US3754577A - Harness frame support rod possessing increased bending strength - Google Patents

Harness frame support rod possessing increased bending strength Download PDF

Info

Publication number
US3754577A
US3754577A US00197202A US3754577DA US3754577A US 3754577 A US3754577 A US 3754577A US 00197202 A US00197202 A US 00197202A US 3754577D A US3754577D A US 3754577DA US 3754577 A US3754577 A US 3754577A
Authority
US
United States
Prior art keywords
body member
support rod
reinforcement means
edge reinforcement
elasticity
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US00197202A
Inventor
R Heller
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.)
Rheinmetall Air Defence AG
Original Assignee
Oerlikon Contraves AG
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 Oerlikon Contraves AG filed Critical Oerlikon Contraves AG
Application granted granted Critical
Publication of US3754577A publication Critical patent/US3754577A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • DTEXTILES; PAPER
    • D03WEAVING
    • D03CSHEDDING MECHANISMS; PATTERN CARDS OR CHAINS; PUNCHING OF CARDS; DESIGNING PATTERNS
    • D03C9/00Healds; Heald frames
    • D03C9/06Heald frames
    • D03C9/0608Construction of frame parts
    • D03C9/0616Horizontal upper or lower rods
    • D03C9/0625Composition or used material
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03CSHEDDING MECHANISMS; PATTERN CARDS OR CHAINS; PUNCHING OF CARDS; DESIGNING PATTERNS
    • D03C9/00Healds; Heald frames
    • D03C9/06Heald frames
    • D03C9/0608Construction of frame parts
    • D03C9/0616Horizontal upper or lower rods
    • D03C9/0633Heald bars or their connection to other frame parts
    • EFIXED CONSTRUCTIONS
    • E04BUILDING
    • E04CSTRUCTURAL ELEMENTS; BUILDING MATERIALS
    • E04C3/00Structural elongated elements designed for load-supporting
    • E04C3/02Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces
    • E04C3/29Joists; Girders, trusses, or trusslike structures, e.g. prefabricated; Lintels; Transoms; Braces built-up from parts of different material, i.e. composite structures

