US2779303A - Ship hull bottom plating having integral bent back reinforcement - Google Patents
Ship hull bottom plating having integral bent back reinforcement Download PDFInfo
- Publication number
- US2779303A US2779303A US184796A US18479650A US2779303A US 2779303 A US2779303 A US 2779303A US 184796 A US184796 A US 184796A US 18479650 A US18479650 A US 18479650A US 2779303 A US2779303 A US 2779303A
- Authority
- US
- United States
- Prior art keywords
- plate
- sections
- structural
- integral
- plating
- 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
Links
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING
- B63B3/00—Hulls characterised by their structure or component parts
- B63B3/14—Hull parts
- B63B3/16—Shells
Definitions
- This invention pertains to a new and useful improvement in the manufacture and production of structural shapes and it is an object or" thisinvention to provide structural shapes fabricated in accordance with this invention which may be used in lieu of the currently employed standard rolled shapes, or may be employed as a structural shape forming an integral part of a plate used in construction work, and in particular where structural shapes are employed in conjunction with metallic flat plates or sheets. i The invention also pertains to providing a series of sections supplementary to rolled sections now in use.
- the expression formed sections will be used for structural shapes, made in accordance with the invention, in contradistinction to the standard structural rolled shapes.
- integral reinforcements will be used throughout the specification where the stiffening members of a structure, now commonly secured to the plating either by riveting or by welding, can be formed as an integral part of the plating itself, thus eliminating the extra weight due to riveting, or the extra weight of welding metal, either or both or which means may be used for the conformal securing of the plate to the structural shape.
- one example of a specific application will be in the construction of ships which will have at least a two-fold purpose, namely, in that in the construction of ships employing partially prefabricated sections, one or more struc tural shapes which may be alike or dissimilar, can be preformed as an integral part of the flat plate or sheet all of which can be handled at the forming mill where adequate facilities are available instead of trying to use make shift methods at the location of assembly of the ships.
- Fig. '1 is an athwartship elevation of a symmetrical half otl'a" transverse bulkhead of a representative vessel looking aft.
- Fig. 2 is a representative section of a conventional welded method of double welding a vertical to a horizontal structural member.
- Fig. '3 shows the method employed in the present invention for reproducing a condition similar to that shown in the conventional method shown in Fig. 2.
- Fig. 4 is an enlarged view of the section outlined in Fig. 1, indicated by the character X, according to conventional methods.
- FIG. 5 is an enlarged view of a section outlined in Fig. 1, indicated by the character X, according to the present invention employing integral reinforcements.
- Fig. 6 shows the method of securing the transverse bulkhead. to the bottom shell plating.
- Fig. 7 is. an isolated view of the bottom shell plating shown in Fig. 6.
- Fig. 8 is an isolated view of the transverse bulkhead shown in Fig. 6.
- Fig. 9 is a view showing a representative method of groove forming in a plate preparatory to bending.
- Fig. 10 shows a representative method of multiple grooving a plate.
- Fig. 12. shows the plate presented in Fig. 11 after "the 180., bending operation is completed.
- Fig. 13 is a plate grooved for double 180 bends.
- Figure 14 is the plate shown in Fig. 13 with one of the bends formed at a groove.
- Fig. 15v is the plate shown in Fig. 13 with both of the bends completed.
- FIG. 1 a representative athwartship elevation of a symmetrical half of a transverse bulkhead of, a representative vessel looking aft wherein the ship 50 has a shell 51 with a longitudinal bulkhead 52 positioned in the. ship.
- Figs. 4 and are comparative sections, respectively, of the conventional method and the method in accordance with the invention as outlined by the area X of Fig. 1.
- the longitudinal bulkhead 52 welded to the bottom shell plating 53 alongside a longitudinal stiltener 5.4..and. a girder 55. all ofwhich are secured to the bottom shell plating '53 by welds 56.
- a comparative structure set up in Fig. 5 shows that the girder portion 57 and the stiffener portion 58- are formed as an integral reinforcement and are part of the bottom shell plating 59.
- FIGs, 2 and 3 are fragmentary comparative representations, reSPQctively, of the conventional welded method of double welding a verticalto a horizontal structural member with the similar condition produced in conjunction with the teaching of the. present invention wherein portionsfifland 61abut each other, thereby eliminating the, doublewelds shown at. 5 6. in Fig. 2.
