REINFORCED COMPOSITE CORRUGATED BODY

Abstract: A reinforced composite corrugated body characterized in that, in order to improve the strength and processability thereof, a corrugated body is formed in such a manner that a sheet material is provided with corrugated lines having vertically arranged alternate ridges and grooves in a smooth meandering waveform in the horizontal direction in such a manner as to define the substantial amplitude ratio H/L of the corrugated line at 0.4 to 1.4 inclusive, the substantial meandering ratio D/N at 0.35 or below, the substantial meandering overlapping ratio D/L at 0.5 or above, and the width narrowing ratio (i) in the direction in which the corrugated line extends at stretch strain ratio of the sheet material +8% or below, and that the crest and bottom of each corrugated line have curved, narrowly chamfered or shoulder-rounded cross sections, and that at least one side of the corrugated body is lined with a flat plate.

Description: This invention relates to a composite corrugated body wherein vertically extending ridges and grooves are formed alternately on a sheet material to form corrugate lines which meander in a plane to form a corrugated body and wherein a flat liner is adhered to at least one of the opposite faces of the corrugated body. The invention also relates to a method of production of such a corrugated body. Various sandwiched materials such as a corrugated board and a honeycomb board are well known already, and one corrugated board which has been actually put into practice includes a corrugated body having straight corrugate lines thereon and having a flat sheet adhered to at least one of the opposite faces thereof. In recent years, however, various modifications and improvements have been made to such a corrugated body and many publications of investigations are available of corrugated bodies which have meandering corrugate lines as hereinafter described. The inventor has made several investigations and experiments, and it has been found that, in order to put such corrugated body into practical use, if must have at least such structural features as given below: (1) As compared with an existing composite corrugated body wherein two flat sheets are applied to the opposite faces of a straight corrugated body as is represented by the structure of an ordinary corrugated board, a composite corrugated body which includes two flat sheets of a similar material and having an equal thickness, the amount of material of the corrugated body is equal or increased by 10%, and the structural strength is improved by more than 15%. (2) A corrugated body can be formed at a working speed higher than 50 meters per minute by roll forming which assures a quality normally maintaining a stable shape and material strength (The workability is high). (3) Consequently, the effect with respect to expense, that is, the structural strength/cost of a product is higher by at least 10%, and desirably by 30% or more, than that of an existing composite corrugated body. The structural strength that a composite corrugated body should have will be described subsequently. In such a composite corrugated body 4 as shown in FIG. 17, wherein a corrugated body 2 having meandering corrugate lines 1 and flat sheets 3 are integrated with each other: 〈Profile Requirement A-1〉 It is essential that the flat crush or shearing rigidity in the x direction in the z-x plane should be sufficiently high, and to this end, it is required that the substantial amplitude ratio H/L of the profile of the corrugate lines 1 should be higher than 0.4 (refer to FIG. 17(A)). The substantial amplitude ratio H/L is a ratio between an amplitude H and a wavelength L of a sectional wave when the corrugate lines 1 are cut along the x-z plane, i.e. are cut along a vertical plane in the x direction in FIG. 17(A). 〈Profile Requirement A-2〉 It is essential that the rigidity in the x direction against bending out of the x-y plane is sufficiently high, and to this end, it is required that the substantial meandering overlapping ratio D/L of the profile of a corrugate line 1 should be higher than 0.5 (refer to FIG. 17(B)). The substantial meandering overlapping ratio D/L is a ratio between an amplitude D and said wavelength L when each corrugate line 1 is viewed in a plane. 〈Profile Requirement A-3〉 It is essential that the compression rigidity in the x-y plane should be sufficiently high, and to this end, it is desired that the joining width w between the corrugated body 2 and the flat sheets 3 when they are adhered to each other should be as great as possible (refer to FIG. 17(C)). Among the three requirements described above, the requirements A-1 and A-2 should be provided at the same time, and if one of the requirements is not satisfied, the required mechanical strength will not be achieved. The workability that a composite corrugated body should have will now be described. When a work sheet is roll formed at a high speed by a corrugator, it is first necessary for a stretch strain ratio to be restricted to lower than 5% at around the crest and bottom portions of the corrugate lines 1. Further, it is essential that no tearing damage should take place at or around neutral axes of the corrugate lines 1 and also that no excess wrinkle should appear at or around the center axes of the grooves of the corrugate lines 1 (refer to FIG. 17(D)). To this end: 〈Profile Requirement B-1〉 Such values of the substantial meandering ratio D/N as well as the substantial amplitude ratio H/L of the profile of the corrugate lines 1 as will make a width narrowing ratio i in the direction of the corrugate lines 1 lower than 10% should be selected. The substantial meandering ratio D/N is a ratio between the amplitude D and the wavelength N when each corrugate line 1 is viewed in a plane. The width narrowing ratio i increases when the ratio D/N increases. 〈Profile Requirement B-2〉 Sections at crest and bottom portions of the corrugate lines 1 should be formed such that they may be curved or chamfered over a small width. 〈Profile Requirement B-3〉 The meandering pattern of the corrugate lines 1 in a plane should be a smooth waveform pattern, and particularly bent portions of the corrugate lines in a plane around center axes of the ridges and grooves should be curved or chamfered with a rather large width. The profile requirements B-1 and B-2 described above should be satisfied at the same time, and if the profile requirement B-3 is satisfied in addition to the two requirements, the workability is improved further. From such a point of view, description will be individually given concerning the reasons why the conventional examples shown in FIGS. 18 to 26 have not been put into practical use in a mass production system (which employs forming rollers, to be hereinafter described) because they lack one or more of the decisive profile requirements found out by the inventor and described above. As shown in FIGS. 18 to 20, a corrugate body 2 of the conventional example is used as a single body and is applied as a cushioning material for glass vessels. However, such a conventional example is quite unsuitable as a composite corrugate body integrated with a flat sheet, and in fact, such a product is not to be found. This is because, as is apparent from the corrugated bodies 2 of the first and second conventional examples shown in FIGS. 18 and 19, the substantial amplitude ratios of sectional profiles of the corrugate lines 1 in the x direction are H/L ≒ 0.15 and H/L ≒ 0.18, respectively. Accordingly, even if composite corrugated bodies integrated with flat sheets are produced, the shearing rigidities in the x direction in the z-x plane will be extremely low and will be very far from the structural strength of an existing corrugated board. In the corrugated body 2 of the third conventional example shown in FIG. 20, since the substantial meandering overlapping ratio of the corrugate lines 1 is D/L ≒ 0.17 and very low, even if a composite corrugated body integrated with flat sheets is produced, the bending rigidity of the composite corrugated body in the x direction outside the x-y plane will not provide a great difference from that of an existing corrugated board. A characteristic of the first to third conventional examples is that the corrugated bodies 2 themselves are mass-produced on an industrial scale by roll forming and are used as cushioning materials. In the first and second conventional examples, H/L and D/N are selected so that the width narrowing ratio i in the