[go: up one dir, main page]

GB2241714A - Lightweight cylinder construction - Google Patents

Lightweight cylinder construction Download PDF

Info

Publication number
GB2241714A
GB2241714A GB9027684A GB9027684A GB2241714A GB 2241714 A GB2241714 A GB 2241714A GB 9027684 A GB9027684 A GB 9027684A GB 9027684 A GB9027684 A GB 9027684A GB 2241714 A GB2241714 A GB 2241714A
Authority
GB
United Kingdom
Prior art keywords
cylinder
module
modules
modular
cylindrical
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.)
Withdrawn
Application number
GB9027684A
Other versions
GB9027684D0 (en
Inventor
John Whiteley
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hollingsworth GmbH
Original Assignee
Hollingsworth GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hollingsworth GmbH filed Critical Hollingsworth GmbH
Publication of GB9027684D0 publication Critical patent/GB9027684D0/en
Priority to US07/664,080 priority Critical patent/US5265750A/en
Priority to CN91102102A priority patent/CN1056319A/en
Priority to KR1019920702165A priority patent/KR920704049A/en
Priority to BR919106123A priority patent/BR9106123A/en
Priority to EP19910301792 priority patent/EP0446006A1/en
Priority to PCT/GB1991/000335 priority patent/WO1991014117A1/en
Priority to JP3505407A priority patent/JPH07509043A/en
Publication of GB2241714A publication Critical patent/GB2241714A/en
Priority to US07/915,220 priority patent/US5267388A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01GPRELIMINARY TREATMENT OF FIBRES, e.g. FOR SPINNING
    • D01G15/00Carding machines or accessories; Card clothing; Burr-crushing or removing arrangements associated with carding or other preliminary-treatment machines
    • D01G15/02Carding machines
    • D01G15/12Details
    • D01G15/14Constructional features of carding elements, e.g. for facilitating attachment of card clothing
    • D01G15/16Main cylinders; Breasts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16JPISTONS; CYLINDERS; SEALINGS
    • F16J10/00Engine or like cylinders; Features of hollow, e.g. cylindrical, bodies in general

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Preliminary Treatment Of Fibers (AREA)
  • Lining And Supports For Tunnels (AREA)

Abstract

A modular cylinder (e.g. textile cards) comprises a plurality of (24) interconnected modules 1 arranged in a circular array. Each module is hollow and has spaced wall portions 2, 3. Each includes a tongue 6 to engage a groove 7 of its neighbour and each either has a camming ramp 9 to engage a camming ramp 8 of its neighbour, or a filler rod 22 inserted between adjacent modules at each interface. The cylinder includes end plates. Where ramps 8, 9 are provided. (n- 1) of the modules are placed into engagement to define an almost complete cylinder and then strained in a radially outward direction to provide gap for the final module 1 which is inserted longitudinally into the gap. Where rods 22 are used, all of the n modules are loosely assembled and then rods 22 are inserted to pre-stress the cylinder. The portion 2 of each module has a biconvex cross-section whereby surface 13 thereof defines a sector of the cylindrical surface of the cylinder but the bonding axis of section 2 is straight and parallel to the tangent to surface 13 at the centre of section 2. At least one reinforcing hoop may be placed inside the cylinder to increase its rigidity. <IMAGE>