Definitions

  • ABSTRACT A support rod for a harness frame of a loom and method for the fabrication of such support rod wherein at least one edge reinforcement means is mounted at the region of at least one of the extremities of a lightweight support rod body member, with a thermally hardenable adhesive material interposed at the interface between the edge reinforcement means and the body member. A force is applied to said edge reinforcement means and said body member sufi'icient to firmly clamp such edge reinforcement means and body member to one another while preventing relative shifting of .said edge reinforcement means and body member.
  • body member and edge reinforcement means are then heated to a temperature sufficient to set the adhesive material while maintaining the clamping force to prevent relative shifting of said edge reinforcement means and body member.
  • the body member and edge reinforcement means are then cooled down to room temperature while still maintaining the clamping force to further prevent shifting of the edge reinforcement means and body member relative to one another, in
  • The'present invention relates to anew and improved harness frame support rod or -rail:for-. looms possessing increased bending strength or structural rigidity, and also is concerned with a novel-method forthe fabrication of such inventive harness frame support rod.
  • Still a further significant object of the present invention relates to a novel, construction of heddlesupport rod for the harness frames of looms possessing increased bending strength, yet relatively low weight.
  • a further significant object of thepresent invention relates to an improved constructionxof support rod or rail for the harness frames of looms formed from a lightweight body member equippedwith reinforcement means at least at one of the extremities of the support rod, the reinforcement means beingformed of amaterial possessinga considerably greater'modulus of elasticity than the modulus of elasticity of the material forming the lightweightsupport rod body.
  • the support rod for a loom harness frame as contemplated by this invention comprises a support rod body member formed of a lightweight material possessing relatively low modulus of elasticity.
  • the body member includes external edgesor edge regions spaced furthest from the neutral bending axis of such body member, reinforcement means being secured to such external edges.
  • the reinforcement means exhibit a total cross-sectional area which is small in relation to the cross-sectional area of the body member.
  • the cross-sectional area of such reinforcement means preferably amounts to no more than approximately one-fifth of the crosssectional area of the solid material of the harness frame body member and no more than approximately onetwentieth of the total cross-sectional area of the body member.
  • Each such reinforcement means is advantageously formed of a material different from the material of the body member and possesses a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member.
  • the modulus of elasticity of the material forming the reinforcement means is preferably at least approximately three times as large as the modulus of elasticity of the material forming the support rod body member.
  • the invention is also concerned with a novel method of fabricating such new and improved construction of harness frame support rods for looms.
  • the reinforcement means are-securely bonded in a stress-free fashion to the support rod body member. This is important inasmuch as the materials forming the reinforcement means and the support rod body member differ from one another and therefore, possess different coefficients of expansion and contraction. Hence, if measures were not otherwise undertaken to provide a stress-free adhesive bond between these different materials during thermal bonding such materials would elongate and contract at different rates.
  • the invention contemplates prevention of relative displacement or shifting of the reinforcement means and body member during the heating and subsequent cooling operations by physically restraining or confining such members.
  • a pasty or liquid thermally hardenable adhesive bonding agent typically a commercially available epoxy resin which sets or hardens at elevated temperatures, typically above 100C, is provided at the interface between the reinforcement means and support rod body member. Sufficient pressure is applied for the purpose of tightly clamping the reinforcement means and body member to one another so no relative shifting occurs.
  • This assembly is then heated, for instance to a temperature in the range of 110 130C, the bonding agent hardening at the elevated temperature, typically for instance at 120C. Then such assembly is permitted to cool down. Owing to the imposed restraint against relative elongation and contraction of the reinforcement means and body member during the heating and cooling of these components the adhesive bond can set without being subjected to any appreciable shearstresses. As a result, there is produced a good firm stress-free bond between these components, promoting high operating speeds of the loom without any great danger of disconnection or rupture of this bond of the heddle support rod, which otherwise could cause heddle failure and loom breakdown.
  • reinforcement means and rod body member can be achieved in a number of different ways.
  • One specific technique which may be employed is to provide an excess length of the reinforcement means and support rod body member, then to fixedly interconnect these members to one another, as by riveting, to prevent relative shifting or displacement.
  • the adhesive bond at the interface between these members is then permitted to set at elevated temperatureswhile a clamping force is applied between the members, and thereafter the assembly is permitted to again cool down to room temperature.
  • the excess length of the reinforcement means and body member which contains the connection rivets is cutaway so that the harness frame construction is then of desired size.
  • Another preferred technique which can be successfully practiced is to clamp the entire assembly of reinforcement means and body member, with the thermally hardenable adhesive material at the interface therebetween, in a press and to apply sufficient clamping pressure to this assembly of components so as to prevent relevant shifting i.e., elongation and contraction of the reinforcement means and body member during the heating and subsequent cooling operations.
  • the adhesive material is then permitted to set at elevated temperature and the assembly cooled down to room temperature, producing the stress-free bond between these components.
  • Such adhesive materialconfining means can be in the form of raised spacer ribs located at the interface between these components, and preferably at each of the recesses of the support rod body member receiving one of the reinforcement means.
  • spacer ribs take-up the forces exerted during the clamping operation so that the clamping pressure is distributed to a large extent over such spacer ribs, thus ensuring that the adhesive material in the recess or recesses at the interface between these abovementioned components will not be expressed out of such recesses, rather will set thereat to provide the desired bond.
  • an open glass fiber fabric or web for instance of about 0.2 mm. thickness, imbued with the adhesive material and providing the same function as the spacer ribs discussed above.
  • FIG. 1 is a fragmentary perspective cross-sectional view of a preferred construction of harness frame support rod equipped with edge reinforcement means .as contemplated by this invention and produced in accordance with the inventive method;
  • FIG. 2 is a fragmentary enlarged view showing details of the connection of an edge reinforcement meanswith an upper end or upper extremity of the support rod body member;
  • FIG. 3 is a fragmentary enlarged view showing details of the connection of a reinforcement means with the lower end or extremity of the support rod body member;
  • FIG. 4 is a modified construction of support rod for a harness frame and also equipped with reinforcement means as contemplated by the invention
  • FIG. 5 is a schematic cross-sectional view of the edge reinforcedsupport rod assembly depicted in FIGS. 1 3 inclusive, during such time as it is clamped in a press during the manufacturing operation;
  • FIG. 6 is an enlarged fragmentary view showing details of adhesive material-confining means in the form of an open glass fiber fabric or web interposed at the interface between the support rod body member and reinforcement means.
  • FIGS. I 3 inclusive a lightweight support rod body member 12.
  • This body member 12 is advantageously in the form of a hollow profile member possessing one or more internal compartments l4 and 16.
  • a transverse rib. l5 separates these compart ments 14 and 16 as shown.
  • the body member 12 incorporates an upper'bodyportion l8and a lower body portion 20, the upper portion 18 possessing a substantially quadratic or rectangular cross-sectional configuration as shown.
  • the lower portion 20 is in the form of a downwardly depending wall or web 22 merging withthe lower wall vl9 of thebox-like upper portion 18 and at which'there is bonded in a recess 30 a-reinforcement'means 24, also referred to as edge reinforcement, providing a heddlecarrier or stringing rail.
  • a-reinforcement'means 24 also referred to as edge reinforcement, providing a heddlecarrier or stringing rail.
  • edge reinforcement means 26 and 28 likewise bonded in suitable recesses 30 formed at the upper region of body member 12.
  • the reinforcementmeans 24, 26 and'28 are for instance in the form of plate-like reinforcement elements.
  • a suitable commercially available adhesive material 3.2 is provided at the interface between each edge reinforcement means 26, 28 and the bottom wall 31 of each of the associated recesses 30 formed at the upper region of body member 12.
  • Such adhesive material 32 is also provided at the interface between the lower edge reinforcement means or element 24 defining the heddle stringing rail and the wall 31 of the recess 30 at the lower end of the downwardly depending web 22 of the body member 12 receiving such edge reinforcement means 24, as best seen by referring to FIG. 3.
  • spacer ribs 34 are provided at the region of the adhesive materialreceiving recesses 30 for the purposes to be explained more fully hereinafter, and specifically, such spacer ribs 34 are here shown provided at the wall 31 of the body member 12 from which the recesses 30 are formed.
  • These spacer ribs or cams 34 advantageously extend over the full length of the associated recesses 30 receiving the edge reinforcement means 24, 26 and 28 bonded therein by the high-grade thermally hardenable adhesive 32.
  • High-grade thermally hardenable adhesive materials which set at elevated temperatures, typically above 100C, suitable for the purposes of the invention are well known in the art and commercially available,
  • the body member 12 is not only advantageously formed to possess a hollow construction, but from a suitable lightweight material, for instancesuch as aluminum or aluminum alloys, glass fiber-reinforced plastic, such as glass fiber-reinforced polyester resins or magnesium alloys, Aluminum alloys are particularly preferred materials for the body member 12 since such can be readily extrudedv or otherwise worked into desired shape.
  • a suitable commercially available aluminum alloy is onehaving a modulus of elasticity of about 700,000 kg/cm a tensile strength or breaking load of 30 kg/cm, andaspecific weight of approximately 2.8 kg/dm.
  • the modulus of elasticity typically amounts toapproximately 300,000 kg/cm the tensional strength to 50 kg/cm and the specific weight'to 1.8 kg/dm".
  • the edge reinforcement means 24, 26 and 28 can be formed of high-grade steel or spring steel, the physical properties of which advantageously can be improved by cold rolling, or else from carbon fiber laminates.
  • typical values for the modulus of elasticity are 2,l00,000kg/cm for the specific weight 8.0 kg/dm, and for the tensile strength or breaking load kg/cm or greater, depending upon the manner of processing the steel in order to improve its properties.
  • the commercially available carbon fiber laminates are preferably of the type comprising unidirectional carbon fibers embedded in a suitable bonding agent and plastic resin, typically an epoxy resin.
  • the modulus of elasticity thereof amounts to 2,500,000 kg/cm the tensile strength or breaking load to 200 kg/cm and the specific weight to 1.6 kg/dm
  • the harness framesupport rod comprises a body member 12 formed of a relatively light weight material possessing a relatively low modulus of elasticity in relation to the edge reinforcement means 24, 26 and 28 which possess a relatively high modulus of elasticity.
  • the modulus of elasticity of body member is preferably less than l,000,000 kg/cm and that of the reinforcement means preferably greater than 1,500,000 kg/cm. In fact, it will be observed the modulus of elasticity of the edge reinforcement means preferably amounts to at least three times that of the material forming the body member.
  • the edge reinforcement means 24, 26 and 28 are advantageously located solely at extremities of the body member 12 i.e., the localities furthest from the neutral bending axis of the heddle framesupport rod to provide maximum bending strength.
  • the lower reinforcement element 24 is advantageously located at the region of the central lengthwise vertically extending axis of the body member 12.
  • edge reinforcement means located in the manner described above affords the requisite bending strength required of the support rod for the harness frame.
  • the thickness and length of the edge reinforcement means are, in actual practice, accommodated to the required bending strength in both main directions of the support rod. Excess material should be avoided in order to retain the total weight of the structure as low as possible and also for reasons of manufacturing economy.
  • the cross-sectional area of an edge reinforcement means usually amounts to no more than approximately one-fifth of the cross-sectional area of the solid material forming the body member 12 and no more than approximately one-twentieth of the total cross-sectional area of the hollow profile body member.
  • the external dimensions and wall thickness of the light-weight hollow profile body member 12 also should be retained as low as possible in order to save on weight, without however falling below the requisite compressiveand shear-strength which is required.
  • filling of the internal hollow space or spaces 14 and 16 with a suitable reinforcing material of a small as possible specific weight i.e., for instance amounting to no more than 0.5 kg/dni results in improvement to the support rod.
  • FIG. 4 A modified construction of support rod 10. for a loom harness frame has been depicted in FIG. 4, wherein like reference characters have been generally used to again designate the same or analogous components.
  • the hollow profile body member 12 of tlie modified support rod is only provided with a single internal compartment 40.
  • additional edge reinforcement means 42 and 44 are provided intermediate the lower edge reinforcement means 24 and the upper edge reinforcement means 26 and 28, and these additional edge reinforcement means 42 and 44 are specifically shown located at the lower region of the upper portion 18 of the body member 12 at the bottom end of the internal compartment 40.
  • the materials for the body member and plate-like reinforcements and physical dimensions are advantageously selected as discussed above.
  • an important aspect of this invention concerns a method of forming the support rod for the harness frames, and specifically bonding the reinforcement elements or means to the body member of the support rod.
  • a preferred technique for carrying out the inventive method will now be considered in conjunction with FIGS. 5 and 6 inclusive.
  • the material to be bonded namely the plate-like reinforcement elements
  • a pasty adhesive bonding agent for instance a commercially available epoxy resin of the type which hardens or sets at approximately 120C is then applied, either to one face of each reinforcement plate or into the various recesses 30 where the individual reinforcement plates are to be inserted.
  • the recesses 30 are advantageously of the type depicted in FIGS.
  • spacer ribs 34 preferably extending the length of the associated recesses or body member and serve to confine the adhesive bonding agent therein during application of the clamping force or pressure.
  • an open glass fiber fabric or web 50 for instance of about 0.2mm. thickness, and of the type depicted in FIG. 6, which is then inserted into each associated recess.
  • the glass fiber fabric or web 50 absorbs the adhesive material and has the same function as the spacer ribs 34 previously discussed above.
  • the plate-like reinforcement elements are inserted into the various recesses so that at the interface between such reinforcement plates and the confronting wall of each recess there appears either the adhesive layer or the glass fiber reinforced web or fabric 50 imbued with the adhesive material.
  • this assembly is then introduced into a suitable press 52 which has been cooled down to room temperature. Press 52 is then closed and the necessary clamping force or pressure is applied, which pressure can be experimentally determined. In any event this force or pressure must be sufficient to tightly clamp the reinforcement elements with the body member of the support rod so as to prevent any relative displacement or shifting between these components during the expansion and contraction occuring by virtue of the heating and cooling operations. For instance, when using a 1 mm. thick reinforcement element and the spacer ribs a clamping pressure in the range of approximately 50 100 kp/cm, based upon each square centimeter of surface area of the reinforcement plate i.e. adhesive location, has been found to be satisfactory.
  • the assembly After the necessary clamping pressure has been applied the assembly is heated to a temperature sufficient for setting or hardening the adhesive bonding agent, and the bonding agent is permitted to harden or set at a temperature between approximately C.
  • the applied clamping force is sufficient to prevent any relative elongation of the reinforcement elements and body member of the support rod, notwithstanding the fact that they are formed of different materials and possess different coefficients of expansion. Further, this clamping pressure or force is also main tained and effective during cooling of the aforementioned components back down to room temperature, so that during contraction of the reinforcement elements and body member again no relative displacement or shifting between these components occurs.
  • the set adhesive bond is free of stresses so that a secure premanent fixation is provided between these components, one which is not likely to rupture when subjected to load during operation of the harness frame at high frequencies. It will be noticed that the reinforcement plates or elements are retained in the complementary configured recesses and advantageously do not protrude past the surface of the associated body member.
  • edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, said body member being constructed in the form of a substantially rectangular hollow profile member possessing four external edges each of which is equipped with a recess, said edge reinforcement means being in the form of a respective edge reinforcement plate member adhesively bonded into an associated edge recess such that said edge reinforcement plate members do not protrude past the external surfaces of the rectangular hollow profile rod member.
  • I including a glass fiber-reinforced material layer con- I taining the adhesive material located in said recess between said edge reinforcement means and said body member for maintaining the adhesive material confined within said recess.
  • edge reinforcement plate members are configured to possess a substantially flat rectangular shape.
  • a support 'rod for the harness frame of a loom possessing increased bending strength comprising a support rod body member having a neutral bending axis, said body member being formed of a lightweight material possessing a relatively low modulus of elasticity, said body member further including external regions spaced remote from the neutral bending axis of the support rod, edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total crosssectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, and
  • edge reinforcement means is a carbon fiber laminate.
  • a support rod for the harness frame of a loom possessing increased bending strength comprising a support rod body member having a'neutral bending axis, said body member being formed of a lightweight material possessing a relatively low modulus of elasticity, said body member further including external re.
  • edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total cross-sectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, and wherein said material of body member is a fiber reinforced plastic.
  • a support rod for the harness frame of a loom possessing increased bending strength comprising a support rod body member having a neutral bending axis, said body member being formed of a lightweight material possessing a relatively low modulus of elasticity, said body member further including external regions spaced remote from the neutral bending axis of the support rod, edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total cross-sectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, at least one recess for receiving each edge reinforcement means provided at said at least one external region, a thermally hardenable adhesive material interposed at the region of said recess for bonding said edge reinforcement means with the body member of the support rod, and a glass fiber-reinforced material layer containing the adhesive material located in said recess
  • Asupport rod for the harness frame of a loom possessing increased bending strength comprising-a support rod body member having a neutral bending axis, said body member being formed of'a lightweight material possessing a relatively low modulus of elasticity, said body member further including external regions spaced remote from the neutral bending axis of the support rod, edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total cross-sectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, and wherein said body member possesses a substantially rectangular configuration and comprising a hollow profile member, said hollow profile member being provided with an integral support web, one of said edge reinforcement means providing a heddle stringing rail connected with said support web, said heddle stringingv rail being disposed substantially in the vertically extending symmetrical plane of said