axial direction of the corrugate lines 1 may be i < 5%, and in the third conventional example, the width narrowing ratio i is i > 10%, but roll forming is made possible only by using a work sheet having a very high stretch performance (a stretch ratio of 5 to 7% or so). However, they have a serious defect in that they cannot be put into practical use because such composite corrugated bodies with integrated flat sheets are low in structural strength. The fourth to ninth convention examples of FIGS. 21 to 26 are characterized in that, while the first to third conventional examples have comparatively shallow and small corrugate lines 1 formed therein, they have comparatively deepened large corrugate lines 1 formed therein. More particularly, since the substantial amplitude ratio H/L of the corrugate lines 1 of the fourth conventional example in FIG. 21 is 0.7 and the substantial meandering overlapping ratio D/L is 0.8, the structural strength of a composite corrugated body obtained by integration of the same with flat sheets is very high in principle. On the other hand, since the substantial meandering ratio D/N is 0.6 or so and very high, the width narrowing ratio i is higher than 23%, and roll forming is impossible in fact. Thus, while the strength is sufficiently high, the fourth conventional example cannot be put into practical use. Further, since bent portions of a meandering pattern in a plane of the corrugate lines 1 at center axes of the ridges and grooves thereof project in acute angles, breaks may still occur around projected portions of a work sheet (a sheet on which corrugate lines are to be formed) during roll forming. Also, since the sectional shapes of the crest and bottom portions of the corrugate lines 1 are bent sharply, portions thereof joining with flat sheets are very weak, and accordingly, it can be said that a sufficient joining strength cannot be provided and thus the actual structural strength is not very high. The fifth conventional example in FIG. 22 is formed in a deeper configuration than the fourth conventional example, and accordingly, it is further improved in structural strength, but the workability is further deteriorated. Then, while the substantial amplitude ratio and the substantial meandering overlapping ratio representing strength are H/L ≒ 0.8 and D/L ≒ 1.3, respectively, and sufficiently high, since the width narrowing ratio representing workability is i < 30% and very high, it can be seen that working formation by roll forming is almost impossible. However, since the bent portions a at the central axes of the ridges and grooves of the corrugate lines 1 form curved projections, there is an advantage that tearing and stretching distortion of a work sheet is moderated a little upon roll forming. The sixth conventional example in FIG. 23 is formed to have substantial amplitude ratio H/L and substantial meandering overlapping ratio D/L values similar to those of the fourth conventional example and is sufficiently high in structural strength. Further, since sections of the crest and bottom portions of the corrugate lines 1 are formed to have a rather large curved shape, joining areas of flat sheets are increased and the structural strength is improved. However, since the substantial amplitude ratio and substantial meandering ratio are H/L ≒ 1.0 and D/N ≒ 0.5, respectively, and high, the width narrowing ratio is i > 25% and inevitably very high. As a result, it is apparent that roll forming is impossible. The seventh conventional example in FIG. 24 is characterized in that the crest and bottom portions of the corrugate lines 1 have a trapezoidal shape that is very convenient for joining to the flat sheets. Further, since the substantial amplitude ratio of the corrugate lines 1 is H/L ≒ 0.8 and high, the shearing rigidity is high, and since the substantial meandering overlapping ratio is D/L ≒ 0.7 and high, the bending rigidity is increased. Consequently, the total structural strength is improved. However, since the width narrowing ratio when H/L ≒ 0.8 and D/N ≒ 0.5 is i > 25% and very high, roll forming is quite impossible. Further, acute projections a are present around the center axes of the ridges and grooves in a meandering pattern of the corrugate lines 1 in the x-y plane, and upon roll forming, a work sheet is subjected to sudden pressurization and deformation by such projections a to yield excessive stretching distortion to finally produce tearing damage. Further, while the trapezoidal shape of the crest and bottom portions forms wide flat faces, strong stretching distortion involved in a width narrowing process is produced in the flat face around the projections a, and as a result, stable working formation is difficult. The eighth conventional example in FIG. 25 is an improvement of the seventh conventional example and is characterized in that portions of the corrugate lines 1 around the center axes of the ridges and grooves in a meandering pattern in the x-y plane are bent in a trapezoidal shape. Since the substantial amplitude ratio of the corrugate lines 1 is H/L ≒ 0.8 and high, the shearing rigidity is sufficiently high, but since the substantial meandering overlapping ratio is D/L ≒ 0.3 and low, the bending rigidity is very low, and as a result, the structural strength is not improved very much compared with that of the shape of an existing corrugated board or the like. Further, since the substantial amplitude ratio and substantial meandering ratio are H/L ≒ 0.8 and D/N ≒ 0.3, respectively, the width narrowing ratio i is i ≒ 14% and high and roll forming is difficult. In addition, since pairs of dull projections of the corrugate lines 1 formed around the center axes of the ridges and grooves in a meandering pattern in a plane locally pressurize a work sheet upon roll forming, remarkable stretching distortion is produced. Also remarkable stretching distortion is produced around the trapezoidal crest and bottom portions similarly as in the seventh conventional example, which makes stable working formation impossible. The ninth conventional example in FIG. 26 can be said to be a further improvement of the eighth conventional example, but since the substantial amplitude ratio H/L and substantial meandering overlapping ratio D/L of the corrugate lines 1 are equal to those of the eighth conventional example, the structural strength obtained is insufficient. Further, since the substantial meandering ratio D/N is substantially equal to that of the eighth conventional example, the width narrowing ratio is i ≒ 14% and high and roll forming is difficult. In addition, since the crest and bottom portions of the corrugate lines 1 have trapezoidal flat faces, problems which take place upon roll forming are similar to those of the seventh or eighth conventional example. However, since no projections are present at bent portions of the corrugate lines 1 in a meandering pattern in the x-y plane, this example is effective to restrict occurrences of stretching distortion or tearing damage of a work sheet a little as compared with the seventh or eighth conventional example. However, the extreme difficulty in roll forming is a decisive reason preventing practical use. For the reasons described above, none of the corrugated bodies of various profiles have been put into practical use, except for utilization thereof by themselves as cushioning materials, in various applications of mass consumption, for example a composite corrugated body which is obtained by integration of a corrugated body and flat sheets with each other is used for a corrugated board which is inexpensive and has a high structural strength. Further, there is no previous instance of mass production other than those described above. Accordingly, the inventor has invented a reinforced composite corrugated body which was disclosed in Japanese Patent Laid-Open No. 284737/1987. Further improvements were then provided by the present inventor in Japanese Patent Laid-Open No. 8031/1989 in order to solve the problems of the prior art. Indeed these reinforced composite corrugated bodies have achieved improvements in structural strength and workability when compared with the earlier prior art corrugated bodies. However, subsequent investigations and experiments have revealed that the corrugated bodies disclosed in Japanese Patent Laid-Open No. 284737/1987 and No. 8031/1989 do not sufficiently meet the contradictory requirements of structural strength and workability. Consequently, reinforced composite corrugated bodies which are effective