Description

:2 ?- -el 3- -7 -1- -G 1 LIGHTWEIGHT CYLINDER CONSTRUCTION The present
invention relates to a lightweight cylinder construction which has structural rigidity but without being made from the solid.
Conventionally cylinders, particularly those used in heavy machinery such as textile cards, are produced from the solid, either by being cast in the form of a solid cylindrical metal block and possibly having been machined away to leave a hollow construction, or by having been cast in hollow form and subsequently machined internally and externally for finishing.
Previous efforts towards reducing the weight of such cylinders has involved the choice of lightweight metals for the casting, but there is a limit as to the weight reduction possible because of the eventual lack of structural rigidity which is necessary for precision equipment (for example cards where the clearance between the fine points on the card clothing wire on the cylinder and those of any cooperating concave carding plate and/or flats is critical to optimum uniformity of the carding action obtained).
In accordance with the first aspect of the present invention, there is provided a hollow cylinder comprising end plates and a hollow cylindrical member formed of a plurality of interengaging modules each extending parallel to the axis of said cylinder and assembled in side-by-side relationship in a circular array. each said module having spaced wall portions which, in the assembled configuration of the cylinder, define at least part of the radially inner faces of the modular cylinder and the radially outer faces thereof.
A second aspect of the present invention provides a module defining a segment of a modular cylinder for assembly with a plurality of identical modules in a circular array to define said modular cylinder, said module being of hollow form manufactured by extrusion and including at one side at 2 least one tongue and at the other side at least one socket, positioned so that the or each tongue of one said module can engage a respective socket of an adjacent said module, and the various modules being provided with radially outer abutment surfaces which ensure that in the assembled condition of a set of said modules in an array occupying a full circle the radially outer panels of the modules are in compression and the radially inner panels of the modules are in tension.
Preferably the modules may be extruded with open- ended geometry, and more preferably end plates may be provided for butting up against the ends of the cylindrical array of assembled modules for the purposes of defining end walls of the cylinder.
Conveniently each of the modules may include all the means necessary for joining it to the adjacent module in the array. More conveniently each module may be identical to its neighbours, in which case one possibility is for the module to have a projecting tongue at one side which conforms with a socket on the other side whereby the tongue of each module may engage the socket of its neighbour(s).
Where such tongue and socket engagement is provided, each module may include can means for cooperating with cam means on its neighbouring module(s) for driving the tongue firmly into engagement with the socket.
Advantageously each said module may have along each o. f two opposite edges close to said radially outer panel a longitudinal recess such that the recess of one said edge will register with the recess of the other edge of an adjacent module, said recesses extending.right up to an end of said module.
Preferably the modules are all shaped such that in the assembled configuration of the modular cylinder, the cylindrical external surface of the cylinder is at a region where the modules are all in compression, and at the radially inwardly facing surface of the modular cylinder the f 3 relevant portion of the module is in tension measured in the peripheral direction. This latter arrangement of the compression and tension of the assembled modular cylinder is particularly advantageo us in the case of a textile carding cylinder which is subsequently clad with card clothing wire tending to bind around the external cylindrical surface of the cylinder and hence to impose additional compressive stress on the external surface of the cylinder.
Advantageously the part of each module which 10 defines the cylindrical outer surface of the assembled is modular cylinder may have a biconvex cross-section, resulting in the neutral axis of bending of that wall of the module being straight as opposed to being convex to follow the cylindrical contour of the modular cylinder.
A third aspect of the present invention provides a method of assembling a modular cylinder consisting of n identical modules in engagement in a cylindrical array, comprising assembling together (n - 1) of said modules and leaving a gap for the final module, straining said array of (n - 1) modules to increase the width of the gap remaining for the final module sufficiently to allow engagement of the final module with its immediate neighbours to either side of the gap, sliding the final module longitudinally into the gap until it is in register with the (n - 1) modules of the array, and then relaxing the strain.
A fourth aspect of the invention provides a method of assembling a modular cylinder consisting of n identical modules in engagement in a cylindrical array, comprising assembling together the n-modules in a loose-fitting cylindrical configuration, and stressing said ass emb ly by inserting filler means between the adjacent surfaces of the modules at each interface between the adjacent modules, said filler means fitting between the sidewalls of the modules near the radially outer panels defining the exterior of the cylinder, whereby insertion of the final said filler means stresses the cylinder in the required manner.
1 4 In order that the present invention may more readily be understood the following description is given, merely by way of example, with reference to the accompanying drawings, in which:
Figure 1 is a transverse sectional view of a cylinder module in accordance with the present invention; Figure 2 is a view, on a reduced scale as compared with Figure 1, showing three of the modules assembled in a part-cylindrical configuration; Figure 3 is a still further reduced scale drawing showing the finished cylinder; Figure 4 shows a view corresponding to Figure 2, but illustrating a modified form of the modules forming the cylinder; Figure 5 is a diagrammatic view illustrating the method of assembling the cylinder comprising the modules of Figures 1 and 2; and Figure 6 is a view corresponding to Figure 5, but showing the assembling of a cylinder comprising the modules of Figure 4.
Figure 1 shows a hollow extruded module 1 which is one of twenty four identical such modules to be used to assemble a hollow cylinder 18 shown in Figure 3, in this case for use as the main carding cylinder of a textile fibre card.
