US1349372A - Method of making hollow bodies - Google Patents

Method of making hollow bodies Download PDF

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US1349372A
US1349372A US1349372DA US1349372A US 1349372 A US1349372 A US 1349372A US 1349372D A US1349372D A US 1349372DA US 1349372 A US1349372 A US 1349372A
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metal
core
fibrous material
hollow bodies
binder
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00Subject matter not provided for in other groups of this subclass
    • B29D99/0025Producing blades or the like, e.g. blades for turbines, propellers, or wings
    • B29D99/0028Producing blades or the like, e.g. blades for turbines, propellers, or wings hollow blades
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C33/00Moulds or cores; Details thereof or accessories therefor
    • B29C33/44Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
    • B29C33/52Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles soluble or fusible
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/44Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/446Moulding structures having an axis of symmetry or at least one channel, e.g. tubular structures, frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/86Incorporated in coherent impregnated reinforcing layers, e.g. by winding
    • B29C70/865Incorporated in coherent impregnated reinforcing layers, e.g. by winding completely encapsulated
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C43/00Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
    • B29C43/02Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
    • B29C43/10Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
    • B29C43/12Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies using bags surrounding the moulding material or using membranes contacting the moulding material

Definitions

  • My invention relates to hollow bodies and more particularly to hollow bodies comprising superimposed layers of fibrous material impregnated with a binder adapted to harden under heat and pressure.
  • The'primary object of my invention is to provide a method by which such bodies may be formed.
  • fibrous material impregnated with a hardened phenolic condensation product is unaffected by moisture, oils, weak acids and alkalis while most metals are materially affected by them.
  • One object of my invention resides. therefore, in reinforcing a hollow body of fibrous ma terial with a metal in such manner that the impregnated fibrous material will protect the metal against corrosion while the metal will supplement the mechanical strength of the fibrous material.
  • a still. further object of my invention is to provide hollow bodies of fibrous material impregnated with a hardened binder and reinforce them with a metal which may be utilized in protecting the fibrous material during the process of forming the body.
  • the metal electro-deposited on the core may be of any desired thickness which may be readily controlled during the deposition.
  • ner may then have superimposed upon it layers of fibrous material impregnated with a suitable binder, after which the body thus assembled may be disposed in a suitable mold and subjected to heat and pressure.
  • the amount of heat employed may be sufficient to not only fuse the inner core but also to harden the binder with which the fibrous material is impregnated and the pressure may be applied simultaneously with the heat to compact the fibrous material.
  • the molten core maybe drained from the body, leaving the electro-deposited casing within the hollow body of fibrous material.
  • Fig. 1 a container 1 composed of layers of fibrous material, such as paper, muslin or duck impregnated with a suitable binder, such as a phenolic condensations.
  • the fusible core 2 is preferably given the outline of the article which it is desired to make, after which the core 2 may have deposited thereon, electrolytically, a metal 8 of higher fusing point and greater mechanical strength.
  • the electro-deposited metal may be brass or any such metal having qualities similar to. brass, the metal employed being governed, to a certain extent,
  • the core 2, having the electro-(leposited casing 3 may then have superimposed thereon the layers of fibrous material, impreging-point metal may be formed.
  • the mold 4 is preferably provided with an inlet pipe 6 which some additional molten metal may be forced to help fuse the inner core.
  • the pipe 6 may also be employed to drain the fused core from the body after it has been completely formed.
  • a small amount of molten metal may be forced into the pipe 6 while pressure is being maintained on the mold to help fuse the core 2 to facilitate its being drained from the container when the fibrous mate rial has been sufficiently compacted and the binder, with which it is impregnated, has been hardened.
  • the electrodeposited casing 3 being of a higher-fusingpoint metal, remains in a solid condition and, therefore, is left in its original position within the superimposed layers of fibrous material. after the fused core has been drained therefrom.
  • the casing of higher fusingpoint metal which engages the fibrous material protects the latter against any injurious effects of the molten metal which would otherwise engage it.
  • the high-fusing-point casing supple ments the mechanical strength of the fibrous material in the finished body.
  • a propeller which may be constructed by following the method above set forth. Exactly the same manner of forming the fusible core which, of course, in this instance would be a different shape, is followed.
  • a mold 7 is shown in which a hollow propeller 8 of fibrous mate rial having an inner casing 9 of high-fun
  • a fusible core 10 may be of any suitable material, such as above mentioned.
  • the mold 7 will, of course, be provided with a suitable means for draining the fusible core 10 from the molded body, this means of draining not being shown in the drawing.
  • ⁇ Vhen forming a propeller by this method, the fusible the propeller which, bein midway between the extending blades, 0 ers the most convenient point of withdrawal of the fused core.
  • a method of making hollow bodies that comprises superimposing layers of sheet material impregnated with a binder about a core including a metal having a low fusing point and a metal having a relatively high fusing point, applying heat and pressure to the body in a mold and removing the low fusing-point metal.
  • a method of making hollow bodies that comprises super-imposing layers of sheet material impregnated with a binder about a core including a metal having a low fusing point inclosed by a metal covering having a relatively high fusing point, disposing the body in a suitable mold, applying heat to fuse the core and to harden the binder, applying pressure to compact the sheet material simultaneously with the application of heat and removing the fused core from the body after the binder has been hardened.
  • a method of making hollow bodies that comprises forming a core of a relatively low-fusing-point metal, electro-depositing thereon a metal having a comparatively high fusing point, superimposing layers of sheet material impregnated with a binder on the core, disposing the assembled body in a suitable mold, applying heat and pressure to compact the fibrous material and to harden the binder and to fuse the low-fusing-point metal and removing the fused metal from the body.
  • a method of making hollow bodies that comprises forming a core, having the outline of the article desired of a relatively low-fusing-point metal, electro-depositing thereon a metal having a relatively high fusing point, superimposing layers of sheet point metal and removing the fused metal material impregnated With a phenolic contherefrom.