as a material for wide applications and mass production could not be provided. The present invention has been made in view of such problems as described above, and it is an object of the present invention to provide a reinforced composite corrugated body which is improved in structural strength against various mechanical external forces and can bring about such workability as will enable stable and high speed roll forming. In order to attain the object, according to the present invention, there is provided a reinforced composite corrugated body, constituted such that corrugate lines provided by vertically extending ridges and grooves formed alternately on a sheet material are formed in a meandering waveform in a horizontal direction such that they may have a substantial amplitude ratio H/L higher than 0.4 but lower than 1.4, a substantial meandering ratio D/N lower than 0.35, a substantial meandering overlapping ratio higher than 0.5 and a width narrowing ratio i in their advancing direction lower than 8% + a stretch strain ratio of the sheet material and sectional shapes of crest and bottom portions of the corrugate lines are curved or chamfered with a small width to form a corrugate body, and a flat liner is adhered to at least one of the opposite faces of the corrugated body. As a result, the reinforced composite corrugate body of the present invention can improve the structural strength remarkably with the same sheet material and same plate thickness and so forth, compared with an existing corrugated board and at the same time enables roll forming at a high working speed without causing tearing damage or excess wrinkling. Thus, it can remarkably improve the structural strength/cost of the product, that is the value of the product compared with that of an existing corrugated board or the like. The above and other objects, features and advantages of the present invention will become apparent from the following description of embodiments described in detail hereinbelow with reference to the accompanying drawings. FIG. 1 is a partial perspective view showing a flat liner material, partly broken, of a composite corrugated body which is used in the present invention; FIG. 2 is a sectional view showing the shape of a composite corrugated body according to the present invention in an x direction of corrugate lines; FIG. 3 (A) is a plan view showing a composite corrugated body of the present invention and a characteristic profile of the same; FIG. 3 (B) is a waveform diagram in a plane showing edges of a meandering pattern of corrugate lines; FIG. 4 is a view schematically showing a direction of shearing stress in a composite corrugated body of the present invention; FIG. 5 is a graph of profile-shearing strength curves illustrating a relationship between a maximum shearing stress index number in the x direction in the z-x plane and a gradient  of inclined wall faces of corrugate lines and a substantial amplitude ratio H/L of corrugate lines in a composite corrugated body; FIG. 6 is a view schematically showing a direction of bending stress in a composite corrugated body; FIG. 7 is a graph of profile-bending strength curves illustrating a relationship between a maximum bending stress index number in the x direction outside the y-x plane and a substantial meandering overlapping ratio D/L as well as a substantial meandering ratio D/N of corrugate lines in a composite corrugated body; FIGS. 8 (1-4) are views illustrating a positional relationship between corrugate lines at different meandering overlapping ratios thereof in a composite corrugated body and a positional relationship between the corrugate lines and a flat liner material; FIGS. 9 (A-D) are waveform diagrams in transverse section of a composite corrugated body in an x direction of corrugate lines; FIG. 10 is a broken perspective view schematically illustrating a roll forming method which is used to work and shape a reinforced corrugated body; FIG. 11 is a graph showing a relationship between a collapse occurrence frequency index number and a width pre-narrowing ratio of a corrugated work sheet upon roll forming of a composite corrugated body; FIG. 12 is a view showing an example of corrugate lines which satisfies a second requirement in production; FIGS. 13 (A-H) are views of various waveforms in a plane showing meandering waveforms of corrugate lines of a composite corrugated body; FIGS. 14 (A-B) are views showing a modification of the present invention; FIGS. 15 (A-D) are views showing a further modification of the present invention; FIG. 16 is a graph of profile curves showing a relationship among a substantial amplitude ratio H/L, a substantial meandering ratio D/N and a y direction width narrowing ratio i of corrugate lines of a composite corrugated body according to the present invention; FIGS. 17 (A-D) are perspective views showing an example of a conventional corrugated body; FIGS. 18 (A-C) are perspective views showing a corrugated body of a first conventional example; FIGS. 19 (A-C) are perspective views showing a corrugated body of a second conventional example; FIGS. 20 (A-C) are perspective views showing a corrugated body of a third conventional example; FIGS. 21 (A-C) are perspective views showing a corrugated body of a fourth conventional example; FIGS. 22 (A-C) are perspective views showing a corrugated body of a fifth conventional example; FIGS. 23 (A-C) are perspective views showing a corrugated body of a sixth conventional example; FIGS. 24 (A-C) are perspective views showing a corrugated body of a seventh conventional example; FIGS. 25 (A-C) are perspective views showing a corrugated body of an eighth conventional example; and FIGS. 26 (A-C) are perspective views showing a corrugated body of a ninth conventional example. In the following, preferred embodiments of the present invention will be described with reference to the accompanying drawings. FIG. 1 shows an example of a single faced reinforced composite corrugated body 10 constituting a wrap around case according to the present invention, body 10 being constituted by a corrugated body 11 and flat liners 12. The corrugated body 11 has ridges M and grooves V provided in vertical (z) planes and arranged alternately in an x direction to form corrugate lines 13. The corrugate lines 13 are meandered in a waveform in a y direction in the x-y plane such that they extend in parallel to each other. Then, the flat liners 12 are adhered integrally to the corrugate lines 13 at the ridges M and grooves V. The profile of the corrugate lines 13 of the corrugated body 11 described above is determined by taking also into consideration facility in production (workability), in order to assure a desired strength and achieve practical use of the corrugated body 11. Before the strength and workability are considered and described, a detailed description (definition) will first be given of a substantial amplitude ratio H/L, a substantial meandering overlapping ratio D/L and a substantial meandering ratio D/N (described briefly in the discussion of the prior art) which will provide a standard of performance of the corrugated body and reinforced composite corrugated body. The substantial amplitude ratio H/L represents a relationship between an amplitude H and a wavelength L of a sectional wave formed by cutting the corrugate lines 13 along the vertical z-x plane in FIG. 1 and is determined in the following manner. In particular, there is determined a substantial amplitude H of a substantial sectional waveform 15 which is obtained by linearly extending slopes of opposite inclined wall portions of a sectional waveform of a corrugate line 13 (see also FIG. 2) in both upward and downward directions. The substantial amplitude ratio H/L is the ratio of the substantial amplitude H to a period L of the sectional waveform. The substantial meandering ratio D/N represents a relationship between an amplitude D and a wavelength N when each corrugate line is viewed in the x-y plane. Particularly, the substantial meandering ratio D/N is determined in the following manner. With reference to FIGS. 3(A) and 3(B), a reference meandering pattern 17 is obtained by extending linearly in the opposite upward and downward directions slopes of portions around each neutral axis of a waveform of a corrugate line 13 as viewed in the x-y plane. A meandering pattern 16 has an amplitude D 0 . The reference meandering pattern 17 has an amplitude D 1 . A substantial meandering pattern 18 has a substantial amplitude D determined as D = D 0 + (D 1 - D 0 ) x k (where k ≒ 0.3) . The substantial meandering ratio D/N is the ratio of the substantial amplitude D to the meandering pattern period N. Further, the substantial meandering overlapping ratio D/L represents, as shown in FIG. 1, a relationship of the amplitude D of each corrugate line and the wavelength L of the sectional wave when the corrugate lines are viewed in the z-x plane. The profile requirements A-1, A-2 and A-3 which are needed for structural strength are described one by one below with regard to bases, origins, actions and effects thereof. 