The module is generally in the form of a boxsection bean having an outer wall 2 which will define the exterior of the cylinder, and an inner wall 3 which will be facing radially inwardly of the assembled modular cylinder, these inner and outer walls being joined.by generally radially extending sidewalls 4 and 5.
In the preferred embodiment the "beam" is closed except at its ends, but in practice any alternative construction providing an external surface of a desired configuration, and providing the necessary strength for the cylinder may be used.
In order to assemble the modules together, each has a tongue 6 at one end of the inner wall panel 3 and a suitably arranged recess 7 at the opposite end of that same wall panel 3, for the purposes of allowing the tongue 6 of one module 1b to engage in the recess or socket 7 of its immediate neighbour la, and so on. as shown in Figure 2.
In order to ensure that the tongue 6 engages firmly in the socket or recess 7, the end of the sidewall 4 remote from the tongue 6 includes a camming ramp 8 which engages with a suitably positioned camming ramp 9 on the end of the other sidewall 5 remote from the socket 7. This has the result that when two adjacent modules la and 1b are pressed together by a force acting in the direction of the arrow F of Figure 1 the camming engagement of the ramps 8 and 9 causes the tongue 6 to press firmly into the socket 7.
In order to ensure that there is no loose fit of the modules one against another, the profile of the tongue 6 is carefully chosen to conform to the profile of the socket 7 to avoid lateral slapping even in the unstressed condition of the modules.
In order to impose a circumferential compression on the assembled modular cylinder, the end of the sidewall 5 remote from the socket 7 has a projection 10 which bears against a shoulder 11 at the end of the other sidewall 4 remote from the tongue 6, as each two adjacent modules 1-a and 1b are pressed against one another in the circumferential direction.
By suitable dimensioning of the distance measured in the circumferential direction between the rightwardly facing end of the projection 10 and the cooperating part of the shoulder 11, on the one hand, and the distance between centres of the tongue 6 and of the recess or socket 7, on the other hand, it is possible to ensure that in the assembled condition the wall 2 is maintained in compression while the wall 3 is maintained in tension. This is particularly advantageous when the assembled modular f 6 cylinder is to be wound around with a binding medium such as card clothing wire in the case of a carding cylinder.
In order to provide the necessary strength and buckling resistance to the radially outer wall panel 2 of each module, the panel 2 is preferably shaped as shown in Figure 1 in that it has a generally inwardly convex inner surface 12 which complements the outwardly convex surface 13 defining the external surface of the assembled modular cylinder, in such a way that, despite the cylindrical exterior of its surface 13 the neutral axis of bending of that panel 2 is substantially straight and is in this'case parallel to the tangent to the external surface 13 of that module at the mid-point of the wall 2.
Each module optionally includes a pair of bent ribs 14 defining between them a generally circular recess 15 for a purpose to be described therebelow.
The operation of assembling the modules 1 to form a hollow cylinder with the ability to withstand structural loading is as follows:- Initially the various modules, such as la, lb and lc in Figure 2, are placed in a suitable configuration (for example by standing them upright on the floor surface with one end of each module engaging the floor, or by mounting then on a suitable former ring or within a former socket) and the tongue 6 of one module 1b is engaged with the socket 7 of its neighbour la, and so on.
After twenty three of the twenty four modules have been assembled in this way, normally -simply by positioning each one of them so that it engages with its tongue in the groove of its neighbour, the almost complete cylindrical structure is then deformed by applying an outward strain at the ends of the array which will receive the sidewalls 4 and 5 of the missing module. Ideally some means, such as spreader-23 in Figure 5, are provided for ensuring that the bending moment applied to the almost assembled modular cylinder is distributed uniformly over the entire cylinder.
1 7 For this purpose there may be load spreading pads 24 or other similar means to apply a relatively uniform deflection around the peripheral direction of the modular cylinder.
While the almost complete cylinder is thus strained, the final module is placed in position by sliding it axially into the gap remaining, whereby its tongue 6 slides along the socket or recess 7 of one of its neighbours and its socket or recess 7 slides along the tongue 6 of the other neighbouring module until the final module is correctly aligned side-by-side with the other twenty three.
At this stage, release of the "opening" bending moment on the other twenty three modules will allow the twenty fourth module to take its share of the load which will be evenly distributed around the modular cylinder and hence the resulting engagement of the ramps 8 and 9 of the final module with its immediate neighbours will help to ensure a tight-fit of the tongues 6 and sockets 7 around the modular cylinder.
If desired, one or other or both of the tongue 6 and the socket 7 may have a slightly tapering profile in order to provide some form of wedging action as the tongue 6 is driven into a cooperating socket 7 as a result of the camming engagement of the ramps 8 and 9.
As an alternative to the preferred tongue and socket interconnection of the modules 1 illustrated, the modules may instead be provided with cooperating dovetailed formations.
Figure 5 shows a suitable tool 23 for spreading the almost complete modular cylinder as, for example, comprising a Y-shaped spreader having the stem 24 of the Y engaging the interior of the almost complete. modular cylinder (for example adjacent modules numbers 11 and 12 (where module number 1 is at one side of the gap and module number 23 is at the other side of the gap to receive module number 2C), and then the branches 25 and 26 of the Y may engage the radially inward surface of the modular cylinder adjacent 8 modules numbers 1 and 23 to apply a radial expansion force F, thereagainst. A suitable hydraulic or screw jack 27 on the stem of the Y can be operated to spread the branches of the Y (preferably by having the branches pivotally connected to the stem of the Y at 28). Load spreading pads 24 are provided on the stem and branches. Preferably a transverse radial compression is applied (for example at modules 6 and 18 in this 24 module example) to exert a diametral compressive force F2 to cause the faces of modules 1 and 23 to be presented at the best orientation to receive module 24 readily.