Abstract

A support rod for a harness frame of a loom and method for the fabrication of such support rod wherein at least one edge reinforcement means is mounted at the region of at least one of the extremities of a lightweight support rod body member, with a thermally hardenable adhesive material interposed at the interface between the edge reinforcement means and the body member. A force is applied to said edge reinforcement means and said body member sufficient to firmly clamp such edge reinforcement means and body member to one another while preventing relative shifting of said edge reinforcement means and body member. The body member and edge reinforcement means are then heated to a temperature sufficient to set the adhesive material while maintaining the clamping force to prevent relative shifting of said edge reinforcement means and body member. The body member and edge reinforcement means are then cooled down to room temperature while still maintaining the clamping force to further prevent shifting of the edge reinforcement means and body member relative to one another, in order to provide a substantially stress-free bond between said edge reinforcement means and body member by virtue of the set adhesive material.

Description

United States Patent [191 Heller HARNESS FRAME SUPPORT ROD POSSESSING INCREASED BENDING STRENGTH [75] Inventor: Rudolf Heller, Zurich, Switzerland [73] Assignee: Contraves AG, Zurich, Switzerland [22] Filed: Nov. 10, 1971 [21] Appl. No.: 197,202
Related US. Application Data [63] Continuation-impart of Ser. No. 854,146, Aug. 29,
1969, abandoned.
[30] Foreign Application Priority Data [451 Aug. 28, 1973 Primary Examiner-Henry S. Jaudon Attorney-Wemer W. Kleeman [5 7] ABSTRACT A support rod for a harness frame of a loom and method for the fabrication of such support rod wherein at least one edge reinforcement means is mounted at the region of at least one of the extremities of a lightweight support rod body member, with a thermally hardenable adhesive material interposed at the interface between the edge reinforcement means and the body member. A force is applied to said edge reinforcement means and said body member sufi'icient to firmly clamp such edge reinforcement means and body member to one another while preventing relative shifting of .said edge reinforcement means and body member. The
body member and edge reinforcement means are then heated to a temperature sufficient to set the adhesive material while maintaining the clamping force to prevent relative shifting of said edge reinforcement means and body member. The body member and edge reinforcement means are then cooled down to room temperature while still maintaining the clamping force to further prevent shifting of the edge reinforcement means and body member relative to one another, in
order to provide a substantially stress-free bond between said edge reinforcement means and body member by virtue of the set adhesive material.
31 Claims, 6 Drawing Figures PAIENTEDAUGZB um 3754.577
sum 2 or 2 W I F IG- 5 2 X242 7 FIG. 6
FIG.4
HARNESS FRAME SUIZPORT ROD-POSSESSING INCREASED BENDING STRENGTH CROSS-REFERENCE TORELATED APPLICATION This application is a continuation-in-partapplication of mycommonly assigned, co-pending,United-States application Ser. No. 854,146, filed Aug. 2-9, 1969 and entitled "ROD W ITH INCREASED 'BENDING STRENGTH AND USE THEREOF, now abandoned.
BACKGROUNDQF THE INVENTION The'present inventionrelates to anew and improved harness frame support rod or -rail:for-. looms possessing increased bending strength or structural rigidity, and also is concerned with a novel-method forthe fabrication of such inventive harness frame support rod.
It should be recognized thatin the case of heddle or harness frames for looms it is especially important to satisfy therequirements of smallest possible weight and greatest possible bending strengthor structural rigidity. This is particularly'the case if it is desired to drive the harness frames at high operating speeds. As is well known the energy required for driving such harness frames increases in proportion to the weight thereof and as a function ofthe square of the speed of move ment. Increased weight of the harness structure requires a corresponding greater amount of drive power. This energy must .be furnished by suitable drive motors or other prime movers. It is therefore desirable to reduce the weight of the harness frames.
On the other hand, bending of the harness frames, and in particular the heddle support rods, owing to insufficient bending strength or structural rigidity causes operational disturbances inasmuch as such, in turn, can bring about buckling and/or rupture of the heddles suspended at the harness frames. By providing minimum weight and maximum bending strength of the mechanical components it is possible to increase the natural frequency of the relevant components, inducement of res onant frequencies only occuring at correspondingly high frequency-dynamic loading.
From what has been stated above, it should be apparent that in the case of harness frames for looms it is extremely desirable to provide a harness frame construction which possesses increased bending strength and minimum weight, thereby permitting the harness frame to be driven at high operating frequencies.
SUMMARY OF THE, INVENTION Hence, it is a primary object of the present invention to provide a novel construction of support rod.- or rail for the harness frame of looms, which effectively and reliably fulfills the existing; need in the art;
I Still a further significant object of the present invention relates to a novel, construction of heddlesupport rod for the harness frames of looms possessing increased bending strength, yet relatively low weight.
A further significant object of thepresent invention relates to an improved constructionxof support rod or rail for the harness frames of looms formed from a lightweight body member equippedwith reinforcement means at least at one of the extremities of the support rod, the reinforcement means beingformed of amaterial possessinga considerably greater'modulus of elasticity than the modulus of elasticity of the material forming the lightweightsupport rod body.
jects of the invention, which will become more readily apparent as the description proceeds, the support rod for a loom harness frame as contemplated by this invention comprises a support rod body member formed of a lightweight material possessing relatively low modulus of elasticity. The body member includes external edgesor edge regions spaced furthest from the neutral bending axis of such body member, reinforcement means being secured to such external edges. The reinforcement means exhibit a total cross-sectional area which is small in relation to the cross-sectional area of the body member. For instance, the cross-sectional area of such reinforcement means preferably amounts to no more than approximately one-fifth of the crosssectional area of the solid material of the harness frame body member and no more than approximately onetwentieth of the total cross-sectional area of the body member. Each such reinforcement means is advantageously formed of a material different from the material of the body member and possesses a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member. Typically, the modulus of elasticity of the material forming the reinforcement means is preferably at least approximately three times as large as the modulus of elasticity of the material forming the support rod body member.
As already explained above the invention is also concerned with a novel method of fabricating such new and improved construction of harness frame support rods for looms. As also previously mentioned the reinforcement means are-securely bonded in a stress-free fashion to the support rod body member. This is important inasmuch as the materials forming the reinforcement means and the support rod body member differ from one another and therefore, possess different coefficients of expansion and contraction. Hence, if measures were not otherwise undertaken to provide a stress-free adhesive bond between these different materials during thermal bonding such materials would elongate and contract at different rates. Thus, when the assembly is again brought down to room temperature relative shifting or displacement between the reinforce ment means and the support rod body member would occur, resulting in loading and particularly the formation of shear stresses at the adhesive bond formed between the reinforcement means and rod body member. Since the harness frames are desirably driven at high operating frequencies or speeds and thus subjected to high dynamic loads these loads would promote rupture of the adhesive bond between such reinforcement means and the body member if special measures were to devise a new and improved technique for fabricating such type edge reinforcedsupport rods of harness frames and specifically to provide a completely novel technique of bonding the reinforcement means with the body of the support rod. In its broadest aspects this technique contemplates thermally bonding the reinforcement means with the support rod body member with an interface of a thermally hardenable adhesive material. It has surprisingly been found that if relative displacement of the reinforcement means and body member are prevented during the thermal bonding operation there can be advantageously formed a relatively stress-free bond capable of withstanding high dynamic loads. To this end, the invention contemplates prevention of relative displacement or shifting of the reinforcement means and body member during the heating and subsequent cooling operations by physically restraining or confining such members. More specifically, a pasty or liquid thermally hardenable adhesive bonding agent, typically a commercially available epoxy resin which sets or hardens at elevated temperatures, typically above 100C, is provided at the interface between the reinforcement means and support rod body member. Sufficient pressure is applied for the purpose of tightly clamping the reinforcement means and body member to one another so no relative shifting occurs. This assembly is then heated, for instance to a temperature in the range of 110 130C, the bonding agent hardening at the elevated temperature, typically for instance at 120C. Then such assembly is permitted to cool down. Owing to the imposed restraint against relative elongation and contraction of the reinforcement means and body member during the heating and cooling of these components the adhesive bond can set without being subjected to any appreciable shearstresses. As a result, there is produced a good firm stress-free bond between these components, promoting high operating speeds of the loom without any great danger of disconnection or rupture of this bond of the heddle support rod, which otherwise could cause heddle failure and loom breakdown.
The previously discussed restraint against relative displacement between these components i.e., reinforcement means and rod body member, can be achieved in a number of different ways. One specific technique which may be employed is to provide an excess length of the reinforcement means and support rod body member, then to fixedly interconnect these members to one another, as by riveting, to prevent relative shifting or displacement. The adhesive bond at the interface between these members is then permitted to set at elevated temperatureswhile a clamping force is applied between the members, and thereafter the assembly is permitted to again cool down to room temperature. Upon completion of the bonding operation the excess length of the reinforcement means and body member which contains the connection rivets is cutaway so that the harness frame construction is then of desired size.
Another preferred technique which can be successfully practiced is to clamp the entire assembly of reinforcement means and body member, with the thermally hardenable adhesive material at the interface therebetween, in a press and to apply sufficient clamping pressure to this assembly of components so as to prevent relevant shifting i.e., elongation and contraction of the reinforcement means and body member during the heating and subsequent cooling operations. The adhesive material is then permitted to set at elevated temperature and the assembly cooled down to room temperature, producing the stress-free bond between these components.