〈Profile Requirement A-1〉 Using, as a variable, an inclination gradient  of an inclined wall portion 20 of a corrugate line 13 with respect to a flat liner 12, that is the substantial amplitude ratio H/L of a sectional waveform of a corrugate line 13, a variation in value of shearing stress Gx (refer to FIG. 4) in the x direction in the x-y plane relative to a variation of such variable is confirmed by experiments, the results of which are illustrated in graphs as a set of profile-shearing strength curves in FIG. 5. Here, the functional expression of the curve set is represented as Gx = g j (H/L) , where Gx is a maximum shearing stress index number in the x direction, g is a functional symbol, and j is a parameter equal to the substantial meandering ratio D/N of a waveform of a corrugate line 13 as viewed in the x-y. As can be seen from the FIG. 5, the individual curves vary such that, as the substantial meandering ratio j increases from 0 to 0.5 in value, the curves are gradually and successively shifted upward in a similar manner to parallel movement, while gradually the distance between the curves decreases. Most characteristic is that each of the curves rises in a comparatively steep gradient until the shearing stress exceeds Gx = 1.0, while the inclination angle varies from  = 10° (H/L ≒ 0.1) to  = 40° (H/L ≒ 0.4). After around  = 45° (H/L ≒ 0.5), the gradient is moderated a little, and then the summit is reached finally around  ≒ 55° (H/L = 0.7). Each curve then drops in a comparatively steep gradient to around  ≒ 70° (H/L = 0.4). After  ≒ 70°, the gradient is moderated a little until ℓ ≒ 90° is reached. In particular, the characteristic of each curve is that a common peak effect appears around  ≒ 55° (H/L = 0.7). In other words, judging from the fact described above, the inclination angle  at which a predetermined shearing strength Gx which can be effective for practical use can be obtained is 40° ≤  ≤ 70° centered at 55°. In terms of the substantial amplitude ratio H/L, it is possible to approximately define 0.4 ≤ H/L ≤ 1.4 as an appropriate substantial amplitude ratio (hatched area in the FIG. 5). It is to be noted that Gx = 1.0 is a maximum shearing stress in the x direction at j = 0, that is, at a peak which can be seen with a composite corrugated body such as an existing corrugated board. 〈Profile Requirement A-2〉 A factor which assures practical use of structural strength of a reinforced composite corrugated body is out-of-plane bending rigidity in a perpendicular direction to a corrugate line, in addition to shearing stress (strength) as described above. In particular, it is a maximum bending stress in the x direction in the z-y plane as shown in FIG. 6. Using as a variable the ratio of the amplitude D of a corrugate line 13 in a waveform as viewed in the x-y plane to a period L of the sectional waveform of corrugate line 13, that is the substantial meandering overlapping ratio D/L, variations of values of the maximum bending stress (index number) relative to variations of such variable is confirmed by experiments, the results of which are indicated as a set of profile-bending strength curves in FIG. 7. The functional expression of the curve set is represented as Mx = h j (D/L) , where Mx is a maximum bending stress index number in the x direction, h is a functional symbol, and j is a parameter equal to the substantial meandering ratio D/N. As is apparent from FIG. 7, the individual curves vary such that, as the value of the substantial meandering ratio j increases from 0 to 0.15, the curves are gradually and successively shifted upwardly while their gradients change slightly and the distance between the curves gradually decreases. Most characteristic is that each of the curves rises in a low gradient while the substantial meandering overlapping ratio D/L varies from 0 to 0.5, but after D/L exceeds 0.5 each curve rises in a steeper gradient, and after D/L exceeds 1.0, the gradient of each curve further increases. In other words, each curve has specific D/L values which produce two bending points for the curve, and such values are common to the individual curves having different values of j. It is to be noted that Mx = 1.0 is a bending stress which can be seen with a composite corrugated body having j = 0, that is, a composite corrugated body like an existing corrugated board. It has been made clear that each of the profile-bending stress curves Mx = h j (D/L) has two bending points where the substantial meandering overlapping ratio D/L is 0.5 and 1.0 as described above. However, variations of the D/L value are observed with regard to a mutual positional relationship of meandering patterns of the corrugate lines as viewed in a plane parallel to the x-y plane. With reference to FIG. 8 (A), there is shown a meandering pattern in the y direction of a pair of adjacent ridges M 1 , M 2 with a groove V therebetween and defining a meandering inclined wall portion extending upwardly from groove V to ridge M 1 and an inclined wall portion extending upwardly from groove V to ridge M 2 . Center axes of bent portions of each ridge and groove extend in the x direction (see FIG. 3(B)). A plane S 1 parallel to the y-z plane defines a line in the y direction that connects all of the center axes of the bent portions m of ridge M 1 at points of contact thereof with an upper liner 12. Similarly, a plane S 2 parallel to the y-z plane defines a line that connects all of the center axes of bent portions n of groove V that are between bent portions m in the y direction at points of contact thereof with a lower liner. A plane S 3 is parallel to the y-z plane and bisects the meandering pattern at the center of groove V. As shown in FIG. 8(A), when D/L < 0.5 plane S 1 is spaced away from plane S 2 in the x direction, with a gap between planes S 1 and S 2 . As shown in FIG. 8(B), when D/L = 0.5 planes S 1 and S 2 coincide. As shown in FIG. 8(C), when D/L = 1.0 plane S 1 is shifted beyond plane S 2 and coincides with plane S 3 . As shown in FIG. 8(D), when D/L > 1.0 plane S 1 is further shifted beyond plane S 3 . Further, if variations of the positional relationship of the meandering patterns of the corrugate lines in a plane with respect to values of D/L described above are observed with regard to a sectional shape of the lines in the y direction of the reinforced composite corrugated body, then the characteristic profile of a truss-like structure which the reinforced composite corrugated body has, and the variation of the out-of-plane bending strength Mx in the x direction which the reinforced composite corrugated body has, become more apparent. In particular, when D/L < 0.5, since the reinforced corrugated body is joined to the flat liners 12 only on one face thereof, the truss-like structure is a little unstable, and consequently, the bending strength Mx is very low (FIG. 8-1). When D/L = 0.5, since the reinforced corrugated body is joined in two flat liners on the opposite upper and lower faces thereof (FIG. 8-2), the characteristic in profile of the truss-like structure is quickly changed into a stable one comparing with the truss-like structure described above. When D/L < 0.5, as the value increases gradually, the inclination angle of a web (diagonal) of the truss-like structure becomes larger. Accordingly, the strength Mx is increased with respect to that when D/L < 0.5. When D/L = 1.0, the joining density of the reinforced corrugated body to the flat liners on the opposite upper and lower faces thereof is doubled (FIG. 8-3) compared with that when D/L = 0.5, and consequently, the characteristic in profile of the truss-like structure is changed suddenly into more stable one comparing with that of the truss-like structure described above. When D/L > 1.0, as the value decreases gradually, the inclination angle of the web of the truss-like structure becomes more steep, and the vertical height of a triangle which is constituted by the web joined only to a flat liner on one face of the reinforced corrugated body and the flat liners is increased, and consequently, the strength Mx increases more rapidly than when D/L < 1.0. While it has been made clear that each of the profile-bending strength curves Mx = h j (D/L) has two singular points at D/L = 0.5 and D/L = 1.0 at which the bending stress Mx increases suddenly as described above, in order to assure a bending stress Mx which is suitable to enable a reinforced composite corrugated body of the present invention to be put into practical use, the substantial meandering overlapping ratio D/L should be D/L > 0.5, and such range is indicated as a hatched area and a meshed portion in FIG. 7. Then, more preferably, D/L should be D/L > 1.0, and such range is indicated by the meshed portion of the same figure. 