Once the modular cylinder has been assembled in this way, end plates may be attached. For example, in the embodiment shown in Figure 1, the end plate may have twenty four clearance holes drilled near its periphery, each one receiving a suitable bolt or screw which penetrates the clearance hole and bites into the socket 15 between the bent ribs 14 on the inward side of the outer panel 2 of the module 1 (Figure 1). For this purpose the sockets 15 are preferably tapped, by use of a suitable guiding fixture, before assembly of the modules to form the cylinder.
The centre of each end plate may provide means for mounting a bearing or stub axle on the cylinder, for the purposes of mounting the finished modular cylinder for rotation.
Although the above description refers to a modular cylinder comprising twenty four identical modules, any smaller or larger number of modules may be chosen, but of course the shape of each module will differ with such differing numbers of modules, even if the same general operating principle of the modules is followed.
Figure 1 shows that there is a radially inwardly facing part-cylindrical surface 16 of each module which can engage an inner former ring, and that the main curved radially inwardly facing panel 3 of each module diverges from the cylindrical configuration of the finished modular 9 is cylinder as one moves away f rom the socket 7 and towards the tongue 6 of the module 1. The panels 3 are deliberately curved in order to allow the effect of straightening them, when the almost complete modular cylinder is strained by application of a bending moment to open the gap for the last module to be inserted, to impart extra flexibility for the straining to be facilitated in the appropriate direction of bending of the cylinder. The curvature of the panel 3 is generally spiral on the cross-section shown in Figures 1 and 2.
The general cylindrical notional cylinder of'which the surface 16 forms part is illustrated in chain-dotted lines at 17. This will coincide with the exterior of the former ring 17, where fitted.
Figure 2 shows the assembly of three of the modules 1 of Figure 1 in engagement with one another during the early stages of assembling a said cylinder 18. This clearly shows the irregular radially inner profile, resulting from the staggering of the tongues 6 and recesses 7, and the generally regular radially outer profile defined by the surfaces 13 of the three modules illustrated.
Figure 4 shows an embodiment of the cylinder module which is generally similar to that of Figures 1 to 3 but which has additional hemi-cylindrical recesses 20 and 21 along the side edges adjacent the radially outer panel 13 of the module. As shown in the central module in Figure 4, the left-hand hemi-cylindrical recess is referenced 20 and the right-hand is referenced 21 such that, when the modules are assembled, the recess 21 to the right of the central module is in register with the other (left-hand) recess 20 of the next adjacent module on the right, and the left-hand recess 20 is in register with the other (right-hand) recess 21 of the next adjacent module on the left.
Although the recesses are shown as being hemicylindrical, they could be of any suitable form which can 1 1 receive a filler which in the present embodiment is in the form of a cylindrical rod 22. With a cylindrical rod it is possible for the recesses 21 and 22 to be noncylindrical but, for example, V-shaped. With other cross- sections of filler instead of the cylindrical rods 22 a different profile of recess 20 and 21 altogether may be used.
In order to assist insertion of the filler rods 22, they have one end tapered to assist in threading them into the registered recesses 20 and 21.
Another difference between the modules of Figure 4 and those of Figures 1 to 3 is that there is no evidence of the bent ribs 14 to assist in clamping end plates to the modular cylinder. However, some other form of securing of the end plates may be incorporated. For example, the filler rods 22 could be used to mount end plates by having suitable turned-down ends to engage in holes drilled in the end plates.
The method of assembling the modular cylinder with the modules of Figure 4 is somewhat different from that of Figures 1 to 3, and is as follows:- The entire assembly of modules is laid out in a cylindrical configuration with the modules standing up on end and the various tongues 6 and grooves 7 interengaged. With the radially outermost panels 13 of the modules arranged so that their edges almost touch at the interface between one module and the next the fit is relatively loose but the cylindrical configuration can be achieved without difficulty, even when the last module of the set is inserted into the available space. It will be recalled that with the embodiment of Figures 1 to 3 the insertion of the last module required the entire assembly of the previous (n-1) modules to be strained to make space for it.
Once the various modules have all been loosely assembled as described above, the various filler rods 22 1 z 1 1 11 are driven into the gaps defined by the registered recesses (in this case the cylindrical openings defined by the two hemi-cylindrical recesses 20 and 21 at each interface between modules).
In order to facilitate insertion of the rods, the loosely assembled cylinder may be. distorted into an elliptical configuration either by expanding a diameter from within the cylinder (in order to cause that diameter to tend to become the major axis of an ellipse, or by contracting a diameter from outside to cause that contracted diameter to become the minor axis of an ellipse. When such an elliptical configuration has been achieved, rods are inserted around the ends of the major diameter, where the radius of curvature of the ellipse is smallest and the gaps between the surfaces 20 and 21 are widest. If a single "elliptical" deformation is not enough to facilitate insertion of all the rods, then this process may be repeated several times with different diameters chosen for contraction or expansion, in order to shift the regions of smallest radius of curvature of the assembly of segments around the array so as to generate the tightest curvature at a region where the rods have not yet been inserted.
By way of example, Figure 6 shows an outward deformation force F3 applied at the 9 o'clock and 3 o'clock positions of the cylinder, so as to generate tightest curvature around those points of application of the internal force to facilitate insertion of the rods locally.
Alternatively, a radially Inward force may be applied, for example at the 9 o'clock and 3 o'clock positions, in order to contract that diameter and to generate the tightest curvature at the 12 o'clock and 6 o'clock positions to facilitate insertion of the rods there.