- the joining seam maybe caulked, to prevent corrosion, shown as 98' inFig. 3.
- Figs. 6, 7-, and 8 show the transverse bulkhead 63 having a notch or slot 64 formed therein so that said transverse bulkhead slot may be fitted into the slot 65 formed in the integral reinforcement bottom shell plat ing 66, with, the slot 65 being formedthe full width of the flgnge 6,7 and partially in the web 68 so that the edge (ifimay come flush on the inner surface of the bottorn. shellplating 70sinee the open'corners where the slot 64' engages the edge 6'9 are rounded to fit the curved area 71 of the bottom shell plating.
- Figs. 11 to 15 inclusive there is shown the progressive "steps in making'the formed sections and integral Cit reinforcements whereby longitudinal grooves such as 72 are formed on either one or both sides of the plate, in separate steps, or in compound operation depending on the necessary requirements of the particular formed section or integral reinforcements in process of fabrication.
- Opposing rollers 73 may be rotatably mounted in the groove forming machine with the groove roller 74 having a pre-shaped annular flange 75, as part thereof, to form a groove 72.
- the plate 76 may have the area to be grooved preheated, or the plate 76 may be rolled cold depending on the dimensions and physical properties of the plate 76
- a bend may be formed in a plate as shown in Fig. 11, resulting from the groove being formed in the plate 102 of Fig. 10. The reduction of metal by the grooving process, whether the groove be formed by rolling as shown in Fig.
- the radius of the semi-circular area removed from the plate before bending be as small as possible and still permit the desired result. Since the neutral axis of the plate lies somewhere within the inner halfthickness of the material, the radius of the semi-circular section should not exceed one-half of this half-thickness. face to the neutral axis then all of the fibers subjected to, the forces of compression in the critical area will have been removed in the process and the intended purpose will have been entirely exceeded. In conclusion, then, the radius of groove 72 should in no case be greater than 25% of the thickness of the plate.
- Figs. 13 and 14 are representative of progressive steps in forming opposing 180 bends in a plate 79 after the pair of grooves 72 are formed in the plate shown in Fig. 10 by using a dual groove forming roller, or by using a similar groove forming roller with two passes through the grooving machine as set forth in Fig. 9.
- groove forming machine may have any desired number of groove forming portions on a single roller or separate rollers may be provided which may be deposited for the particular section to be formed on either or both sides-
- the bend test specimens for bars and shapcs is quite well standardized and include that the bars and shapes shall stand being bent cold through 180 without crackiing on the outside of the bent portion. material or under it shall be bent back upon itself without cracking while material from to. and includ ing 1 /2" in thicknessshall be bent around a pin thediameter of which is equal to the thickness of thespecirnen. Since the bend test mentioned above refers. to. bending cold the material through 180 without fracture,then,
- steel plate is used as the basis for all calculations contained here the idea is much broader than this and must include other metals and alloys as well as other materials such as plastic products, etc.
- a vessel is in the process of design.
- the naval architects make up their drawings as at present showing welded stiffening members.
- the engineers at the mill can easily substitute for the welded members shown on the drawings suitable and equivalent integral reinforcements.
- the plates are prepared at the mill and shipped to the building site ready for immediately assembly; the only additional requirement being to secure the butt edges of the prepared plates to each other.
- the integral reinforcements may be provided from large plates and may not only include the structural shapes, but may also take advantage of the fact that the plate itself may be curved, angled or bent in any shape or conformation depending on the requirement of the engineer.