It is a further aspect of this invention, and pnrticw larly when practicing the inventive method, to provide means for confining the adhesive material at the interface between the reinforcement means and body member so that when the clamping pressure is exerted the adhesive material is not displaced out of such interface, which otherwise would not afford the firm bond which is desired. Such adhesive materialconfining means can be in the form of raised spacer ribs located at the interface between these components, and preferably at each of the recesses of the support rod body member receiving one of the reinforcement means. These spacer ribs take-up the forces exerted during the clamping operation so that the clamping pressure is distributed to a large extent over such spacer ribs, thus ensuring that the adhesive material in the recess or recesses at the interface between these abovementioned components will not be expressed out of such recesses, rather will set thereat to provide the desired bond. Instead of using these spacer ribs it would be also possible to use an open glass fiber fabric or web, for instance of about 0.2 mm. thickness, imbued with the adhesive material and providing the same function as the spacer ribs discussed above.
DETAILED DESCRIPTION OF THE DRAWINGS The invention will be better understood and objects other than those set forth above, will become apparent when consideration is given to the following detailed description thereof. Such description makes reference to the annexed drawings wherein:
FIG. 1 is a fragmentary perspective cross-sectional view of a preferred construction of harness frame support rod equipped with edge reinforcement means .as contemplated by this invention and produced in accordance with the inventive method;
FIG. 2 is a fragmentary enlarged view showing details of the connection of an edge reinforcement meanswith an upper end or upper extremity of the support rod body member;
FIG. 3 is a fragmentary enlarged view showing details of the connection of a reinforcement means with the lower end or extremity of the support rod body member;
FIG. 4 is a modified construction of support rod for a harness frame and also equipped with reinforcement means as contemplated by the invention;
FIG. 5 is a schematic cross-sectional view of the edge reinforcedsupport rod assembly depicted in FIGS. 1 3 inclusive, during such time as it is clamped in a press during the manufacturing operation; and
FIG. 6 is an enlarged fragmentary view showing details of adhesive material-confining means in the form of an open glass fiber fabric or web interposed at the interface between the support rod body member and reinforcement means.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS Describing now the drawings, and referring initially in particular to the exemplary embodiment of harness or heddle frame support rod 10 depicted in FIGS. I 3 inclusive, it will be seen that such embodies a lightweight support rod body member 12. This body member 12 is advantageously in the form of a hollow profile member possessing one or more internal compartments l4 and 16. A transverse rib. l5 separates these compart ments 14 and 16 as shown. lnthe embodiment under consideration the body member 12 incorporates an upper'bodyportion l8and a lower body portion 20, the upper portion 18 possessing a substantially quadratic or rectangular cross-sectional configuration as shown. The lower portion 20 is in the form of a downwardly depending wall or web 22 merging withthe lower wall vl9 of thebox-like upper portion 18 and at which'there is bonded in a recess 30 a-reinforcement'means 24, also referred to as edge reinforcement, providing a heddlecarrier or stringing rail. At theupper region or .ex-
tremities of body member .12 there are provided additional edge reinforcement means 26 and 28 likewise bonded in suitable recesses 30 formed at the upper region of body member 12. The reinforcementmeans 24, 26 and'28 are for instance in the form of plate-like reinforcement elements.
As best seen by referring to FIG. 2 a suitable commercially available adhesive material 3.2 is provided at the interface between each edge reinforcement means 26, 28 and the bottom wall 31 of each of the associated recesses 30 formed at the upper region of body member 12. Such adhesive material 32 is also provided at the interface between the lower edge reinforcement means or element 24 defining the heddle stringing rail and the wall 31 of the recess 30 at the lower end of the downwardly depending web 22 of the body member 12 receiving such edge reinforcement means 24, as best seen by referring to FIG. 3. Further, in the exemplary embodiment under consideration adhesive materialconfining means in the form of spacer ribs 34 are provided at the region of the adhesive materialreceiving recesses 30 for the purposes to be explained more fully hereinafter, and specifically, such spacer ribs 34 are here shown provided at the wall 31 of the body member 12 from which the recesses 30 are formed. These spacer ribs or cams 34 advantageously extend over the full length of the associated recesses 30 receiving the edge reinforcement means 24, 26 and 28 bonded therein by the high-grade thermally hardenable adhesive 32. High-grade thermally hardenable adhesive materials which set at elevated temperatures, typically above 100C, suitable for the purposes of the invention are well known in the art and commercially available,
atypical example thereof being a pasty epoxy resin of q the type which hardens or sets for instance at about 120C. v
Now in consideration of maintaining the weight of the support rod for the harness frame as small as possible the body member 12 is not only advantageously formed to possess a hollow construction, but from a suitable lightweight material, for instancesuch as aluminum or aluminum alloys, glass fiber-reinforced plastic, such as glass fiber-reinforced polyester resins or magnesium alloys, Aluminum alloys are particularly preferred materials for the body member 12 since such can be readily extrudedv or otherwise worked into desired shape. A suitable commercially available aluminum alloy is onehaving a modulus of elasticity of about 700,000 kg/cm a tensile strength or breaking load of 30 kg/cm, andaspecific weight of approximately 2.8 kg/dm. In the caseofglass-fibenreinforced plastic the modulus of elasticity typically amounts toapproximately 300,000 kg/cm the tensional strength to 50 kg/cm and the specific weight'to 1.8 kg/dm". As far as the edge reinforcement means 24, 26 and 28 are concerned such can be formed of high-grade steel or spring steel, the physical properties of which advantageously can be improved by cold rolling, or else from carbon fiber laminates. In the case of steel, typical values for the modulus of elasticity are 2,l00,000kg/cm for the specific weight 8.0 kg/dm, and for the tensile strength or breaking load kg/cm or greater, depending upon the manner of processing the steel in order to improve its properties. The commercially available carbon fiber laminates are preferably of the type comprising unidirectional carbon fibers embedded in a suitable bonding agent and plastic resin, typically an epoxy resin. The modulus of elasticity thereof amounts to 2,500,000 kg/cm the tensile strength or breaking load to 200 kg/cm and the specific weight to 1.6 kg/dm Hence, from what has been explained above it will be seen that the harness framesupport rod comprises a body member 12 formed of a relatively light weight material possessing a relatively low modulus of elasticity in relation to the edge reinforcement means 24, 26 and 28 which possess a relatively high modulus of elasticity.
The modulus of elasticity of body member is preferably less than l,000,000 kg/cm and that of the reinforcement means preferably greater than 1,500,000 kg/cm. In fact, it will be observed the modulus of elasticity of the edge reinforcement means preferably amounts to at least three times that of the material forming the body member. Further, the edge reinforcement means 24, 26 and 28 are advantageously located solely at extremities of the body member 12 i.e., the localities furthest from the neutral bending axis of the heddle framesupport rod to provide maximum bending strength. The lower reinforcement element 24 is advantageously located at the region of the central lengthwise vertically extending axis of the body member 12. The foregoing construction provides a support rod for a harness frame of a loom which possesses not only low weight but, in-
creased bending strength, thereby requiring less power for driving the harness frame at high frequencies or operating speeds.
The use of the edge reinforcement means located in the manner described above affords the requisite bending strength required of the support rod for the harness frame. The thickness and length of the edge reinforcement means are, in actual practice, accommodated to the required bending strength in both main directions of the support rod. Excess material should be avoided in order to retain the total weight of the structure as low as possible and also for reasons of manufacturing economy. Typically, the cross-sectional area of an edge reinforcement means usually amounts to no more than approximately one-fifth of the cross-sectional area of the solid material forming the body member 12 and no more than approximately one-twentieth of the total cross-sectional area of the hollow profile body member. By the same token the external dimensions and wall thickness of the light-weight hollow profile body member 12 also should be retained as low as possible in order to save on weight, without however falling below the requisite compressiveand shear-strength which is required. In some instances filling of the internal hollow space or spaces 14 and 16 with a suitable reinforcing material of a small as possible specific weight i.e., for instance amounting to no more than 0.5 kg/dni results in improvement to the support rod.
A modified construction of support rod 10. for a loom harness frame has been depicted in FIG. 4, wherein like reference characters have been generally used to again designate the same or analogous components. In this instance the hollow profile body member 12 of tlie modified support rod is only provided with a single internal compartment 40. The main difference over the construction here shown from that of FIGS. 1 3 is that additional edge reinforcement means 42 and 44 are provided intermediate the lower edge reinforcement means 24 and the upper edge reinforcement means 26 and 28, and these additional edge reinforcement means 42 and 44 are specifically shown located at the lower region of the upper portion 18 of the body member 12 at the bottom end of the internal compartment 40. The materials for the body member and plate-like reinforcements and physical dimensions are advantageously selected as discussed above.
It was previously explained that an important aspect of this invention concerns a method of forming the support rod for the harness frames, and specifically bonding the reinforcement elements or means to the body member of the support rod. A preferred technique for carrying out the inventive method will now be considered in conjunction with FIGS. 5 and 6 inclusive. In practicing the method the material to be bonded, namely the plate-like reinforcement elements, are advantageously initially sand blasted or scoured, and degreased. A pasty adhesive bonding agent for instance a commercially available epoxy resin of the type which hardens or sets at approximately 120C is then applied, either to one face of each reinforcement plate or into the various recesses 30 where the individual reinforcement plates are to be inserted. The recesses 30 are advantageously of the type depicted in FIGS. 1 3 possessing the spacer ribs 34 preferably extending the length of the associated recesses or body member and serve to confine the adhesive bonding agent therein during application of the clamping force or pressure. if no such spacer ribs are provided for the recesses then, there is advantageously employed an open glass fiber fabric or web 50, for instance of about 0.2mm. thickness, and of the type depicted in FIG. 6, which is then inserted into each associated recess. The glass fiber fabric or web 50 absorbs the adhesive material and has the same function as the spacer ribs 34 previously discussed above. Then the complete assembly is mounted together, in other words, the plate-like reinforcement elements are inserted into the various recesses so that at the interface between such reinforcement plates and the confronting wall of each recess there appears either the adhesive layer or the glass fiber reinforced web or fabric 50 imbued with the adhesive material.