Driving in the last rod will be difficult, but 1 12 will be helped by virtue of the optional tapering of the leading end of the filler rod this can be achieved without difficulty.
Once the various filler rods 22 have been inserted, the radially outer panels 13 will all have been placed in compressive stress and it has been found that this is the configuration in which the cylinder preserves its structural integrity most reliably.
In the case of a carding cylinder manufactured by the method of the present invention, the outer panel 2 of each module will be thick enough to provide for the possibility of machining of the radially outwardly facing surface of the assembled modular cylinder 18 for the purposes of allowing precise dimensioning of the finished cylinder and for dressing the cylinder to receive the necessary card clothing wire.
As indicated above, the material used for each extruded module 1 is preferably aluminium or an aluminium alloy, and the hollow box-beam type construction allows a very lightweight module to be formed such that the engagement of the designed number of such modules to form a cylinder, with a radially outer compressive stressing and a radially inner tensile stressing of the finished modules, allows a particularly impressive structural integrity of the finished modular cylinder to be obtained despite the extreme light weight of the cylinder as compared with the conventional carding cylinder using a hollow cylindrical casting which has a radial distance substantially equal to the length of a sidewall 4 or 5 of the module 1.
If desired, such a modular cylinder may be reinforced by at least one radially inwardly arranged reinforcement hoop (not shown) which has its cylindrical exterior conforming to the notional cylindrical interior 17 of the modular cylinder, and in this way the modules can be braced against radial deformation in that the -7 13 tension in the inwardly facing module panels 3 of the cylinder 18 can be responsible for applying compression to the exterior of the reinforcement hoop, provided appropriate measures are taken during assembly to ensure that there is a tight fit upon relaxation of the modular cylinder 18 and the reinforcement hoop.
If absolutely necessary, more than one such reinforcement may be employed.
An alternative or additional reinforcement mechanism relies on the injection of a rigid polyurethane foam into the cavities bounded by each module 1.
14 C L A 1 M S 1. A hollow cylinder comprising end plates and a hollow cylindrical member formed of a plurality of interengaging modules each extending parallel to the axis of said cylinder and assembled in side-by-side relationship in a circular array, each said module having spaced wall portions which, in the assembled configuration of the cylinder, define at least part of the radially inner faces of the modular cylinder and the radially outer faces thereof.
2. A cylinder according to claim 1, wherein each module is of extruded metal construction.
3. A cylinder according to either of the preceding claims, wherein each module has a generally rectangular cross-section defining a box-section beam.
4. A cylinder according to any one of the preceding claims, wherein each module includes the necessary means for joining it to its neighbouring modules in the cylinder.
5. A cylinder according to any one of the preceding claims, and including means for stressing the modules to have the radially outer wall of the modular cylinder stressed in compression and the radially inwardly facing wall of the modular cylinder stressed in tension.
6. A cylinder according to claim 5, wherein the means for stressing the modules comprise filler means able to be inserted at each interface between adjacent modules, near the radially outer wall of the modular cylinder, and adapted to cooperate with.the filler means of the other interfaces whereby insertion of the last filler means places the entire cylinder under the desired stress.
7. A module defining a segment of a modular cylinder for assembly with a plurality of identical modules in a circular array to define said modular f cylinder, said module being of hollow form manufactured by extrusion and including at one side at least one tongue and at the other side at least one socket, positioned so that the or each tongue of one said module can engage a respective socket of an adjacent said module, and the various modules being provided with radially outer abutment surfaces which ensure that in the assembled condition of a set of said modules in an array occupying a full circle the radially outer panels of the modules are in compression and the radially inner panels of the modules are in tension.
8. A module according to claim 7, wherein the or each said tongue projects in a direction generally radially of the circular cylinder segment defined by said module and the or each recess is open in the same generally radial direction, and including camming means at the radially outer parts of said module on the outwardly facing surface of the sidewalls thereof, whereby pressing two adjacent modules circumferentially against one another with the or each tongue of one engaged in the respective groove of the other causes camming inter-engagement between said camming means to thrust the tongue more firmly into said recess.
9. A module according to claim 8, wherein at the radially outer part of each modular segment each module has a projection at one side and a shoulder at the other side for abutting engagement with the projection of the adjacent module.
10. A module according to claim 8, wherein recesses are formed along said outwardly facing surface of the sidewalls of the module, whereby the recess of a first sidewall of one module is in register with the recess of the second sidewall of an adjacent identical module in the assembled condition, and where the camming means comprise filler means adapted to be inserted in said recesses.
1 16 11. A module according to any one of claims 7 to 10, wherein the radially outer part of the cylinder segment defined by the module coincides with a panel of the box beam-like module, said panel having a biconvex form whereby the neutral axis of bending of said panel considered in a transverse cross-section through the module is rectilinear and is generally parallel to a tangent to the module at the mid-point of said panel between the two sides of the module.
12. A module according to any one of claims 7 to 11, and including on the interior of said module a pair of bent ribs turned towards one another to define therebetween a generally circular recess for engagement with a respective bolt or screw to secure an end plate in place on the module.