- a bottom shell plating having an integral longitudinal-extending structural stiffening portion formed of the plating bent back upon itself interior of the hull and providing vertical abutting surfaces lying in the outer side of the plating, said structural portion being further bent to provide a web and flange running coextensively of the plating, said structural portion having a slot through the flange and extending partially down through the web transversely thereof, and a bulkhead extending transversely through the structural portion and having a slot in its lower edge fitted in said slot in the structural portion and receiving the remainder of the web.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Butt Welding And Welding Of Specific Article (AREA)
Description
Jan. 29, 1957 J. CUPPLES SHIP HULL BOTTOM PLATING HAVING INTEGRAL BENT BACK REINFORCEMENT 2 Sheets-Sheet 1 Filed Sept. 14. 1950 w NW w 50 |L LL Li L I IT INVENTOR JOSEPH GUPPLES Jan. 29, 1957 J. CUPPLES 2,779,303
SHIP HULL BOTTOM FLATING HAVING INTEGRAL ENI BACK REINFORCEMENT Filed Sept. 1%, 1950 2 Sheets-Sheet 2 lNvEN l'OR JOSEPH GUIPPLES ATTORNEY United States Patent SHIP HULL BOTTOM PLATING HAVING INTE- GRAL BENT BACK REINFORCEMENT Joseph Cupples, Brooklyn, N. Y. Application September 14, 1950, Serial No. 184,796 3 (Ilaims. (Cl. 114-79) This invention pertains to a new and useful improvement in the manufacture and production of structural shapes and it is an object or" thisinvention to provide structural shapes fabricated in accordance with this invention which may be used in lieu of the currently employed standard rolled shapes, or may be employed as a structural shape forming an integral part of a plate used in construction work, and in particular where structural shapes are employed in conjunction with metallic flat plates or sheets. i The invention also pertains to providing a series of sections supplementary to rolled sections now in use.
Throughout the invention the expression formed sections will be used for structural shapes, made in accordance with the invention, in contradistinction to the standard structural rolled shapes. Further, the expression integral reinforcements will be used throughout the specification where the stiffening members of a structure, now commonly secured to the plating either by riveting or by welding, can be formed as an integral part of the plating itself, thus eliminating the extra weight due to riveting, or the extra weight of welding metal, either or both or which means may be used for the conformal securing of the plate to the structural shape.
.One of the advantages of the invention is that by employing structural shapes as either formed sections, or integral reinforcements, there will be a greater degree of accuracy in the ultimate product since there is a complete elimination of the variations in the thickness of the metal when formed in accordance with the teachings of the present invention.
Among the advantages of the present invention are the following:
.To provide a method for executing a 180 deg. backupon-itself bend in plate structures.
To provide an additional series of sections, supplementary to the rolled structural sections at present in use, and having engineering properties of an intermediate nature, thereby providing a more comprehensive and selective choice for engineers and designers.
To reduce weight in metal structures by either eliminating entirely or reducing considerably the necessity for welding and/ or riveting.
To eliminate the dangers coincident with objectionable stresses which are induced in steel structures by excessive use'of welding.
To eliminate the necessity for stress-relieving in large welded steel structures by reducing the necessity for weldmg.
To facilitate the sub-assembly phase of construction by making reinforcement members integral parts of the structure, thereby saving time and costs during shipping and at final assembly. I I
Engineers employing structural shapes fully recognize that variations indesigning and detailing must be kept in mind when employing conventional rolled structural shapes since, in production of the structural shapes, the
roll passes are modified in the wear of the rolls, and the actual dimensions do not always conform to the theoretical, even in the case of minimum weight sections. By using fiat plates in forming sections any variation in dimensions of the section can be contained within the rolling limits of the plate.
By employng flat plates or sheets of metal in fabricating the formed sections and integral reinforcements, there is no necessity to be concerned with the thickness of the.
metal conforming to the theoretical, since flat plates and sheets are made to conform to a thickness of the plate or sheet. This is different than the conformance which would be necessary, for example, in the thickness of the various cross sectional portions of a rolled shape such as. an I-beam or a channel.
While the present invention will find application in practically every field where structural'shapes are now used, one example of a specific application will be in the construction of ships which will have at least a two-fold purpose, namely, in that in the construction of ships employing partially prefabricated sections, one or more struc tural shapes which may be alike or dissimilar, can be preformed as an integral part of the flat plate or sheet all of which can be handled at the forming mill where adequate facilities are available instead of trying to use make shift methods at the location of assembly of the ships. Further, not only will there be the elimination in engineering over theconcern of variation in dimensions of the structural shape for possible reinforcement, but there will be the desired security obtained by practicing the present invention due to the elimination of the vast tween a light ship and a loaded ship, is the cargo capacity of the vessel. The load-water line is always assigned to a vessel and cannot under any circumstances be exceeded without breaching the safety regulations for vessels at sea. However, the light-load line should be as low as possible in order to leave a maximum volume for cargocarrying capacity. Therefore, whatever is saved in light ship tonnage is gained in cargo tonnage and the economy and profit of this saving is continuously repeated when ever the particular vessel makes a voyage.