〈Profile Requirement A-3〉 In order to obtain a desired strength for the corrugate lines, it is necessary to satisfy a requirement described below in addition to the various requirements described above. In particular, the various structural strengths which a reinforced composite corrugated body according to the present invention has can be obtained only by joining and integration of a reinforced corrugated body and flat liners. Above all, the shearing strength in the x direction and the bending strength in the x direction are determined to a significant extent by the joining area between the reinforced corrugated body and flat liners. Where the joining method and the bonding agent are the same, such strengths increase in proportion to the increasing joining area. Accordingly, the contact area should be made comparatively great. More particularly, as shown in FIG. 9, the reinforced corrugated body should be formed such that the sectional shapes of the crest and bottom portions of the corrugate lines are such that the bending width w of the crest and bottom portions is increased as much as possible. Thus, requirements (profile requirements B-1, B-2 and B-3) for a reinforced composite corrugated body which can be produced easily will be described one by one below in connection with bases, origins, actions, and effects thereof. 〈Profile Requirement B-1〉 A procedure for producing a reinforced corrugated body will first be described. As shown in FIG. 10, a corrugated work sheet 24 to which a predetermined width narrowing process has been applied in advance is inserted between a pair of forming rollers 23 each of which has a large number of tooth-shaped ribs 22 formed in a circumferential direction on a peripheral face thereof such that they substantially coincide with the corrugate lines to be produced. Then, as the corrugated work sheet 24 is shaped under pressure between the two forming rollers 23, corrugate lines of a desired profile are produced (roll forming method). It is to be noted that the width narrowing applied to the corrugated work sheet 24 (width pre-narrowing ratio i 0 ) is set substantially equal to a final width narrowing ratio i (strictly, i ≥ i 0 because the sheet itself shrinks upon working). The width narrowing ratio i denotes a coefficient of contraction of the width of a sheet after formation of the corrugate lines with respect to the width of the sheet in the form of a flat plate before formation of the corrugate lines. If the width narrowing ratio i (pre-narrowing ratio i 0 ) is increased beyond a certain limit, excess wrinkling and breaking in the x direction frequently occur. This is because the H/L ratio of a sectional waveform of the corrugated body 11 becomes excessively high and irregular buckling deformation takes place locally in a sectional waveform which is pressurized directly after the corrugated body 11 is supplied between the forming rollers 23. Consequently, collapse and accompanying cramping are caused while at the same time the distribution of a uniform width narrowing ratio i in the lateral direction is prevented to a remarkable degree. More particularly, if a limit to a predetermined width narrowing ratio i is described with reference to the graph in FIG. 11 which shows a relationship between the occurrence of collapse and the width pre-narrowing ratio i 0 , the predetermined narrowing ratio i required for the corrugated body 11 which is obtained by roll forming in the first place is given by i > i 0 + β. Here, β is a lateral direction limit of stretch strain ratio of the corrugated work sheet 24 and is such that, if the limit is exceeded, the deterioration in material strength (a condition in which the strength is decreased by 30% of that in the initial state) is so remarkable that the corrugated work sheet 24 can no longer be used in practice. In the case of a paper sheet, a steel sheet or a semi-rigid plastic sheet which has a low stretching limit, 2.0% is determined as the limit stretch strain ratio β, and in the case of an aluminium sheet or a plastic sheet, the stretching limit is relatively high and accordingly 5.0% is determined as the limit stretch strain ratio β. It is to be noted that the collapse frequency index number in FIG. 11 is determined to be 1.0 where the width pre-narrowing ratio i 0 = 5.0%. As is apparent from FIG. 11, while the value of the collapse frequency increases together with a variation of the width pre-narrowing ratio i 0 , such increase becomes radical after substantially i 0 = 8.0% is exceeded. Accordingly, in order to minimize occurrences of collapse and so forth of the work sheet, it is necessary to set the width pre-narrowing ratio i 0 within the range of 0 < i 0 ≤ 8.0% (hatched area in the figure). Accordingly, in order for the final corrugate body 11 to be worked and shaped by a stable and high speed roll forming method, the predetermined width narrowing ratio i should be 0 < i ≤ 8% + β, and particularly, when the stretch strain ratio β of the work sheet is 0 ≤ β ≤ 2.2%, the value i should be within the range of 0 < i ≤ 10.0%. 〈Profile Requirement B-2〉 While the crest and bottom portions of the corrugate lines have a predetermined bent width w due to the necessity to provide a predetermined strength as described above, if a corrugate line 13' is formed to have, for example, a substantially trapezoidal cross section in which it is flat at the crest and bottom portions M and V, as shown in FIG. 12, in order to satisfy the requirement, then when it is worked and shaped by the roll forming as described above, the trapezoidal flat faces at the crest and bottom portions of the corrugate line are subjected, when seen microscopically, to in-plane curving deformation mainly at bent portions near the center axes ℓ1 and ℓ2 of the ridges and grooves. Because the trapezoidal faces are flat, outside portions (hatched portions in FIG. 12) in a plane of the corrugate lines of the trapezoidal faces around the bent portions undergo stretching deformation due to strain. Thus, remarkable distortion deformation or break damage is caused in a concentrated manner, which will prevent the product being of practical use. In order to solve this problem various sectional shapes of the crest and bottom portions M and V should be as shown in FIGS. 9 A to D. In particular, the sectional shape of each of the crest and bottom portions M and V is formed such that either a flat face is eliminated (FIGS. 9 A-1, A-2, A-4, B-1, B-3, C or D) or a very restricted small flat face is left (FIGS. 9 A-3 or B-2). The former examples provide in-plane curving deformation mainly of the bent portions involved in predetermined width narrowing in the y direction. This makes it easy to restrict as much as possible occurrences of residual distortion stress such as distortion deformation. As a result, it is possible to prevent occurrence of break damage and so forth. In the case of the latter examples, since very small flat faces remain in the sectional shapes of the crest and bottom portions, that is since strip-like flat faces of a small width remain, the amount of local in-plane stretching distortion and in-plane curving deformation of the bent portions involved in predetermined width narrowing in the y direction are very small. Thus, no break damage takes place and residual distortion stress can almost be ignored. 