As best seen by referring to FIG. 5 this assembly is then introduced into a suitable press 52 which has been cooled down to room temperature. Press 52 is then closed and the necessary clamping force or pressure is applied, which pressure can be experimentally determined. In any event this force or pressure must be sufficient to tightly clamp the reinforcement elements with the body member of the support rod so as to prevent any relative displacement or shifting between these components during the expansion and contraction occuring by virtue of the heating and cooling operations. For instance, when using a 1 mm. thick reinforcement element and the spacer ribs a clamping pressure in the range of approximately 50 100 kp/cm, based upon each square centimeter of surface area of the reinforcement plate i.e. adhesive location, has been found to be satisfactory. After the necessary clamping pressure has been applied the assembly is heated to a temperature sufficient for setting or hardening the adhesive bonding agent, and the bonding agent is permitted to harden or set at a temperature between approximately C. The applied clamping force is sufficient to prevent any relative elongation of the reinforcement elements and body member of the support rod, notwithstanding the fact that they are formed of different materials and possess different coefficients of expansion. Further, this clamping pressure or force is also main tained and effective during cooling of the aforementioned components back down to room temperature, so that during contraction of the reinforcement elements and body member again no relative displacement or shifting between these components occurs. Hence no shear-stresses, at least none of an appreciable nature, are present at the intermediate layer of adhesive bonding agent so that a good permanent bond is attained for securely and fixedly attaching the reinforcement plates or elements with the body member. After the assembly has been cooled down to room temperature the support rod with the now therewith affixed reinforcement elements is removed from the press 52. The spacer rib means 34 or glass fiber fabric web 50, respectively, are effective to confine the adhesive material within the associated recesses to prevent such adhesive material from being expressed out of such recesses when the clamping force or pressure is applied. Such also contribute to provide adequate frictional forces between the body member and reinforcement elements to safeguard relative shifting or displacement.
An alternative technique for practising the inventive method of fabricating such support rods for harness frames resorts to the use of fastening means for fixedly interconnecting the reinforcement elements with the body member of the support rod during the heating and cooling operations. In this case the reinforcement elements and body member possess a length exceeding that ultimately desired, and at the excess length portion of such members fastening elements such as rivets for instance are connected between the reinforcement elements and the body member so as to securely nondisplaceably attach such to one another. The rivets then contribute to prevent any relative shifting or displacement of the reinforcement elements and body member relative to one another during the heating and cooling operations, carried out while this assembly is in the press 52, so that again the interface of adhesive bonding material between these elements is free of stresses. In this case where the fastening elements are used the clamping pressure applied by the press 52 can be lower, typical values amounting to for instance 2 5 kp/cm per unit area of adhesive material.
Regardless of the technique which is employed in any event due to the provision of measures to prevent different relative elongation and contraction of the reinforcement elements and body member of the support rod the set adhesive bond is free of stresses so that a secure premanent fixation is provided between these components, one which is not likely to rupture when subjected to load during operation of the harness frame at high frequencies. It will be noticed that the reinforcement plates or elements are retained in the complementary configured recesses and advantageously do not protrude past the surface of the associated body member.
While there is shown and described present preferred embodiments of the invention, it is to be distinctly understood that the invention is not limited thereto but may be otherwise variously embodied andpracticed which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, said body member being constructed in the form of a substantially rectangular hollow profile member possessing four external edges each of which is equipped with a recess, said edge reinforcement means being in the form of a respective edge reinforcement plate member adhesively bonded into an associated edge recess such that said edge reinforcement plate members do not protrude past the external surfaces of the rectangular hollow profile rod member.
2. The support rod as defined in claim 1, wherein the modulus of elasticity of the material forming said edge reinforcement means is at least three times greater than the modulus of elasticity of the material forming said body member.
3. The support rod as defined in claim 1, wherein said edge reinforcement means is formed of steel.
4. The support rod as defined in claim 1, wherein said body member is formed of a material containing at least aluminum. I
5. The support rod as defined in claim 1, wherein the cross-sectional area of said edge reinforcement means isv no greater than one-twentieth of the total crosssectional area of said body member.
6. The support rod as defined in claim 1, further including an edge reinforcement means provided for each of said external regions.
7. The support rod as defined in claim 6, wherein said edge reinforcement means are located solely at said external regions.
, 8. The support rod as defined in claim 6, wherein one ofsaid edge reinforcement means simultaneously forms a heddle stringing rail.
edge reinforcement means with the body member of the support rod.
I including a glass fiber-reinforced material layer con- I taining the adhesive material located in said recess between said edge reinforcement means and said body member for maintaining the adhesive material confined within said recess.
12. The support rod as defined in claim 10, further including spacer ribs disposed at the region of said recess.
13. The support rod as defined in claim 11, wherein said spacer ribs extend over the length of the associated recess.
14. The support rod as defined in claim 10, wherein said spacer ribs are located at the boundary wall of said recess and serve to confine the adhesive material therein.
15. The support rod as defined in claim 1, wherein said body member is formed as a hollow profile member containing at least one internal compartment.
16. The support rod as defined in claim 1, wherein said edge reinforcement plate members are configured to possess a substantially flat rectangular shape.
17. The support rod as defined in claim I, wherein said edge reinforcement means is a carbon fiber laminate.
18. A support 'rod for the harness frame of a loom possessing increased bending strength, comprising a support rod body member having a neutral bending axis, said body member being formed of a lightweight material possessing a relatively low modulus of elasticity, said body member further including external regions spaced remote from the neutral bending axis of the support rod, edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total crosssectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, and
wherein said edge reinforcement means is a carbon fiber laminate.
19. A support rod for the harness frame of a loom possessing increased bending strength, comprising a support rod body member having a'neutral bending axis, said body member being formed of a lightweight material possessing a relatively low modulus of elasticity, said body member further including external re. gions spaced remote from the neutral bending axis of the support rod, edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total cross-sectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, and wherein said material of body member is a fiber reinforced plastic.
20. A support rod for the harness frame of a loom possessing increased bending strength, comprising a support rod body member having a neutral bending axis, said body member being formed of a lightweight material possessing a relatively low modulus of elasticity, said body member further including external regions spaced remote from the neutral bending axis of the support rod, edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total cross-sectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, at least one recess for receiving each edge reinforcement means provided at said at least one external region, a thermally hardenable adhesive material interposed at the region of said recess for bonding said edge reinforcement means with the body member of the support rod, and a glass fiber-reinforced material layer containing the adhesive material located in said recess between said edge reinforcement means and said body member for maintaining the adhesive material confined within said recess.
21. Asupport rod for the harness frame of a loom possessing increased bending strength, comprising-a support rod body member having a neutral bending axis, said body member being formed of'a lightweight material possessing a relatively low modulus of elasticity, said body member further including external regions spaced remote from the neutral bending axis of the support rod, edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total cross-sectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, and wherein said body member possesses a substantially rectangular configuration and comprising a hollow profile member, said hollow profile member being provided with an integral support web, one of said edge reinforcement means providing a heddle stringing rail connected with said support web, said heddle stringingv rail being disposed substantially in the vertically extending symmetrical plane of said hollow profile member, said external edges of said hollow profile member facing away from said heddle stringing rail being provided with recesses receiving additional edge reinforcement means.
22. The support rod as defined in claim 21, wherein the modulus of elasticity of the material forming said edge reinforcement means is at least three times greater than the modulus of elasticity of the material forming said body member.
23. The support rod as defined in claim 21, wherein said edge reinforcement means is formed of steel.
24. The support rod as defined in claim 21, wherein said edge reinforcement means is a carbon fiber laminate.
25. The support rod as defined in claim 2], wherein said body member is formed of a material containing at least aluminum.
26. The support rod as defined in claim 21, further including at least one recess for receiving each edge reinforcement means provided at said at least one external region, and a thermally hardenable adhesive mate-' rial interposed at the region of said recess for bonding said edge reinforcement means with the body member of the support rod.
27. The support rod as defined in claim 26, further including spacer ribs disposed at the region of said recess.
28. The support rod as defined in claim 27, wherein said spacer ribs extend over the length of the associated recess.
29. The support rod as defined in claim 27, wherein said spacer ribs are located at the boundary wall of said recess. and serve to confine the adhesive material therein.
30. The support rod as defined in claim 26, further including a glass fiber-reinforced material layer containing the adhesive material located in said recess between said edge reinforcement means and said body member for maintaining the adhesive material confined within said recess.
31. The support rod as defined in claim 21, wherein said body member is formed as a hollow profile member containing at least one internal compartment.

