15 2002-05-21 Honda Giken Kogyo Kabushiki Kaisha Method for forming fiber-reinforced composite member
WO2017202836A1 (en) * 2016-05-24 2017-11-30 Wood Tube Sweden Ab Studs of lined papers for non-supporting walls
SE541248C2 (en) * 2016-05-24 2019-05-14 Wood Tube Sweden Ab Rule of wrapped paper for non-load-bearing walls, rule with fastening device and method
US20220080624A1 (en) * 2019-05-31 2022-03-17 Airbus Operations Gmbh Device and method
US11780120B2 (en) * 2019-05-31 2023-10-10 Airbus Operations Gmbh Device and method

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