〈Profile Requirement B-3〉 Further, according to the present invention, the meandering pattern of each of the corrugate lines 13 in the x-y plane is a smooth meandering pattern of a waveform shape. More particularly, the meandering pattern has the form of a continuous curves over the overall length of each corrugate line 13 (FIG. 13(A)), or has curved bent portions which are interconnected by straight lines (FIG. 13(B)), or has straight bent portions which are interconnected by curved lines (FIG. 13(C)), or has a trapezoidal shape formed by connection of straight line sections over the overall length with chamfered corner portions (FIG. 13 (D)), or has a trapezoidal shape formed by connection of straight line sections over the overall length in a comparatively flat profile such that the interior angle  between opposing oblique lines is greater than 120° (FIG. 13(E)), or has a comparatively flat zigzag pattern having an interior angle ▪ of 120° or more (FIG. 13(F)), or else has bent portions of curved line segments which are interconnected by wave-shaped curves of a comparatively small period (FIG. 13 (G) or (H)). Various acute projections in the waveforms are not included in the meandering patterns of corrugate lines according to the present invention which rather are formed in a smooth waveform in a plane as described above. This further signifies that tooth-shaped ribs 22 of the forming roller are formed to have a meandering pattern of a smooth waveform shape. Upon roll forming, pressure applied to the corrugated work sheet 24 is dispersed over a comparatively wide area by the tooth-shaped ribs 22. As a result, local distortion deformation is eliminated, and at the same time, slipping movement of the work sheet on the ribs upon stepwise feeding in the x direction is not obstructed at all. Thus, stretching distortion deformation in the x direction and breaks due to such stretching distortion deformation can be prevented. Further, slipping movement of the work sheet 24 on the tooth-shaped ribs 22 upon fine adjustment of width narrowing in the y direction is not obstructed at all. Thus, stretching distortion deformation in the y direction and breaks due to such stretching distortion deformation can be restricted sufficiently. As a result, roll forming of a reinforced corrugated body of the present invention can be performed stably and at a high speed. 〈Requirements to Further Improve the Workability〉 While a good workability can be exhibited by the profile requirements B-1 to B-3 described above, the workability is further improved if the following requirements are met. In particular, the work sheet is divided for convenience into an anterior wave portion (portion A) and a posterior wave portion (portion B) of the corrugate lines 13 as shown in FIGS. 14 and 15. Division the work sheet into the portion A and portion B is such that a forward portion in the advancing direction of the corrugated work sheet 24 to be inserted between the forming rollers 23 in order to form corrugate lines 13 is determined as the portion A while a rearward portion is determined as the portion B. The width narrowing ratio i a at the anterior wave portion (portion A) should be lower than the width narrowing ratio i b at the posterior wave portion (portion B). Means for changing the width narrowing ratio should be such that, for example, a total of y direction waveform components of the posterior wave portion B in a waveform in a plane should be greater than a total of y direction wave components of the anterior wave portion A. A "waveform component" denotes a gradient (angle) of a tangential line to each point on a continuous waveform. More particular means can be such that, for example, as shown in FIG. 14 (A), a relationship between a curvature r a of the portion A and another curvature r b of the portion B in the waveforms of the corrugate lines 13 should be r a > r b . It is to be noted that, in the present example, the sectional waveforms at the portions A and B are substantially similar as shown in FIG. 14(B). According to another such means, a sheet section extension ℓb of the posterior wave portion B per unit wavelength L of the sectional waveform should be greater than a sheet section extension ℓa of the anterior wave portion A. A "sheet section extension" denotes an actual total length of a sheet used for a unit wavelength, and in other words, the length of stepwise movement of the portion B should be increased. As a more particular such means, there is a solving means shown in FIG. 15. In this example, contrary to the example described above, waveforms of the portions A and B in a plane have substantially the same shapes (refer to FIG. 15(A)), but the sectional waveforms are different. In particular, as apparent from FIGS. 15 (B) to (D), the relationship between a curvature r a ' of the portion A and a curvature r b ' of the portion B in a sectional waveform should be r a ' < r b ', or a difference should be provided between the crests Wa and Wb. It is to be noted that the means for changing the width narrowing ratio is not limited to such two means as described above, and for example, the two means may be combined with each other, or a quite different technique may be adopted. Where such means are adopted, a reinforced corrugated body to be formed can be adjusted so that a predetermined low tensile force may be applied, upon roll forming of the reinforced corrugated body, substantially equally and uniformly to portions of the sheet at both of the waveforms of the anterior waves and posterior waves of the meandering corrugate. Accordingly, even if the speed of rotation of the forming rollers 23 is raised, occurrence of relaxation or of excess wrinkling at a portion of the posterior wave portions or occurrence of stretching distortion and operating difficulties such as a tearing damage at a portion of the anterior wave portions can be restricted. 〈Total Profile Requirements〉 Preferable profile requirements for corrugate lines are attained only after the two necessary conditions for the strength and the production described above are satisfied, and they are particularly as follows. The profile requirements are illustrated by a set of profile curves shown in the graph of FIG. 16, and the profile curve expression is represented as H/L = f i (D/N) . It is to be noted that the substantial meandering overlapping ratio D/L and the bent width w have no relationship to the curve expression. The profile curve expression stands independently of absolute values of the individual profile values H, L, D and N. In particular, the profile curve expression is composed of profile ratios and is a functional relationship in principle describing only a profile characteristic of the present corrugated body 11 and then is independent of structural strength and high or low workability of the corrugated body. More particularly, only one combination of H/L and D/N of variable values which satisfies the profile curve expression described above exists for one fixed value of the parameter variable constant i. For example, a combination of a value of the variable constant i and a value of the variable H/L decisively defines a value of the variable D/N. Also, a combination of a value of the variable constant i and value of the variable D/N decisively defines a value of the variable H/L, or else a combination of values of the variables H/L and D/N decisively defines a value of the constant i. In other words, the relationship is substantially that the values of H/L and D/N change proportionally when the value of i is changed. It is to be noted that the set of profile curves in FIG. 16 are drawn as a set of similar hyperbolas obtained by parallel movement, and only profile curves where the width narrowing ratio i is 5% ≤ i ≤ 20% are illustrated while profile curves for i < 5% and i > 20% outside the range are omitted. It is to be noted that the set of profile curves has been drawn by measuring variations of profiles, that is, the substantial amplitude ratio H/L and the substantial meandering ratio D/N, of various portions worked and formed from actual corrugated bodies having different substantial meandering ratios D/N, where the substantial amplitude ratio H/L = 0 while varying the width narrowing ratio i. Optimum ranges which simultaneously satisfy a substantial amplitude ratio and a width narrowing ratio among the profile requirements for structural strength and workability which are most important and essential in order to make practical use possible are such that a substantial amplitude ratio H/L is optimum at H/L = 0.7 and the optimum range thereof is limited to 0.4 ≤ H/L ≤ 1.4, while profile curves having an optimum width narrowing ratio i are limited to the range of 0 < i ≤ 10% (D/N). As a result, an optimum substantial meandering ratio D/N is limited to the range of 0 < D/N ≤ 0.35. A hatched area in the graph of FIG. 16 