13. A module according to any one of claims 7 to 11, wherein the radially inner panel of the module is curved about an axis extending parallel to the longitudinal axis of a cylinder to be formed of several such modules.
14. A module according to claim 13, wherein the curvature is generally spiral in cross-section.
15. A module according to any one of claims 7 to 14, wherein the hollow centre of the module is filled with rigid polyurethane foam.
16. A modular cylinder according to any one of claims 1 to 6, or a cylinder constructed from a plurality of modules according to any one of claims 7 to 15, and including at least one reinforcement ring as a tightfit within the cylinder and engaging the radially inner surface thereof at a location between the ends of each module.
17. A method of assembling a modular cylinder consisting of n identical modules in engagement in a cylindrical array, comprising assembling together (n - 1) of said modules and leaving a gap for the final module, 8 r 17 straining said array of (n - 1) modules to increase the width of the gap remaining for the final module sufficiently to allow engagement of the final module with its immediate neighbours to either side of the gap, sliding the final module longitudinally into the gap until it is in register with the (n - 1) modules of the array, and then relaxing the strain.
18. A method according to claim 17. wherein said radial strain is applied to the almost complete array of (n - 1) modules by application of a deforming jack in the interior of the array of (n - 1) modules to engage modules adjacent either side of the gap remaining for the last module.
19. A method according to claim 17 or 18, and is including the step of applying diametral contraction along a diameter which extends substantially perpendicular to a diameter which in the finished configuration of the cylinder will intersect the last installed module.
20. A method of assembling a modular cylinder consisting of n identical modules in engagement in a cylindrical array, comprising assembling together the n-modules in a loose-fitting cylindrical configuration, and stressing said assembly by inserting filler means between the adjacent surfaces of the modules at each interface between the adjacent modules, said filler means fitting between the sidewalls of the modules near the radially outer panels defining the exterior of the cylinder, whereby insertion of the final said filler means stresses the cylinder in the required manner.
21. A method according to claim 20, wherein the modules all include recesses in the external surfaces of their sidewalls adjacent said radially outer panel of each module, and said filler means comprise cylindrical rods adapted to be driven into the space between registering said recesses at each interface.
r 18 22. A method according to claim 20, wherein each of said cylindrical rods has a tapered end to facilitate insertion into said spaces.
23. A method according to any one of claims 20 to 22 including deforming the cylinder of loosely assembled segments into an elliptical configuration and inserting said filler means at the regions of smallest radius of curvature of the ellipse, i.e. in the vicinity of the ends of the major axis of the ellipse.
24. A method according to claim 23, comprising deforming the loosely assembled cylindrical array into an ellipse by application of a radially outward force to expand a diameter of the cylindrical array to form the major axis of an elliptical array.
25. A modular cylinder substantially as hereinbefore described with reference to, and as illustrated in, the accompanying drawings.
26. A module for a cylinder, substantially as hereinbefore described with reference to, and as illustrated in, Figure 1 of the accompanying drawings.
27. A method of assembling a modular cylinder, substantially as hereinbefore described with reference to Figures 1 to 3 and 5 of the accompanying drawings.
28. A method of assembling a modular cylinder, substantially as hereinbefore described with reference to Figures 4 and 6 of the accompanying drawings.
2 1 R Amendments to the claims have been filed as follows 1. A hollow cylinder comprising end plates and a hollow cylindrical member formed of a plurality of hollow modules each extending parallel to the axis of said cylinder and assembled in side-by-side relationship in a circular array, each said module having spaced wall portions which, in the assembled configuration of the cylinder, define at least part of the radially inner faces of the modular cylinder and the radially outer faces thereof, and further side wall portions having interengaging hook portions to engage the side wall portions of the next adjacent modules in the array; and including means for stressing the modules in said array.
2. A cylinder according to claim 1, wherein each module is of extruded metal construction.
3. A cylinder according to either of the preceding claims, wherein each module has a generally rectangular cross-section defining a box-section beam.
4. A cylinder according to any one of the preceding claims, wherein said means for stressing the modules leaves the radially outer wall of the modular cylinder stressed in compression and the radially inwardly facing wall of the modular cylinder stressed in tension.
5. A cylinder according to claim 4, wherein the means for stressing the modules comprise f iller raeans able to be inserted at each interface between adjacent modules, near the radially outer wall of the modular cylinder, and adapted to cooperate with the filler means of the other interfaces whereby insertion of the last filler means places the entire cylinder under the desired stress.
6. A module defining a segment of a modular cylinder for assembly with a plurality of identical modules in a circular array to define said modular cylinder, said module being of hollow form manufactured 9L 0 by extrusion and including at one side at least one tongue and at the other side at least one socket, positioned so that the or each tongue of one said module can engage a respective socket of an adjacent said module, and the various modules being provided with radially outer abutment surfaces which ensure that in the assembled condition of a set of said modules in an array occupying a full circle the radially outer panels of the modules are in compression and the radially inner panels of the modules are in tension.
7. A module according to claim 6, wherein the or each said tongue projects in a direction generally radially of the circular cylinder segment defined by said module and the or each socket is open in the same is generally radial direction, and including camming means at the radially outer parts of said module on the outwardly facing surface of the sidewalls thereof, whereby pressing two adjacent modules circumferentially against one another with the or each tongue of one engaged in the respective groove of the other causes camming inter- engagement between said camming means to thrust the tongue more firmly into said recess.