Description

W. F. EGAN.
. METHOD OF MAKING HOLLOW BODIES.
APPLICATION FILED FEB. 15. I919.
Patented Aug. 10,1920.
INVENTOR VII/709m f'f afl.
' WITNESSES:
ATTORNEY UNITED STATES PATENT OFFICE.
WILLIAM E EGAN, OF WILKINSBURG, PENNSYLVANIA, ASSIGNOR T0 WESTINGHOUSE ELECTRIC & MANUFACTURING COMPANY, A CORPORATION OF PENNSYLVANIA.
METHOD OF MAKING HOLLOW BODIES.
Specification of Letters Patent.
Patented Aug. 1c, 1920.
Application filed February 15, 1919. Serial No. 277,218.
To all whom it may concern:
Be it known that I, WILLIAM F. EGAN, a citizen of the United States, and a resident of Wilkinsburg, in the county of Allegheny and State of Pennsylvania, have invented a new and usefullmprovement in Methods of Making Hollow Bodies, of which the following is a specification.
My invention relates to hollow bodies and more particularly to hollow bodies comprising superimposed layers of fibrous material impregnated with a binder adapted to harden under heat and pressure. The'primary object of my invention is to provide a method by which such bodies may be formed.
My invention has particular relation to bodies formed of fibrous sheet material impregnated with a binder such as a phenolic condensation product. It is sometimes desirable to construct hollow bodies composed of such material and to reinforce them by means of a suitable metal. While the metal possesses some advantageous features which may supplement those possessed by a fibrous material, impregnated with a phenolic condensation product, it is desirable that these materials be combined in such manner that the advantageous qualities of both materials be retained. a
It is well known that fibrous material impregnated with a hardened phenolic condensation product is unaffected by moisture, oils, weak acids and alkalis while most metals are materially affected by them. One object of my invention resides. therefore, in reinforcing a hollow body of fibrous ma terial with a metal in such manner that the impregnated fibrous material will protect the metal against corrosion while the metal will supplement the mechanical strength of the fibrous material.
A still. further object of my invention is to provide hollow bodies of fibrous material impregnated with a hardened binder and reinforce them with a metal which may be utilized in protecting the fibrous material during the process of forming the body.
With these andother objects in view, my invention will be more fully described. illustrated in the drawings, in the several views of which corresponding numerals in dicate like parts, and then particularly pointed out in the claims.
sectional view of a mold and a container on, electrolytically, a metal of higher fusing point and relatively great mechanical strength. The metal electro-deposited on the core may be of any desired thickness which may be readily controlled during the deposition. A fusible core incased with a metal of higher fusing point, in this man-.
ner, may then have superimposed upon it layers of fibrous material impregnated with a suitable binder, after which the body thus assembled may be disposed in a suitable mold and subjected to heat and pressure. The amount of heat employed may be sufficient to not only fuse the inner core but also to harden the binder with which the fibrous material is impregnated and the pressure may be applied simultaneously with the heat to compact the fibrous material. After the layers of fibrous material have been sufficiently compacted and the binder has been hardened. the molten core maybe drained from the body, leaving the electro-deposited casing within the hollow body of fibrous material.
In Fig. 1 is shown a container 1 composed of layers of fibrous material, such as paper, muslin or duck impregnated with a suitable binder, such as a phenolic condensations. The fusible core 2 is preferably given the outline of the article which it is desired to make, after which the core 2 may have deposited thereon, electrolytically, a metal 8 of higher fusing point and greater mechanical strength. The electro-deposited metal may be brass or any such metal having qualities similar to. brass, the metal employed being governed, to a certain extent,
by the nature of the article to be formed about it.
The core 2, having the electro-(leposited casing 3, may then have superimposed thereon the layers of fibrous material, impreging-point metal may be formed.
' through nated with a phenolic condensation product, to form a container 1. and the assembled body, disposed in a suitable mold 4 having heating ducts 5 through which steam may be passed to heat the mold. However, the manner of heating the mold and the particular mold employed forms no part of my invention. In this instance, the mold 4 is preferably provided with an inlet pipe 6 which some additional molten metal may be forced to help fuse the inner core. The pipe 6 may also be employed to drain the fused core from the body after it has been completely formed. After the body or container 1, with the core 2, has been placed in the mold 4, heat may be applied to fuse the core 4 and to harden the binder with which the fibrous material is impregnated, pressure being applied, simultaneously with the heat, to compact the fibrous material.