indicates the optimum ranges. Profile designing of corrugate lines of a reinforced corrugated body according to the present invention, profile designing of tooth-shaped ribs of a forming roller, and so forth can be performed efficiently using the present graph in which the optimum range of the profile in the profile curve set is shown. It is useful in an application, for example, to a method wherein, after optimum H/L and i are set in advance, D/N is determined and designed to enable a reinforced corrugated body which has both a high structural strength and an excellent workability, or to an automatic control system for a pre-corrugating roller (an apparatus for working a sheet in the form of a flat plate into a corrugated work sheet 24) which calculates and controls an i value which achieves the optimum H/L and D/N set in advance. It is to be noted that the profile curves apply regardless of the type of material of the work sheet. * Results of Experiments Three characteristic cases among many embodiments are described below. In the first case, a reinforced corrugated body was formed using a paper sheet such that, in the profile of the corrugate lines, the substantial amplitude ratio is H/L = 0.7; the substantial meandering ratio is D/N = 0.18; the substantial meandering overlapping ratio is D/L = 1.0; and the width narrowing ratio is i = 5%. The waveform in a plane is a smooth waveform consisting of continuous curves and the crest and bottom portions of the corrugate lines have a curved sectional shape. The reinforced corrugated body was obtained by roll forming with heating type forming rollers without any operating difficulty at a speed of 150 m or so per minute. The width pre-narrowing ratio ws 5% and the stretch strain ratio was β ≒ 0 upon roll forming. Thus, the reinforced corrugated body obtained has an ideal structure characterized in that it can be substantially developed topologically. Further, a reinforced composite corrugated body which was obtained by integrally applying two flat paper sheets to the opposite faces of the reinforced corrugated body was compared with a known corrugated board having an equal sheet material rib amplitude H 0 , an equal sheet material rib period L and an equal sheet material rib bending width w. The result obtained was that, while the amount of use of the sheet increased by 2% or so, the x direction maximum shearing strength increased by 50% or so and the x direction bending strength increased by 60% or so. In the second case, another reinforced corrugated body was formed using a paper sheet such that the substantial amplitude ratio of the corrugate lines is H/L = 0.7; the substantial meandering overlapping ratio is D/L = 1.0; the substantial meandering ratio is D/N = 0.24; and the width narrowing ratio is i = 8%. The meandering pattern of the corrugate lines has a smooth waveform in a plane forming continuous curves and the crest and bottom portions of the corrugate lines have a curved sectional shape. The reinforced corrugated body was obtained by roll forming by heating, type forming rollers without causing any operating difficulties at a speed of 100 m or so per minute. The width pre-narrowing ratio was 6.5% and the stretch strain ratio of the sheet was β ≒ 1.5% upon roll forming. Thus, the reinforced corrugated body obtained is rather difficult to be developed topologically, and the material strength of the work sheet in lateral direction deteriorated somewhat. Further, a reinforced composite corrugated body which was obtained by integrally applying two flat paper sheets to the opposite faces of the reinforced corrugated body was compared under the same conditions with the known corrugated board. As a result, it was confirmed that, while the amount of use of the work sheet increased by 3% or so, the x direction maximum shearing strength increased by 55% or so and the x direction bending strength increased by 75% or so. In the third case, a reinforced corrugated body was worked and formed by a similar roll forming method to that of the reinforced corrugated body of the first case, and a flat paper sheet was integrally applied to one face of the reinforced corrugated body formed from a paper sheet having a similar profile to obtain a single faced reinforced corrugated body. The reinforced corrugated body obtained in this manner was compared with a known single faced corrugated board under the same conditions as to the material of the sheet, corrugate rib amplitude H 0 , corrugate rib period L, corrugate rib bent width w and so forth. Excellent results confirmed that, while the amount of use of the sheet increased by 3% or so, the x direction bending strength increased by 220% or so. As seen in the above-mentioned first and second cases, since the increase in cost of a product as compared with a known corrugated board was less then 10% (the increase of material was less than 4% and the increase in production cost due to reduction of the roll forming speed was less than 6%), and the various structural strengths were increased by 50%, the value of the product, i.e. strength/cost is ≤ 150/110 = 1.36. Thus, because other performances are equal, an increase in product value greater than about 40% was realized. Meanwhile, in the third case, since the increase in cost of a product was restricted to 7% (the increase of material was less than 3% and the increase in the production cost was 4%), and the bending strength was increased by 220%, the value of the product, i.e. strength/cost is ≤ 320/107 = 2.99. Thus, because other performances are equal, a difference in product value greater than about 200% was realized. Subsequently, the single faced reinforced composite corrugated body (H/L = 0.5, D/L = 1.1 and D/N = 0.32) according to the present invention obtained in such a manner as described above was compared in strength with a conventional single faced corrugated board (H/L = 0.5) as shown in FIG. 18. Results of an examination of in-plane compression strength are shown in Table 1. As is apparent from Table 1, when a composite corrugated body which is used in the present invention is compared with a conventional single faced corrugated board, it is apparent that, while the in-plane compression strength in the y direction is substantially the same, the composite corrugated body has a strength in the x direction three or more times as high as that of the conventional single faced corrugated board. Results of an examination of out-of-plane compression strength are shown in Table 2, and from this table, it is apparent that the single faced reinforced composite corrugated body which is used in the present invention has an out-of-plane compression strength higher by almost twice compared to that of the conventional single faced corrugated board. Results of an examination of out-of-plane bending strength in a direction of a plane perpendicular to the x direction in FIGS. 1 and 17 are shown in Table 3. From this table, it is apparent that the single faced reinforced composite corrugated body according to the present invention has a very high bending strength which is about 22 times that of the conventional single faced corrugated board. Results of Examination of In-plane Compression Strength Single Faced Corrugated Board Composite Corrugated Body y Direction In-Plane Compression Strength 2.40 kgf 2.52 kgf Index of the Same 100 105 x Direction In-Plane Compression Strength 0.82 kgf 2.50 kgf Index of the Same 100 350 Specimen: BF: K180-Scp125 Method of Examination: Static pressurizing examination by column crush testing machine Results of Examination of Out-of-Plane Compression Strength Single Faced Corrugated Board Composite Corrugated Body Vertical Direction Out-of-Plane Compression Strength 1.51 kgf 2.96 kgf Index of the Same 100 194 Specimen: The same as in Table 1 Method of Examination: Static pressurizing examination by column crush testing machine Results of Examination of Out-of-Plane Bending Strength Conventional Product Composite Corrugated Body y Direction Out-of-Plane Bending Strength 220 kgf 227 kgf Index of the Same 100 103 x Direction Out-of-Plane Bending Strength 8 kgf 178 kgf Index of the Same 100 2225 Specimen: The same as in Table 1 Method of Examination: Static pressurizing examination by bending testing machine of 2-point supporting type As is apparent from the foregoing description, it can be said that the single faced reinforced composite corrugated body is very superior to the conventional single faced corrugated board with respect to various structural strengths.