8. A module according to claim 7, wherein said radially outer abutment surfaces comprise, at the radially outer part of each module, a projection at one side and a shoulder at the other side for abutting engagement with the projection of the adjacent module.
9. A module according to claim 7, wherein said radially outer abutment surfaces comprise recesses formed along said outwardly facing surface of the sidewalls of the module, whereby the recess of a first sidewall of one module is in register with the recess of the second sidewall of an adjacent identical module in the assembled condition, and including filler means adapted to be inserted in said recesses.
10. A module according to any one of claims 6 to 1 9L 1 9, wherein the radially outer part of the cylinder segment defined by the module coincides with a panel of the box beam-like module, said panel having a biconvex form whereby the neutral axis of bending of said panel considered in a transverse cross-section through the module is rectilinear and is generally parallel to a tangent to the module at the mid-point of said panel between the two sides of the module.
11. A module according to any one of claims 6 to 10, and including on the interior of said module a pair of bent ribs turned towards one another to define therebetween a generally circular recess for engagement with a respective bolt or screw to secure an end plate in place on the module.
12. A module according to any one of claims 6 to 10, wherein the radially inner panel of the module is curved about an axis extending parallel to the longitudinal axis of a cylinder to be formed of several such modules.
13. A module according to claim 12, wherein the curvature is generally spiral in cross-section.
14. A module according to any one of claims 6 to 13, wherein the hollow centre of the module is filled with rigid polyurethane foam.
15. A modular cylinder according to any one of claims 1 to 5, or a cylinder constructed from a plurality of modules according to any one of claims 6 to 14, and including at least one reinforcement.ring as a tight fit within the cylinder and engaging the radially inner surface thereof at a location between the ends of each module.
16. A method of assembling a modular cylinder consisting of n identical modules according to any one of claims 6 to 15 in engagement in a cylindrical array, comprising assembling together (n - 1) of said modules and leaving a gap for the final module, straining said r 12 array of (n 1) modules to increase the width of the gap remaining for the final module sufficiently to allow engagement of the final module with its immediate neighbours to either side of the gap, sliding the final nodule longitudinally into the gap until it is in register with the (n - 1) modules of the array, and then relaxing the strain.
17. A method according to claim 16, wherein said radial strain is applied to the almost complete array of (n - 1) modules by application of a deforming jack in the interior of the array of (n - 1) modules to engage modules adjacent either side of the gap remaining for the last module.
18. A method according to claim 16 or 17, and including the step of applying diametral contraction along a diameter which extends substantially perpendicular to a diameter which in the finished configuration of the cylinder will intersect the last installed module.
19. A method of assembling a modular cylinder consisting of n identical modules according to any one of claims 6 to 15 in engagement in a cylindrical array, comprising assembling together the n-modules in a loose fitting cylindrical configuration, and stressing said assembly by inserting filler means between the adjacent surfaces of the modules at each interface between the adjacent modules, said filler means fitting between the sidewalls of the modules near the radially outer panels defining the exterior of the cylinder, whereby insertion of the final said filler means stresses the cylinder in the required manner.
20. A method according to claim 19, wherein the modules all include recesses in the external surfaces of their sidewalls adjacent said radially outer panel of each module, and said filler means comprise cylindrical rods adapted to be driven into the space between 23> c registering said recesses at each interface.
21. A method according to claim 20, wherein each of said cylindrical rods has a tapered en d to facilitate insertion into said spaces.
22. A method according to any one of claims 19 to 21 including deforming the cylinder of loosely assembled segments into an elliptical configuration and inserting said filler means at the regions of smallest radius of curvature of the ellipse, i.e. in the vicinity of the ends of the major axis of the ellipse.
23. A method according to claim 22, comprising deforming the loosely assembled cylindrical array into an ellipse by application of a radially outward force to expand a diameter of the cylindrical array to form the major axis of an elliptical array.
24. A modular cylinder substantially as hereinbefore described with reference to, and as illustrated in, the accompanying drawings.
25. A module for a cylinder, substantially as hereinbefore described with reference to, and as illustrated in, Figure 1 of the accompanying drawings.
26. A method of assembling a modular cylinder, substantially as hereinbefore described with reference to Figures 1 to 3 and 5 of the accompanying drawings.
27. A method of assembling a modular cylinder, substantially as hereinbefore described with reference to Figures 4 and 6 of the accompanying drawings.
Published 1991 at 71te Patent Office. Concept House. Cardiff Road. Newport. Gwent NP9 I RH. Further copies rilay be obtained frorn Sales Branch. Unit 6. Nine Mile Point. CAmifelinfach. Cross Keys. Newport. NP1 7HZ Printed by Multiplex techWquCs ltd. 51 Mary Cray. Kent.
GB9027684A 1990-03-05 1990-12-20 Lightweight cylinder construction Withdrawn GB2241714A (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US07/664,080 US5265750A (en) 1990-03-05 1991-03-04 Lightweight cylinder construction
CN91102102A CN1056319A (en) 1990-03-05 1991-03-05 Lightweight cylinder construction
KR1019920702165A KR920704049A (en) 1990-03-05 1991-03-05 Light weight cylinder structure
BR919106123A BR9106123A (en) 1990-03-05 1991-03-05 Hollow cylinder, module that defines a segment of a modular cylinder and process for the assembly of a modular cylinder
EP19910301792 EP0446006A1 (en) 1990-03-05 1991-03-05 Lightweight cylinder construction
PCT/GB1991/000335 WO1991014117A1 (en) 1990-03-05 1991-03-05 Lightweight cylinder construction
JP3505407A JPH07509043A (en) 1990-03-05 1991-03-05 Lightweight cylinder structure
US07/915,220 US5267388A (en) 1990-03-05 1992-07-20 Method of forming a lightweight cylinder