Claims (31)

1. A support rod for the harness frame of a loom possessing increased bending strength, comprising a support rod body member having a neutral bending axis, said body member being formed of a lightweight material possessing a relatively low modulus of elasticity, said body member further including external regions spaced remote from the neutral bending axis of the support rod, edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total cross-sectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, said body member being constructed in the form of a substantially rectangular hollow profile member possessing four external edges each of which is equipped with a recess, said edge reinforcement means being in the form of a respective edge reinforcement plate member adhesively bonded into an associated edge recess such that said edge reinforcement plate members do not protrude past the external surfaces of the rectangular hollow profile rod member.
2. The support rod as defined in claim 1, wherein the modulus of elasticity of the material forming said edge reinforcement means is at least three times greater than the modulus of elasticity of the material forming said body member.
3. The support rod as defined in claim 1, wherein said edge reinforcement means is formed of steel.
4. The support rod as defined in claim 1, wherein said body member is formed of a material containing at least aluminum.
5. The support rod as defined in claim 1, wherein the cross-sectional area of said edge reinforcement means is no greater than one-twentieth of the total cross-sectional area of said body member.
6. The support rod as defined in claim 1, further including an edge reinforcement meAns provided for each of said external regions.
7. The support rod as defined in claim 6, wherein said edge reinforcement means are located solely at said external regions.
8. The support rod as defined in claim 6, wherein one of said edge reinforcement means simultaneously forms a heddle stringing rail.
9. The support rod as defined in claim 6, wherein each of said edge reinforcement means comprises an edge reinforcement plate member adhesively bonded to the associated external region of said body member.
10. The support rod as defined in claim 1, further including at least one recess for receiving each edge reinforcement means provided at said at least one external region, and a thermally hardenable adhesive material interposed at the region of said recess for bonding said edge reinforcement means with the body member of the support rod.
11. The support rod as defined in claim 10, further including a glass fiber-reinforced material layer containing the adhesive material located in said recess between said edge reinforcement means and said body member for maintaining the adhesive material confined within said recess.
12. The support rod as defined in claim 10, further including spacer ribs disposed at the region of said recess.
13. The support rod as defined in claim 11, wherein said spacer ribs extend over the length of the associated recess.
14. The support rod as defined in claim 10, wherein said spacer ribs are located at the boundary wall of said recess and serve to confine the adhesive material therein.
15. The support rod as defined in claim 1, wherein said body member is formed as a hollow profile member containing at least one internal compartment.
16. The support rod as defined in claim 1, wherein said edge reinforcement plate members are configured to possess a substantially flat rectangular shape.
17. The support rod as defined in claim 1, wherein said edge reinforcement means is a carbon fiber laminate.
18. A support rod for the harness frame of a loom possessing increased bending strength, comprising a support rod body member having a neutral bending axis, said body member being formed of a lightweight material possessing a relatively low modulus of elasticity, said body member further including external regions spaced remote from the neutral bending axis of the support rod, edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total crosssectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, and wherein said edge reinforcement means is a carbon fiber laminate.
19. A support rod for the harness frame of a loom possessing increased bending strength, comprising a support rod body member having a neutral bending axis, said body member being formed of a lightweight material possessing a relatively low modulus of elasticity, said body member further including external regions spaced remote from the neutral bending axis of the support rod, edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total cross-sectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, and wherein said material of body member is a fiber reinforced plastic.
20. A support rod for the harness frame of a loom possessing increased bending strength, comprising a support rod body member having a neutral bending axis, said body member being formed of a lightweight material posseSsing a relatively low modulus of elasticity, said body member further including external regions spaced remote from the neutral bending axis of the support rod, edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total cross-sectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, at least one recess for receiving each edge reinforcement means provided at said at least one external region, a thermally hardenable adhesive material interposed at the region of said recess for bonding said edge reinforcement means with the body member of the support rod, and a glass fiber-reinforced material layer containing the adhesive material located in said recess between said edge reinforcement means and said body member for maintaining the adhesive material confined within said recess.
21. A support rod for the harness frame of a loom possessing increased bending strength, comprising a support rod body member having a neutral bending axis, said body member being formed of a lightweight material possessing a relatively low modulus of elasticity, said body member further including external regions spaced remote from the neutral bending axis of the support rod, edge reinforcement means provided for at least one of said external regions, said edge reinforcement means exhibiting a total cross-sectional area which is small in relation to the cross-sectional area of said body member, said edge reinforcement means being formed of a material different from the material of said body member and possessing a relatively high modulus of elasticity in relation to the modulus of elasticity of the material forming the body member, and wherein said body member possesses a substantially rectangular configuration and comprising a hollow profile member, said hollow profile member being provided with an integral support web, one of said edge reinforcement means providing a heddle stringing rail connected with said support web, said heddle stringing rail being disposed substantially in the vertically extending symmetrical plane of said hollow profile member, said external edges of said hollow profile member facing away from said heddle stringing rail being provided with recesses receiving additional edge reinforcement means.
22. The support rod as defined in claim 21, wherein the modulus of elasticity of the material forming said edge reinforcement means is at least three times greater than the modulus of elasticity of the material forming said body member.
23. The support rod as defined in claim 21, wherein said edge reinforcement means is formed of steel.
24. The support rod as defined in claim 21, wherein said edge reinforcement means is a carbon fiber laminate.
25. The support rod as defined in claim 21, wherein said body member is formed of a material containing at least aluminum.
26. The support rod as defined in claim 21, further including at least one recess for receiving each edge reinforcement means provided at said at least one external region, and a thermally hardenable adhesive material interposed at the region of said recess for bonding said edge reinforcement means with the body member of the support rod.
27. The support rod as defined in claim 26, further including spacer ribs disposed at the region of said recess.
28. The support rod as defined in claim 27, wherein said spacer ribs extend over the length of the associated recess.
29. The support rod as defined in claim 27, wherein said spacer ribs are located at the boundary wall of said recess and serve to confine the adhesive material therein.
30. The support rod as defined in claim 26, further including a glass fiber-reinforced material layer containing the adhesive materiaL located in said recess between said edge reinforcement means and said body member for maintaining the adhesive material confined within said recess.
31. The support rod as defined in claim 21, wherein said body member is formed as a hollow profile member containing at least one internal compartment.
US00197202A 1968-09-13 1971-11-10 Harness frame support rod possessing increased bending strength Expired - Lifetime US3754577A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH1422468A CH525352A (en) 1968-09-13 1968-09-13 Rod with high flexural rigidity and use of the same

Publications (1)

Publication Number Publication Date
US3754577A true US3754577A (en) 1973-08-28

Family

ID=4398998

Family Applications (1)

Application Number Title Priority Date Filing Date
US00197202A Expired - Lifetime US3754577A (en) 1968-09-13 1971-11-10 Harness frame support rod possessing increased bending strength

Country Status (7)

Country Link
US (1) US3754577A (en)
JP (1) JPS5514184B1 (en)
CH (1) CH525352A (en)
DE (2) DE6929985U (en)
FR (1) FR2018050A1 (en)
GB (1) GB1279860A (en)
SE (1) SE363357B (en)