Claims: A reinforced composite corrugated body comprising: a corrugated body formed of a sheet material having formed therein corrugate lines including, with respect to an x-y-z coordinate system, ridges and grooves formed alternately in an x direction and located in respective planes spaced in a z direction and parallel to an x-y plane, each said ridge and groove of each said corrugate line having a smooth meandering waveform in a y direction as viewed in said x-y plane, and said ridges and grooves defining a smooth meandering sectional waveform in said x direction as viewed in an x-z plane; said sectional waveform having an amplitude H in said z direction and a wavelength L in said x direction defining a substantial amplitude ratio H/L; said meandering waveform of each said corrugate line having an amplitude D in said x direction and a wavelength N in said y direction defining a substantial meandering ratio D/N; said corrugate lines defining a substantial meandering overlapping ratio D/L; said corrugate lines having a width narrowing ratio i, equal to an amount of contraction of said sheet material in said y direction after formation therein of said corrugate lines to a width in said y direction of said sheet material in the form of a flat sheet before formation therein of said corrugate lines; said waveform of each said corrugate line having crest and bottom portions spaced in said y direction, each said crest and bottom portion being curved or chamfered and having a relatively small dimension in said y direction; and a flat liner adhered to at least one opposite face of said corrugated body; characterised in that: said width narrowing ratio i, said substantial amplitude ratio H/L and said meandering ratio D/N substantially satisfying a profile curve relationship such that the values of H/L and D/N change proportionally when i is changed; said substantial amplitude ratio H/L is within the limits 0.4 ≤ H/L ≤ 1.4; said substantial meandering ratio D/N ≤ 0.35; said width narrowing ratio i ≤ 8% plus β, wherein β is a % stretch limit of the sheet material in the y-direction beyond which the material strength is decreased by at least 30%; and said substantial meandering overlapping ratio D/L ≥ 0.5. A reinforced composite corrugated body as claimed in claim 1, wherein said crest and bottom portions of said waveforms of said corrugate lines are entirely smoothly curved. A reinforced composite corrugated body as claimed in claim 1, wherein said meandering overlapping ratio D/L ≥ 1.0. A reinforced composite corrugated body as claimed in claim 1, wherein said width narrowing ratio i at a portion of each said corrugate line on an anterior wave side thereof is smaller than that at a posterior wave side thereof. A reinforced composite corrugated body as claimed in claim 1, wherein said substantial amplitude ratio H/L is approximately 0.7. A method of producing a reinforced composite corrugated body, said method comprising: forming a corrugated body by forming in a sheet material corrugate lines including, with respect to an x-y-z coordinate system, ridges and grooves formed alternately in an x direction and located in respective planes spaced in a z direction and parallel to an x-y plane, each said ridge and groove of each said corrugate line having a smooth meandering waveform in a y direction as viewed in said x-y plane, and said ridges and grooves defining a smooth meandering sectional waveform in said x direction as viewed in an x-z plane; forming said sectional waveform to have an amplitude H in said z direction and a wavelength L in said x direction defining a substantial amplitude ratio H/L such that 0.4 ≤ H/L ≤ 1.4; forming said meandering waveform of each said corrugate line to have an amplitude D in said x direction and a wavelength N in said y direction defining a substantial meandering ratio D/N ≤ 0.35; forming said corrugate lines to define a substantial meandering overlapping ratio D/L ≥ 0.5; forming said corrugate lines to have a width narrowing ratio i, equal to a coefficient of contraction of said sheet material in said y direction after formation therein of said corrugate lines to a width in said y direction of said sheet material in the form of a flat sheet before formation therein of said corrugate lines, ≤ 8% plus β wherein β is a stretch limit of the sheet material in the y-direction beyond which the material strength is decreased by at least 30%; forming said waveform of each said corrugate line to have crest and bottom portions spaced in said y direction, each said crest and bottom portion being curved or chamfered and having a relatively small dimension in said y direction; forming said width narrowing ratio i, said substantial amplitude ratio H/L and said meandering ratio D/N to substantially satisfy a profile curve relationship such that the values of H/L and D/N change proportionally when i is changed; and adhering a flat liner to at least one opposite face of said corrugated body. A method as claimed in claim 6, comprising forming said crest and bottom portion of said waveforms of said corrugate lines to be entirely smoothly curved. A method a claimed in claim 6, comprising forming said corrugate lines to define said substantial meandering overlapping ratio D/L ≥ 1.0. A method as claimed in claim 6, comprising forming said corrugated lines such that said width narrowing ratio i at a portion of each said corrugate line on an anterior wave side thereof is smaller than that at a posterior wave side thereof. A method as claimed in claim 6, comprising forming said sectional waveform to define said substantial amplitude ratio such that H/L is approximately 0.7.

Inventors: ICHIKAWA HIROO, ICHIKAWA, HIROO
Applicants: ICHIKAWA HIROO, ICHIKAWA, HIROO
Application year: 1989
Main classification: B32B3
IPC codes: E04C2, B65D65, B32B3