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9004850A GB2241713A (en) 1990-03-05 1990-03-05 Lightweight cylinder construction

Publications (2)

Publication Number Publication Date
GB9027684D0 GB9027684D0 (en) 1991-02-13
GB2241714A true GB2241714A (en) 1991-09-11

Family

ID=10671997

Family Applications (2)

Application Number Title Priority Date Filing Date
GB9004850A Withdrawn GB2241713A (en) 1990-03-05 1990-03-05 Lightweight cylinder construction
GB9027684A Withdrawn GB2241714A (en) 1990-03-05 1990-12-20 Lightweight cylinder construction

Family Applications Before (1)

Application Number Title Priority Date Filing Date
GB9004850A Withdrawn GB2241713A (en) 1990-03-05 1990-03-05 Lightweight cylinder construction

Country Status (2)

Country Link
KR (1) KR920704049A (en)
GB (2) GB2241713A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114990741B (en) * 2022-07-01 2023-03-21 江苏迎阳无纺机械有限公司 Non-cylindrical cylinder structure and control method

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB494323A (en) * 1936-01-18 1938-10-24 Georges Edouard Riveau Improvements in and relating to rotary printing machines
EP0094781A1 (en) * 1982-05-12 1983-11-23 Carding Specialists (Canada) Limited Improvements relating to carding engines

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB494323A (en) * 1936-01-18 1938-10-24 Georges Edouard Riveau Improvements in and relating to rotary printing machines
EP0094781A1 (en) * 1982-05-12 1983-11-23 Carding Specialists (Canada) Limited Improvements relating to carding engines

Also Published As

Publication number Publication date
GB9027684D0 (en) 1991-02-13
GB2241713A (en) 1991-09-11
GB9004850D0 (en) 1990-05-02
KR920704049A (en) 1992-12-19

Similar Documents

Publication Publication Date Title
US5265750A (en) Lightweight cylinder construction
KR101328617B1 (en) Elastic joint body
DE3803683C2 (en)
US5664327A (en) Method for producing a hollow composite members
WO1980001197A1 (en) Pipe coupling for lap joints
CA2074938A1 (en) Pipe connection particularly on composite pipes
DE10143290A1 (en) Curved pipe for transporting e.g. cement comprises inner abrasion -resistant pipe mounted between rings attached to steel connecting collars, outer steel pipe being welded to ribs on outside of collars
KR102010810B1 (en) Pressure coupler for connecting steel bars
GB2124679A (en) Tunnel wall structure
DE2459237C2 (en) Vertical type electric machine
CA2011626C (en) Arcuate precast tunnel lining segments
AU630437B2 (en) Perforated connecting disk for scaffolding elements
JP3837334B2 (en) Manufacturing method of shaft / hub joint
CN1788129A (en) Joint equipment for steel reinforcing
GB2039576A (en) Method and device for assembling voussoirs for lining a tunnel
GB2241714A (en) Lightweight cylinder construction
US2826800A (en) Pre-stressing of concrete assemblies
US5267388A (en) Method of forming a lightweight cylinder
JP4580355B2 (en) Synthetic segment
US3479697A (en) Pin-type connecting joint and method of assembling
JP7586389B2 (en) Inner surface material fitting device and inner surface material fitting method
US4252464A (en) Device for limiting stresses in particular for buried tubular structures
US9593449B2 (en) Screening device
US20240328453A1 (en) Integrated composite drive shafts
JPH0244994B2 (en) TATEKOYORAINAAPUREETONORENKETSUSEKOHOHO

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)