Cited By (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4106530A (en) * 1976-10-22 1978-08-15 Kaufmann Frank H Heddle frame
US4112983A (en) * 1976-07-08 1978-09-12 Ruti Machinery Works Ltd Picking bands and drive arrangement for gripper weaving machine
DE2839488A1 (en) * 1978-09-11 1980-03-13 Schmeing Geb WEBSITE
DE2933442A1 (en) * 1979-07-13 1981-01-22 Grob & Co Ag WEBSITE
US4390045A (en) * 1979-09-26 1983-06-28 Grob & Co. Aktiengesellschaft Heddle frame stave
DE3323224A1 (en) * 1982-06-30 1984-01-05 Steel Heddle Mfg. Co., 29602 Greenville, S.C. EXTRUDED WEBBAR BRACKET AND COVER
US4476900A (en) * 1982-01-27 1984-10-16 Steel Heddle Manufacturing Company Composite heddle rod
US4484604A (en) * 1983-09-06 1984-11-27 Steel Heddle Mfg. Co. Composite dual-face heddle frame slat
US4633916A (en) * 1985-06-24 1987-01-06 Rast John L Roll-formed shear-resistant frame slat
US4901767A (en) * 1987-01-28 1990-02-20 Grob & Co. Aktiengesellschaft Supporting bar of a heddle frame
US4913194A (en) * 1988-11-18 1990-04-03 Steel Heddle Mfg. Co. Light weight heddle frame assembly slat
US4913193A (en) * 1989-02-14 1990-04-03 Steel Heddle Mfg. Co. Light weight heddle support bar
US4993122A (en) * 1988-11-04 1991-02-19 Reiter Machine Works, Ltd. Nipper for a combing machine using bonded fiber material
US5183082A (en) * 1991-01-19 1993-02-02 Grob & Co. Aktiengesellschaft Frame stave for a heddle frame
US5280810A (en) * 1992-07-16 1994-01-25 Nankai Kogyo Kabushiki Kaisha Heald frame with stabilizer rod
WO1997025465A1 (en) * 1996-01-13 1997-07-17 Firma Schmeing Gmbh & Co. Process for producing a heald shaft for weaving shafts out of a metal hollow section
DE19625076A1 (en) * 1996-01-13 1997-07-17 Schmeing Gmbh & Co Process for producing a heald frame for heald frames from a hollow metal profile
EP1331293A1 (en) * 2002-01-25 2003-07-30 Etablissements Burckle et Compagnie S.A.S. Method of fabricating a heddle frame slat for the heddle frame of a weaving machine and a heddle frame slat obtained by such method
EP1516948A2 (en) * 2003-09-18 2005-03-23 Groz-Beckert KG Heddle frame slat
US20050081941A1 (en) * 2003-10-21 2005-04-21 Groz-Beckert Kg Heald shaft of composite construction
US20050109417A1 (en) * 2003-10-07 2005-05-26 Groz-Beckert Kg Shaft rod for weaving machines
WO2006008043A1 (en) * 2004-07-16 2006-01-26 Picanol N.V. Heald shaft comprising a heald support rod
WO2006008042A2 (en) * 2004-07-16 2006-01-26 Picanol N.V. Heald shaft comprising frame pieces and heald support rods
DE102004036025A1 (en) * 2004-07-16 2006-02-09 Picanol N.V. Loom heald frame, with a frame section and a heald slide rod, has a longitudinal bar fastener for the slide rod within a frame groove fitted with projecting studs through openings in the slide rod
US20060102243A1 (en) * 2004-11-17 2006-05-18 Groz-Beckert Kg Shaft rod for heald shafts
DE102004059319A1 (en) * 2004-12-02 2006-06-08 Picanol N.V. heald
DE102004059819A1 (en) * 2004-12-03 2006-06-08 Picanol N.V. Loom heald frame, with a frame section and a heald slide rod, has a longitudinal bar fastener for the slide rod within a frame groove fitted with projecting studs through openings in the slide rod
WO2007006539A1 (en) * 2005-07-12 2007-01-18 Picanol N.V. Weaving frame for a weaving machine
US20070062596A1 (en) * 2005-09-16 2007-03-22 Groz-Beckert Kg Shaft rod and heald shaft
WO2008040559A1 (en) * 2006-10-05 2008-04-10 Picanol N.V. Heddle frame with reinforcing profile for a weaving machine
DE102006057256A1 (en) * 2006-11-22 2008-05-29 Picanol N.V. heald
JP2009068158A (en) * 2007-09-11 2009-04-02 Groz-Beckert Kg Glued heald mounting rail
US7610940B2 (en) * 2005-11-23 2009-11-03 Promatech S.P.A. Crossbar for heald-carrying frames of weaving looms with improved attachment of the heald-carrying plate
CN101173414B (en) * 2006-11-03 2010-07-14 丁宏利 Fly-shuttle loom harness frame position limiter
WO2011023383A1 (en) 2009-08-31 2011-03-03 Picanol Heald frame for a weaving machine
US20110198890A1 (en) * 2010-02-17 2011-08-18 Gm Global Technology Operations, Inc. Closed-section structural member for a vehicle
WO2013064355A2 (en) 2011-11-03 2013-05-10 Picanol Heald frame with a reinforcement profile
US8733371B1 (en) 2011-04-14 2014-05-27 Jan Rassman Apparatus and method for the controlled delivery of skin products and therapeutic agents
FR3011864A1 (en) * 2013-10-10 2015-04-17 Jacques Sarrat HARDWOOD MATRIX COMPOSITE BEAM IN ALUMINUM EXTRUDE ARMORED WITH FULLY COATED CARBON FIBER PROFILES
US9293729B2 (en) * 2013-10-14 2016-03-22 Samsung Display Co., Ltd. Organic light emitting diode display package with sealant and adhesive reinforcing member
IT201900008379A1 (en) 2019-06-07 2020-12-07 Itema Spa SQUARE-LICCIO CROSSBAR FOR WEAVING FRAMES WITH IMPROVED RIGIDITY
EP3792382A1 (en) * 2019-09-10 2021-03-17 Groz-Beckert KG Reed with plurality of strips

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3948296A (en) * 1972-06-30 1976-04-06 Grob & Co. Aktiengesellschaft Frame stave for heald frame of weaving machine
CH553267A (en) * 1972-06-30 1974-08-30 Grob & Co Ag STAFF FOR WEAVING.
CH610993A5 (en) * 1976-06-08 1979-05-15 Sulzer Ag
JPH0281989U (en) * 1988-12-12 1990-06-25
DE10343159B4 (en) * 2003-09-18 2005-10-06 Groz-Beckert Kg Cross member of heald frame for a loom includes a recess shaped to hold a reinforcing member in position while the glue is setting
EP2037020B1 (en) * 2007-09-12 2015-11-04 Groz-Beckert KG Profile rod and support rod for a heald shaft

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB412706A (en) * 1932-03-10 1934-07-05 David & Gisclon Improvements in heddle frames for looms
US2674237A (en) * 1950-09-19 1954-04-06 Melville F Peters Ignition control
FR1181962A (en) * 1956-09-04 1959-06-19 Frohlich A G E Blade for looms
US3412762A (en) * 1966-11-21 1968-11-26 Robert M. Goodman Jr. Heddle frame assembly having an improved heddle rod support
US3604469A (en) * 1967-11-17 1971-09-14 Contraves Ag Loom harness

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB412706A (en) * 1932-03-10 1934-07-05 David & Gisclon Improvements in heddle frames for looms
US2674237A (en) * 1950-09-19 1954-04-06 Melville F Peters Ignition control
FR1181962A (en) * 1956-09-04 1959-06-19 Frohlich A G E Blade for looms
US3412762A (en) * 1966-11-21 1968-11-26 Robert M. Goodman Jr. Heddle frame assembly having an improved heddle rod support
US3604469A (en) * 1967-11-17 1971-09-14 Contraves Ag Loom harness