By using the present invention with the example of ships, there can be a saving in eliminating the necessity for welding any structural members and a further advantage of elimination of many of the distortions due to stresses within the structure by reason of the intense concentra-' tion of the high temperatures required by arc welding.
It will be seen from the specification by comparison between the teaching of the present invention, and the conventional rolled shapes, that much less time will be required at the steel mill to fabricate the formed sections whether individually or as part of a plate, than would be required at the shipyard to weld a similar member to the plating plus the time required originally at the mill to herein, are cheaper to manufacture, can be produced faster, are stronger in physical properties, and are better suited for welded and riveted construction than the standard rolled sections.
The present showing are preferred embodiments of the invention but it is to be understood that variatiqns,,
Patented Jan. 29, 1957 changes and modifications may be made without departing from the spirit of the appended claims.
In the drawings:
' Fig. '1 is an athwartship elevation of a symmetrical half otl'a" transverse bulkhead of a representative vessel looking aft.
Fig. 2 is a representative section of a conventional welded method of double welding a vertical to a horizontal structural member.
Fig. '3 shows the method employed in the present invention for reproducing a condition similar to that shown in the conventional method shown in Fig. 2.
Fig. 4 is an enlarged view of the section outlined in Fig. 1, indicated by the character X, according to conventional methods. i
.Fig'. 5. is an enlarged view of a section outlined in Fig. 1, indicated by the character X, according to the present invention employing integral reinforcements.
Fig. 6 shows the method of securing the transverse bulkhead. to the bottom shell plating.
Fig. 7, is. an isolated view of the bottom shell plating shown in Fig. 6.
Fig. 8 is an isolated view of the transverse bulkhead shown in Fig. 6.
Fig. 9 is a view showing a representative method of groove forming in a plate preparatory to bending.
-;Fig. 10. shows a representative method of multiple grooving a plate.
Fig. ll-the portion of the plate shown in Fig. 9 after the, groove forming operation is completed.
Fig. 12. shows the plate presented in Fig. 11 after "the 180., bending operation is completed.
Fig. 13 is a plate grooved for double 180 bends.
Figure 14 is the plate shown in Fig. 13 with one of the bends formed at a groove.
Fig. 15v is the plate shown in Fig. 13 with both of the bends completed.
-Referring to the drawings, and more particularly to Fig. 1, there is shown a representative athwartship elevation of a symmetrical half of a transverse bulkhead of, a representative vessel looking aft wherein the ship 50 has a shell 51 with a longitudinal bulkhead 52 positioned in the. ship.
Figs. 4 and are comparative sections, respectively, of the conventional method and the method in accordance with the invention as outlined by the area X of Fig. 1. There is shown the longitudinal bulkhead 52 welded to the bottom shell plating 53 alongside a longitudinal stiltener 5.4..and. a girder 55. all ofwhich are secured to the bottom shell plating '53 by welds 56.
A comparative structure set up in Fig. 5 shows that the girder portion 57 and the stiffener portion 58- are formed as an integral reinforcement and are part of the bottom shell plating 59.
.Figs, 2 and 3, are fragmentary comparative representations, reSPQctively, of the conventional welded method of double welding a verticalto a horizontal structural member with the similar condition produced in conjunction with the teaching of the. present invention wherein portionsfifland 61abut each other, thereby eliminating the, doublewelds shown at. 5 6. in Fig. 2. The joining seam maybe caulked, to prevent corrosion, shown as 98' inFig. 3.
Figs. 6, 7-, and 8 show the transverse bulkhead 63 having a notch or slot 64 formed therein so that said transverse bulkhead slot may be fitted into the slot 65 formed in the integral reinforcement bottom shell plat ing 66, with, the slot 65 being formedthe full width of the flgnge 6,7 and partially in the web 68 so that the edge (ifimay come flush on the inner surface of the bottorn. shellplating 70sinee the open'corners where the slot 64' engages the edge 6'9 are rounded to fit the curved area 71 of the bottom shell plating.
In Figs. 11 to 15 inclusive, there is shown the progressive "steps in making'the formed sections and integral Cit reinforcements whereby longitudinal grooves such as 72 are formed on either one or both sides of the plate, in separate steps, or in compound operation depending on the necessary requirements of the particular formed section or integral reinforcements in process of fabrication.