A small amount of molten metal may be forced into the pipe 6 while pressure is being maintained on the mold to help fuse the core 2 to facilitate its being drained from the container when the fibrous mate rial has been sufficiently compacted and the binder, with which it is impregnated, has been hardened. When the fused core 2 is drained from the container 1, the electrodeposited casing 3, being of a higher-fusingpoint metal, remains in a solid condition and, therefore, is left in its original position within the superimposed layers of fibrous material. after the fused core has been drained therefrom. The casing of higher fusingpoint metal which engages the fibrous material protects the latter against any injurious effects of the molten metal which would otherwise engage it. Furthermore, the high-fusing-point casing supple ments the mechanical strength of the fibrous material in the finished body.
In Fig. 2 is shown a propeller which may be constructed by following the method above set forth. Exactly the same manner of forming the fusible core which, of course, in this instance would be a different shape, is followed. In Fig. 3 a mold 7 is shown in which a hollow propeller 8 of fibrous mate rial having an inner casing 9 of high-fun A fusible core 10 may be of any suitable material, such as above mentioned. The mold 7 will, of course, be provided with a suitable means for draining the fusible core 10 from the molded body, this means of draining not being shown in the drawing. \Vhen forming a propeller by this method, the fusible the propeller which, bein midway between the extending blades, 0 ers the most convenient point of withdrawal of the fused core.
Although I' have described a method and a plurality of bodies which may be formed in accordance with my invention, it is obvious that, by slightly different methods, various articles, comprising superimposed layers of fibrous material impregnated With a hardened binder having a lining of metal, may be formed within the scope of my invention and I desire, therefore, that no limitations shall be imposed except such as are indicated in the appended claims.
I claim as my invention:
1. A method of making hollow bodies that comprises superimposing layers of sheet material impregnated with a binder about a core including a metal having a low fusing point and a metal having a relatively high fusing point, applying heat and pressure to the body in a mold and removing the low fusing-point metal.
2. A method of making hollow bodies that comprises superimposing layers of sheet material impregnated with a binder about a core including a metal having a low fusing point inclosed by a metal covering having a relatively high fusing point, applying heat and pressure to the body in a mold and removing the metal having a low fusing point.
3. A method of making hollow bodies that comprises super-imposing layers of sheet material impregnated with a binder about a core including a metal having a low fusing point inclosed by a metal covering having a relatively high fusing point, disposing the body in a suitable mold, applying heat to fuse the core and to harden the binder, applying pressure to compact the sheet material simultaneously with the application of heat and removing the fused core from the body after the binder has been hardened.
4. A method of making hollow bodies that comprises forming a core of a relatively low-fusing-point metal, electro-depositing thereon a metal having a comparatively high fusing point, superimposing layers of sheet material impregnated with a binder on the core, disposing the assembled body in a suitable mold, applying heat and pressure to compact the fibrous material and to harden the binder and to fuse the low-fusing-point metal and removing the fused metal from the body.
5. A method of making hollow bodies that comprises forming a core, having the outline of the article desired of a relatively low-fusing-point metal, electro-depositing thereon a metal having a relatively high fusing point, superimposing layers of sheet point metal and removing the fused metal material impregnated With a phenolic contherefrom. I
densation product on the core, disposing the In testimony whereof I have hereunto 10 assembled body in a suitable mold, applying subscribed my name this 31st day of J an, heat and pressure to compact the fibrous 1919.
material and to harden the phenolic condensation product and to fuse the low-fusing- WILLIAM F. EGAN.
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4248817A (en) * 1976-03-04 1981-02-03 Karl Frank Method for the manufacture of workpieces in particular fan blades, complete fan rotors and other bodies
WO1987001650A1 (en) * 1985-09-24 1987-03-26 Grumman Aerospace Corporation Method for forming corrugated materials using memory metal alloy cores
US4683099A (en) * 1985-04-02 1987-07-28 Rolls-Royce Plc Moulding of composite materials
US5853651A (en) * 1995-09-07 1998-12-29 Simula, Inc. High pressure hollow process for manufacturing composite structures

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4248817A (en) * 1976-03-04 1981-02-03 Karl Frank Method for the manufacture of workpieces in particular fan blades, complete fan rotors and other bodies
US4683099A (en) * 1985-04-02 1987-07-28 Rolls-Royce Plc Moulding of composite materials
WO1987001650A1 (en) * 1985-09-24 1987-03-26 Grumman Aerospace Corporation Method for forming corrugated materials using memory metal alloy cores
US4675061A (en) * 1985-09-24 1987-06-23 Grumman Aerospace Corporation Method for forming corrugated materials using memory metal cores
US5853651A (en) * 1995-09-07 1998-12-29 Simula, Inc. High pressure hollow process for manufacturing composite structures

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