Cited By (82)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4112983A (en) * 1976-07-08 1978-09-12 Ruti Machinery Works Ltd Picking bands and drive arrangement for gripper weaving machine
US4106530A (en) * 1976-10-22 1978-08-15 Kaufmann Frank H Heddle frame
US4106529A (en) * 1976-10-22 1978-08-15 Steel Heddle Manufacturing Company Heddle frame
DE2839488A1 (en) * 1978-09-11 1980-03-13 Schmeing Geb WEBSITE
EP0008793A1 (en) * 1978-09-11 1980-03-19 Gebrüder Schmeing Frame for looms
DE2933442A1 (en) * 1979-07-13 1981-01-22 Grob & Co Ag WEBSITE
US4387742A (en) * 1979-07-13 1983-06-14 Grob & Co. Aktiengesellschaft Weaving heddle frame
US4390045A (en) * 1979-09-26 1983-06-28 Grob & Co. Aktiengesellschaft Heddle frame stave
US4476900A (en) * 1982-01-27 1984-10-16 Steel Heddle Manufacturing Company Composite heddle rod
DE3323224A1 (en) * 1982-06-30 1984-01-05 Steel Heddle Mfg. Co., 29602 Greenville, S.C. EXTRUDED WEBBAR BRACKET AND COVER
US4492256A (en) * 1982-06-30 1985-01-08 Steel Heddle Manufacturing Company Extruded heddle rod and cap
US4484604A (en) * 1983-09-06 1984-11-27 Steel Heddle Mfg. Co. Composite dual-face heddle frame slat
US4633916A (en) * 1985-06-24 1987-01-06 Rast John L Roll-formed shear-resistant frame slat
US4901767A (en) * 1987-01-28 1990-02-20 Grob & Co. Aktiengesellschaft Supporting bar of a heddle frame
US4993122A (en) * 1988-11-04 1991-02-19 Reiter Machine Works, Ltd. Nipper for a combing machine using bonded fiber material
US4913194A (en) * 1988-11-18 1990-04-03 Steel Heddle Mfg. Co. Light weight heddle frame assembly slat
US4913193A (en) * 1989-02-14 1990-04-03 Steel Heddle Mfg. Co. Light weight heddle support bar
US5183082A (en) * 1991-01-19 1993-02-02 Grob & Co. Aktiengesellschaft Frame stave for a heddle frame
US5280810A (en) * 1992-07-16 1994-01-25 Nankai Kogyo Kabushiki Kaisha Heald frame with stabilizer rod
WO1997025465A1 (en) * 1996-01-13 1997-07-17 Firma Schmeing Gmbh & Co. Process for producing a heald shaft for weaving shafts out of a metal hollow section
DE19625076A1 (en) * 1996-01-13 1997-07-17 Schmeing Gmbh & Co Process for producing a heald frame for heald frames from a hollow metal profile
DE19625076C2 (en) * 1996-01-13 1998-11-26 Schmeing Gmbh & Co Process for producing a heald frame for heald frames from a hollow metal profile
CN1045641C (en) * 1996-01-13 1999-10-13 施梅因两合公司 Process for producing coir frame monofilament rod f metal hollow section
US6076250A (en) * 1996-01-13 2000-06-20 Firma Schmeing Gmbh & Co. Process for producing a heald shaft for weaving shafts out of a metal hollow section
EP1331293A1 (en) * 2002-01-25 2003-07-30 Etablissements Burckle et Compagnie S.A.S. Method of fabricating a heddle frame slat for the heddle frame of a weaving machine and a heddle frame slat obtained by such method
FR2835264A1 (en) * 2002-01-25 2003-08-01 Burckle Et Cie Ets METHOD FOR MANUFACTURING A BUSHING FOR A WEAVING MACHINE SMOOTH FRAME AND A BUSHING OBTAINED BY SAID METHOD
US6926042B2 (en) 2002-01-25 2005-08-09 Stäubli Alsace Method for manufacturing a crossbeam for a heddle frame of a loom and crossbeam obtained by said method
US20030140981A1 (en) * 2002-01-25 2003-07-31 Etablissements Burckle Et Compagnie S.A.S. Method for manufacturing a crossbeam for a heddle frame of a loom and crossbeam obtained by said method
EP1516948A2 (en) * 2003-09-18 2005-03-23 Groz-Beckert KG Heddle frame slat
US20050061385A1 (en) * 2003-09-18 2005-03-24 Groz-Beckert Kg Shaft road
EP1516948A3 (en) * 2003-09-18 2005-11-30 Groz-Beckert KG Heddle frame slat
US7231942B2 (en) * 2003-09-18 2007-06-19 Groz-Beckert Kg Shaft rod
US20050109417A1 (en) * 2003-10-07 2005-05-26 Groz-Beckert Kg Shaft rod for weaving machines
US7290569B2 (en) * 2003-10-07 2007-11-06 Groz-Beckert Kg Shaft rod for weaving machines
US7114528B2 (en) * 2003-10-21 2006-10-03 Groz-Beckert Kg Heald shaft of composite construction
US20050081941A1 (en) * 2003-10-21 2005-04-21 Groz-Beckert Kg Heald shaft of composite construction
DE10349382B3 (en) * 2003-10-21 2005-06-09 Groz-Beckert Kg Weave in composite construction
WO2006008042A2 (en) * 2004-07-16 2006-01-26 Picanol N.V. Heald shaft comprising frame pieces and heald support rods
WO2006008042A3 (en) * 2004-07-16 2006-04-13 Picanol Nv Heald shaft comprising frame pieces and heald support rods
US20070181206A1 (en) * 2004-07-16 2007-08-09 Joost Deseyne Heald shaft comprising a heald support rod
EP1953278A3 (en) * 2004-07-16 2008-09-03 Picanol N.V. Heald shaft with a heald support rod
DE102004036025A1 (en) * 2004-07-16 2006-02-09 Picanol N.V. Loom heald frame, with a frame section and a heald slide rod, has a longitudinal bar fastener for the slide rod within a frame groove fitted with projecting studs through openings in the slide rod
EP1953278A2 (en) 2004-07-16 2008-08-06 Picanol N.V. Heald shaft with plaiting load rod
DE102004035996A1 (en) * 2004-07-16 2006-02-02 Picanol N.V. Weave with heald bar
WO2006008043A1 (en) * 2004-07-16 2006-01-26 Picanol N.V. Heald shaft comprising a heald support rod
US20060102243A1 (en) * 2004-11-17 2006-05-18 Groz-Beckert Kg Shaft rod for heald shafts
CN1776051B (en) * 2004-11-17 2010-12-29 格罗兹-贝克特公司 Shaft rod for heald shafts
US7264022B2 (en) * 2004-11-17 2007-09-04 Groz-Beckert Ag Shaft rod for heald shafts
DE102004059319A1 (en) * 2004-12-02 2006-06-08 Picanol N.V. heald
US7568506B2 (en) * 2004-12-02 2009-08-04 Picanol N.V. Heald frame
US20080110520A1 (en) * 2004-12-02 2008-05-15 Picanol N.V. Heald Frame
WO2006058565A1 (en) * 2004-12-02 2006-06-08 Picanol N.V. Heald frame
JP2008522047A (en) * 2004-12-02 2008-06-26 ピカノール エヌ. ヴィ. Frame
DE102004059819A1 (en) * 2004-12-03 2006-06-08 Picanol N.V. Loom heald frame, with a frame section and a heald slide rod, has a longitudinal bar fastener for the slide rod within a frame groove fitted with projecting studs through openings in the slide rod
BE1016677A3 (en) * 2005-07-12 2007-04-03 Picanol Nv WEAVING FRAMEWORK FOR A WEAVING MACHINE.
WO2007006539A1 (en) * 2005-07-12 2007-01-18 Picanol N.V. Weaving frame for a weaving machine
US20070062596A1 (en) * 2005-09-16 2007-03-22 Groz-Beckert Kg Shaft rod and heald shaft
US7823608B2 (en) * 2005-09-16 2010-11-02 Groz-Beckert Kg Shaft rod and heald shaft
US7610940B2 (en) * 2005-11-23 2009-11-03 Promatech S.P.A. Crossbar for heald-carrying frames of weaving looms with improved attachment of the heald-carrying plate
US7866349B2 (en) 2006-10-05 2011-01-11 Picanol N.V. and Verbrugge N.V. Heddle frame with reinforcing profile for a weaving machine
US20100043907A1 (en) * 2006-10-05 2010-02-25 Joost Deseyne Heddle frame with reinforcing profile for a weaving machine
BE1017334A3 (en) * 2006-10-05 2008-06-03 Picanol Nv WEAVING FRAME WITH REINFORCEMENT PROFILE FOR A WEAVING MACHINE.
WO2008040559A1 (en) * 2006-10-05 2008-04-10 Picanol N.V. Heddle frame with reinforcing profile for a weaving machine
CN101535541B (en) * 2006-10-05 2011-09-07 必佳乐有限公司 Heddle frame with reinforcing profile for a weaving machine
CN101173414B (en) * 2006-11-03 2010-07-14 丁宏利 Fly-shuttle loom harness frame position limiter
DE102006057256A1 (en) * 2006-11-22 2008-05-29 Picanol N.V. heald
JP2009068158A (en) * 2007-09-11 2009-04-02 Groz-Beckert Kg Glued heald mounting rail
WO2011023383A1 (en) 2009-08-31 2011-03-03 Picanol Heald frame for a weaving machine
BE1018874A3 (en) * 2009-08-31 2011-10-04 Picanol Nv WEAVING FRAMEWORK FOR A WEAVING MACHINE.
US20110198890A1 (en) * 2010-02-17 2011-08-18 Gm Global Technology Operations, Inc. Closed-section structural member for a vehicle
US8733371B1 (en) 2011-04-14 2014-05-27 Jan Rassman Apparatus and method for the controlled delivery of skin products and therapeutic agents
WO2013064355A2 (en) 2011-11-03 2013-05-10 Picanol Heald frame with a reinforcement profile
CN104024500A (en) * 2011-11-03 2014-09-03 必佳乐公司 Heald frame with a reinforcement profile
CN104024500B (en) * 2011-11-03 2016-01-20 必佳乐公司 There is the heald frame of reinforced section
FR3011864A1 (en) * 2013-10-10 2015-04-17 Jacques Sarrat HARDWOOD MATRIX COMPOSITE BEAM IN ALUMINUM EXTRUDE ARMORED WITH FULLY COATED CARBON FIBER PROFILES
US9293729B2 (en) * 2013-10-14 2016-03-22 Samsung Display Co., Ltd. Organic light emitting diode display package with sealant and adhesive reinforcing member
IT201900008379A1 (en) 2019-06-07 2020-12-07 Itema Spa SQUARE-LICCIO CROSSBAR FOR WEAVING FRAMES WITH IMPROVED RIGIDITY
CN112048800A (en) * 2019-06-07 2020-12-08 意达股份公司 Harness frame cross bar for loom with improved rigidity
EP3748056A1 (en) 2019-06-07 2020-12-09 ITEMA S.p.A. Heald frame crossbar with improved rigidity for weaving looms
EP3792382A1 (en) * 2019-09-10 2021-03-17 Groz-Beckert KG Reed with plurality of strips
WO2021048131A1 (en) * 2019-09-10 2021-03-18 Groz-Beckert Kg Reed comprising a multiplicity of slats
US20220316107A1 (en) * 2019-09-10 2022-10-06 Groz-Beckert Kg Reed Comprising a Multiplicity of Slats

Also Published As

Publication number Publication date
GB1279860A (en) 1972-06-28
DE1938554A1 (en) 1970-04-02
DE6929985U (en) 1974-11-07
JPS5514184B1 (en) 1980-04-14
FR2018050A1 (en) 1970-05-29
CH525352A (en) 1972-07-15
SE363357B (en) 1974-01-14

Similar Documents

Publication Publication Date Title
US3754577A (en) Harness frame support rod possessing increased bending strength
US5100713A (en) Reinforcing woven fabric and preformed material, fiber reinforced composite material and beam using it
US3219333A (en) Bar-shaped spring element or the like made from resinous material
CA2716287A1 (en) Aircraft opening panel, especially an airplane cabin door
CA1310503C (en) Natural stone element for lining facades
JPS60233254A (en) Wall element
CN111206722A (en) Fiber composite material
US4913194A (en) Light weight heddle frame assembly slat
US3889721A (en) Intermediate connector for heddle supporting beam
US5345974A (en) Heald supporting frame
US3984266A (en) Process for bonding a ferro-cement structure with fiberglass reinforced plastic
DE3302554A1 (en) UPPER FRAME
US4530871A (en) Ski construction
US4762307A (en) Leaf spring of plastic material and method for its manufacture
CN110185219A (en) A kind of decoration integrated system of architectural exterior insulation
US2601873A (en) Loom harness
JPS6223139B2 (en)
GB2156166A (en) Improvements in electrodynamic shakers
JP3227603U (en) Heddle frame crossbar for weaving machines with improved rigidity
JPS62156331A (en) Heald frame member for loom
US9006119B2 (en) Composite material, a structural element comprised of the composite material, an airplane wing spar and their methods of production
JP2006138040A (en) Heald frame made of fiber-reinforced composite material
CN218436362U (en) Reinforced carbon fiber structure and reinforcing rib applying same
CN215243408U (en) High-temperature-resistant cushion block
US3071325A (en) Insulating fish plates