Opposing rollers 73 may be rotatably mounted in the groove forming machine with the groove roller 74 having a pre-shaped annular flange 75, as part thereof, to form a groove 72. The plate 76 may have the area to be grooved preheated, or the plate 76 may be rolled cold depending on the dimensions and physical properties of the plate 76 By utilizing the grooves 72 as set forth herein, a bend may be formed in a plate as shown in Fig. 11, resulting from the groove being formed in the plate 102 of Fig. 10. The reduction of metal by the grooving process, whether the groove be formed by rolling as shown in Fig. 9, or by a cutter wherein the metal is actually removed rather than deformed, permits the 180 bend to be made by a rolling operation so that the surfaces 77 and 78 may be substantially parallel, which would not be the case if the groove were not formed in the plate or sheet 76.
In order to hold the reduction in area of section through the bending plane to an absolute minimum it is suggested that the radius of the semi-circular area removed from the plate before bending be as small as possible and still permit the desired result. Since the neutral axis of the plate lies somewhere within the inner halfthickness of the material, the radius of the semi-circular section should not exceed one-half of this half-thickness. face to the neutral axis then all of the fibers subjected to, the forces of compression in the critical area will have been removed in the process and the intended purpose will have been entirely exceeded. In conclusion, then, the radius of groove 72 should in no case be greater than 25% of the thickness of the plate.
Figs. 13 and 14 are representative of progressive steps in forming opposing 180 bends in a plate 79 after the pair of grooves 72 are formed in the plate shown in Fig. 10 by using a dual groove forming roller, or by using a similar groove forming roller with two passes through the grooving machine as set forth in Fig. 9.
'It is to be understood that according to the basic teach ing presented in the invention of groove forming to pro vide integral reinforcements and formed sections, the.
groove forming machine may have any desired number of groove forming portions on a single roller or separate rollers may be provided which may be deposited for the particular section to be formed on either or both sides- The bend test specimens for bars and shapcsis quite well standardized and include that the bars and shapes shall stand being bent cold through 180 without crackiing on the outside of the bent portion. material or under it shall be bent back upon itself without cracking while material from to. and includ ing 1 /2" in thicknessshall be bent around a pin thediameter of which is equal to the thickness of thespecirnen. Since the bend test mentioned above refers. to. bending cold the material through 180 without fracture,then,
certainlya preheated plate can be bentback upon itself without any adverse effects.
When a metal is subjected to heat its molecular struc If radius equals the distance from the inner sur,,
Ordinarily for.
ture is thereby rendered sufficiently fluid to permit the shape to be easily altered. Referring to the back upon itself" bend shown in Fig. 12, it may be said that while the fibers on the outside of the bend may be in tension those on the inside will be in compression. The physical interference of these elements coming to bear upon each other can be overcome by removing some of them entirely from the critical area thereby providing space in which other fibers can re-align themselves and thus relieve the induced forces of compression. If a semicircular area of inch radius is removed from one surface of the plate at the bending plane the reduction in area of section will only be 0.025 sq. inch. This is, for material of 1%. thickness, a negligible amount which is of very little importance to the strength of the member. If now the plate is bent back upon itself this open area of 0.025 sq. inch will, theoretically, be distributed throughout a small complete circle of radius equal to 0.09 inch. In effect this provides a circle of approximately 1 of an inch diameter in which the compressed fibers can redistribute themselves and thus relieve the most severe compressive forces.
In view of the foregoing, it will be seen that by following the teachings of the present invention not only is it possible to make formed sections comparable to the conventional rolled sections but that many other derivatives are possible in structural shapes, regardless of whether they are formed sections or integral reinforcements.
There exists at present an enormous capital investment in machinery and methods for manufacturing rolled sections and it is not the intention to wish to eliminate this by substituting formed sections. The intention is rather to supplement rolled sections by offering to industry a form more easily and more economically manufactured from standard flat plates or sheets. This new form contains many advantages in physical properties, as we shall see, and its addition to the list of standard rolled sections will afford a much wider selective choice for engineers and designers.
During the recent war years when precious time and material were being allocated to effect maximum results the office of production management, in the interests of maximum steel mill production and the conservation of available steel supply, suspended the manufacture of many rolled steel sections as being non-essential and wisely diverted the materials to other uses. Formed sections manufactured out of standard rolled plate could have been an ideal substitute in such an emergency.
In longitudinally framed vessels the longitudinal structural members secured to the shell-plating must increase in sectional area as we proceed from the deckedge down past the bilge-turn and along the bottom shell to the docking girder. Present practice is to use standard rolled angle progressively up to 8" x 8" which is the largest size rolled. Where greater sections are required flat plate is cut and bent in a fianging machine to a 90 deg. right angle shape. In short, rolled angle sections are supplemented with flanged plate sections. The intention in these notes is to supplement all rolled sections, I beam, H beams, channels, angles, Ts, bulb angles, Zs, with formed sections.
Although steel plate is used as the basis for all calculations contained here the idea is much broader than this and must include other metals and alloys as well as other materials such as plastic products, etc.
The present-day practice of welded structural members has effected a considerable saving in weight over riveted structural members. The use of integral reinforcements can elfect a further saving by eliminating the necessity for welding many structural members. Not only will the weight of weld metal be saved but a further advantage will be elimination of many of the distortions due to stresses set up within the structure by reason of the intense concentration of the high temperatures required by arc welding. A further advantage is that this is an important step in the trendtoward prefabrication of assemblies and as such will be the means of effecting a considerable saving of time. Muchless time will be required at the steel mill to form the reinforcement within the plate than would be required at the shipyard to weld a similar member to the plating plus the time required originally at the mill to roll the section. I
The following situation should be readily visualized: A vessel is in the process of design. The naval architects make up their drawings as at present showing welded stiffening members. As the structural drawings are completed they are submitted to the steel-mill for the purpose of ordering material. The engineers at the mill can easily substitute for the welded members shown on the drawings suitable and equivalent integral reinforcements. The plates are prepared at the mill and shipped to the building site ready for immediately assembly; the only additional requirement being to secure the butt edges of the prepared plates to each other.
The idea can no doubt be extended to other fields, particularly in the mass production of similar units. For example, in automobile body work and chassis fabrication where a saving in weight would mean greater economy in fuel consumption.
From the foregoing it will be observed. that in accordance with the present invention it is possible to provide all of the existing structural shapes as part of integral reinforcements. Further, many variations are possible with the present invention so that structural shapes may be provided in accordance with the engineering design as it advances in demand.
Not only does the present invention provide equivalent shapes to those presently used but permits a great saving in labor at the mill and in labor of assembly and construction in the field.
By employing the teachings set forth herein prefabrication of many designs will be possible, and as was previously pointed out by way of example, will have a special application in relation to ship construction. In this latter field, the integral reinforcements may be provided from large plates and may not only include the structural shapes, but may also take advantage of the fact that the plate itself may be curved, angled or bent in any shape or conformation depending on the requirement of the engineer.
An extremely wide latitude in fabricating formed sections and integral reinforcements is possible by the teachings of the present invention.
What is claimed as new and desired to be secured by Letters Patent of the United States is:
1. In a ship hull construction, a bottom shell plating having an integral longitudinal-extending structural stiffening portion formed of the plating bent back upon itself interior of the hull and providing vertical abutting surfaces lying in the outer side of the plating, said structural portion being further bent to provide a web and flange running coextensively of the plating, said structural portion having a slot through the flange and extending partially down through the web transversely thereof, and a bulkhead extending transversely through the structural portion and having a slot in its lower edge fitted in said slot in the structural portion and receiving the remainder of the web.
2. In a ship hull construction as defined in claim 1, and said web affording curved areas at the inward bends of the structural portion and said open edge slot in the bulkhead being rounded at the opposite sides to fit the curved areas whereby the lower edge of the bulkhead may be bottomed flush upon the shell plating.
3. In a ship hull construction as defined in claim 1, and said structural portion having opposing outer curved areas below the abutting surfaces thereof, and closure material extending therebetween.
(References on following page) 8 White Aug. 12, 1930 Weyerbacher Dec. 26, 1933 Vass July 9, 1935 Oeckl et a1. June 10, 1941 Krueger June 17, 1941 FOREIGN PATENTS Great Britain Oct. 15, 1942 France Dec. 1, 1947 France Dec. 1, 1947
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US184796A US2779303A (en) | 1950-09-14 | 1950-09-14 | Ship hull bottom plating having integral bent back reinforcement |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US184796A US2779303A (en) | 1950-09-14 | 1950-09-14 | Ship hull bottom plating having integral bent back reinforcement |
Publications (1)
Publication Number | Publication Date |
---|---|
US2779303A true US2779303A (en) | 1957-01-29 |
Family
ID=22678367
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US184796A Expired - Lifetime US2779303A (en) | 1950-09-14 | 1950-09-14 | Ship hull bottom plating having integral bent back reinforcement |
Country Status (1)
Country | Link |
---|---|
US (1) | US2779303A (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3128851A (en) * | 1964-04-14 | Interlocking metallic structural | ||
US4478126A (en) * | 1981-09-22 | 1984-10-23 | Dan Holmlund | Chamber for containing explosions, deflagrations or detonation and method of manufacture |
US4638754A (en) * | 1985-03-27 | 1987-01-27 | Tornay Edmund G | Vessel hull and bulkheads construction employing curved plating |
US4674430A (en) * | 1983-07-11 | 1987-06-23 | Hitachi Zosen Corporation | Ship without transverse reinforcing members between the inner and outer hull plating |
US5287671A (en) * | 1992-03-26 | 1994-02-22 | Ueki Kokan Kabushiki Kaisha | Construction panel with edges adapted to be coupled together |
US20040164580A1 (en) * | 2003-01-16 | 2004-08-26 | Armstrong Bradford D. | Lightweight composite tailgate |
US20040228991A1 (en) * | 2003-03-13 | 2004-11-18 | James Goggin | Hollow plastic article |
Citations (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US496465A (en) * | 1893-05-02 | Structural iron form | ||
US739650A (en) * | 1902-04-08 | 1903-09-22 | Joseph F Clutter | Method of making metallic columns. |
US831755A (en) * | 1902-04-12 | 1906-09-25 | Alwin Vietor | Rolled girder. |
US1429400A (en) * | 1921-04-30 | 1922-09-19 | Standard Sheet Metal Works | Sheet-metal building |
US1508743A (en) * | 1919-04-15 | 1924-09-16 | Orpha G Sigler | Signal box |
US1578416A (en) * | 1923-08-28 | 1926-03-30 | Frease Hurxthal Field | Structural material |
US1605513A (en) * | 1921-12-21 | 1926-11-02 | William M Connery | Reenforced fabricated metal plate wall section |
US1760332A (en) * | 1928-06-26 | 1930-05-27 | Vickers Aviat Ltd | Aeroplane wing and the like |
US1772694A (en) * | 1928-05-02 | 1930-08-12 | Truscon Steel Co | Roof decking and fastening means therefor |
US1940830A (en) * | 1931-10-03 | 1933-12-26 | Ralph D Weyerbacher | Form for making aircraft fuselages |
US2007354A (en) * | 1932-10-31 | 1935-07-09 | United States Gypsum Co | Composite building deck |
US2244847A (en) * | 1937-12-27 | 1941-06-10 | Henschel Flugseugwerke A G | Method of making structural elements of sheet metal |
US2245690A (en) * | 1940-12-19 | 1941-06-17 | H E Beyster Corp | Roof structure |
GB548572A (en) * | 1941-06-19 | 1942-10-15 | Alfred Elliott | Improvements relating to members consisting of a frame covered with sheet metal |
DE932820C (en) * | 1953-03-22 | 1955-09-08 | Torwegge Maschf F | Double abbreviation saw with a roller table made of prism rails |
DE932743C (en) * | 1953-03-26 | 1955-09-08 | Anton Bode | Thermal protective cover that surrounds the jug on all sides and can be adjusted to the height of the jug |
-
1950
- 1950-09-14 US US184796A patent/US2779303A/en not_active Expired - Lifetime
Patent Citations (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US496465A (en) * | 1893-05-02 | Structural iron form | ||
US739650A (en) * | 1902-04-08 | 1903-09-22 | Joseph F Clutter | Method of making metallic columns. |
US831755A (en) * | 1902-04-12 | 1906-09-25 | Alwin Vietor | Rolled girder. |
US1508743A (en) * | 1919-04-15 | 1924-09-16 | Orpha G Sigler | Signal box |
US1429400A (en) * | 1921-04-30 | 1922-09-19 | Standard Sheet Metal Works | Sheet-metal building |
US1605513A (en) * | 1921-12-21 | 1926-11-02 | William M Connery | Reenforced fabricated metal plate wall section |
US1578416A (en) * | 1923-08-28 | 1926-03-30 | Frease Hurxthal Field | Structural material |
US1772694A (en) * | 1928-05-02 | 1930-08-12 | Truscon Steel Co | Roof decking and fastening means therefor |
US1760332A (en) * | 1928-06-26 | 1930-05-27 | Vickers Aviat Ltd | Aeroplane wing and the like |
US1940830A (en) * | 1931-10-03 | 1933-12-26 | Ralph D Weyerbacher | Form for making aircraft fuselages |
US2007354A (en) * | 1932-10-31 | 1935-07-09 | United States Gypsum Co | Composite building deck |
US2244847A (en) * | 1937-12-27 | 1941-06-10 | Henschel Flugseugwerke A G | Method of making structural elements of sheet metal |
US2245690A (en) * | 1940-12-19 | 1941-06-17 | H E Beyster Corp | Roof structure |
GB548572A (en) * | 1941-06-19 | 1942-10-15 | Alfred Elliott | Improvements relating to members consisting of a frame covered with sheet metal |
DE932820C (en) * | 1953-03-22 | 1955-09-08 | Torwegge Maschf F | Double abbreviation saw with a roller table made of prism rails |
DE932743C (en) * | 1953-03-26 | 1955-09-08 | Anton Bode | Thermal protective cover that surrounds the jug on all sides and can be adjusted to the height of the jug |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3128851A (en) * | 1964-04-14 | Interlocking metallic structural | ||
US4478126A (en) * | 1981-09-22 | 1984-10-23 | Dan Holmlund | Chamber for containing explosions, deflagrations or detonation and method of manufacture |
US4674430A (en) * | 1983-07-11 | 1987-06-23 | Hitachi Zosen Corporation | Ship without transverse reinforcing members between the inner and outer hull plating |
US4638754A (en) * | 1985-03-27 | 1987-01-27 | Tornay Edmund G | Vessel hull and bulkheads construction employing curved plating |
US5287671A (en) * | 1992-03-26 | 1994-02-22 | Ueki Kokan Kabushiki Kaisha | Construction panel with edges adapted to be coupled together |
US20040164580A1 (en) * | 2003-01-16 | 2004-08-26 | Armstrong Bradford D. | Lightweight composite tailgate |
US6951357B2 (en) * | 2003-01-16 | 2005-10-04 | Decoma International Inc. | Lightweight composite tailgate |
US20040228991A1 (en) * | 2003-03-13 | 2004-11-18 | James Goggin | Hollow plastic article |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US4319121A (en) | Method of producing clad steel materials | |
EP3572256B1 (en) | Door beam | |
US20050077427A1 (en) | Lightweight structural component in particular for aircraft and method for its production | |
US3104454A (en) | Method of making structural members | |
US2779303A (en) | Ship hull bottom plating having integral bent back reinforcement | |
Chatti | Production of profiles for lightweight structures | |
CA1150986A (en) | Method for producing i-beam having centrally corrugated web and rolls for producing such i-beam | |
US4660491A (en) | Double hull ship without reinforcing transverse members between the inner and outer hull platings | |
WO2013106069A1 (en) | Welded hot-rolled high-strength steel structural members and method | |
US8079320B1 (en) | Perimeter frame system for use with construction barges | |
US11642712B1 (en) | Method of manufacturing vehicle body structure component to include reinforced regions | |
US20100012783A1 (en) | Coupling for joining two frame segments | |
US993242A (en) | Solid-rolled cross-sectionally-h-shaped metal bar or structural section. | |
US3112559A (en) | Hollow articles | |
RU2117561C1 (en) | Strip-bulb shape and method of its production | |
JP6574924B2 (en) | Lip channel steel | |
US2003138A (en) | Metallic structure and method of making the same | |
US5823042A (en) | Method of making an improved hot rolled I-beam and associated product | |
CN204590374U (en) | A kind of furred ceiling of large-scale storage tank | |
CN216969607U (en) | Landing leg assembly, landing leg and engineering machinery | |
US2179820A (en) | Metallic structure | |
CN106436927B (en) | Universal assembly type connecting system for two-way bending box-shaped section rods | |
CN218050773U (en) | Welded joint of superposed steel plates and metal sandwich plate | |
CN217705944U (en) | Sub-frame and working machine | |
CN110116783A (en) | LNG fills the drainage system and expansion expansion joint production method of boat deck |