CA1083371A - Joint structure and method of joining - Google Patents
Joint structure and method of joiningInfo
- Publication number
- CA1083371A CA1083371A CA327,743A CA327743A CA1083371A CA 1083371 A CA1083371 A CA 1083371A CA 327743 A CA327743 A CA 327743A CA 1083371 A CA1083371 A CA 1083371A
- Authority
- CA
- Canada
- Prior art keywords
- universal joint
- cavity
- shaft member
- shaft
- joint member
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
- F16D3/16—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts
- F16D3/26—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected
- F16D3/38—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another
- F16D3/40—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another with intermediate member provided with two pairs of outwardly-directed trunnions on intersecting axes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C3/00—Shafts; Axles; Cranks; Eccentrics
- F16C3/02—Shafts; Axles
- F16C3/023—Shafts; Axles made of several parts, e.g. by welding
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C3/00—Shafts; Axles; Cranks; Eccentrics
- F16C3/02—Shafts; Axles
- F16C3/026—Shafts made of fibre reinforced resin
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
- F16D1/064—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end non-disconnectable
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
- F16D1/08—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end with clamping hub; with hub and longitudinal key
- F16D1/0805—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end with clamping hub; with hub and longitudinal key with radial clamping due to deformation of a resilient body or a body of fluid
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
- F16D3/16—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts
- F16D3/26—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected
- F16D3/38—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another
- F16D3/382—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another constructional details of other than the intermediate member
- F16D3/387—Fork construction; Mounting of fork on shaft; Adapting shaft for mounting of fork
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C2326/00—Articles relating to transporting
- F16C2326/01—Parts of vehicles in general
- F16C2326/06—Drive shafts
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Ocean & Marine Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Moulding By Coating Moulds (AREA)
- Standing Axle, Rod, Or Tube Structures Coupled By Welding, Adhesion, Or Deposition (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
ABSTRACT
A tubular shaft member and a universal joint member are connected together without the use of welding by interfitting the shaft member and the universal joint member so as to leave a cavity into which adhesive is injected through one opening whilst air is expelled through another opening, the adhesive then being cured. The cavity may be formed by moulding grooves in one of the members.
A tubular shaft member and a universal joint member are connected together without the use of welding by interfitting the shaft member and the universal joint member so as to leave a cavity into which adhesive is injected through one opening whilst air is expelled through another opening, the adhesive then being cured. The cavity may be formed by moulding grooves in one of the members.
Description
This invention relates to universal joint and shaft assemblies and methods of making same. The invention has been developed primarily for application to assemblies of this kind for use in motor road or other automotive vehicles for trans-mitting the drive from the prime mover to driving wheels either at the rear or at the front of the vehicle.
It is desirable to avoid or minimise vibration due to an out-of-balance mass in such assembly, a condition which exists when the combined centre of mass of the universal joint and the shaft member is offset radially from, i.e. is eccentric with respect to, the axis about which the shaft member and the member of the universal joint to which the shaft is secured rotate.
Such eccentricity can be brought about by the following causes. Firstly, the axis about which the assembly of shaft -member and the member of the universal joint connected thereto actually rotates is determined by the axis of rotation of the other member of the universal joint, and eccentricity may be produced by the dimensional tolerances in the universal joint 20 itself and the accuracy of fit of the universal joint members F-with respect to each other, i.e. presence or absence of any radial play or lost motion. Secondly, eccentricity may be -produced by reason of lack of accuracy with which the shaft member is connected to that part of the universal joint member ; to which it is connected and which usually is in the form of a stub shaft or spigot (of which the geometrical axis should ideally be coaxial with the actual axis of rotation of the universal joint). Thirdly, eccentricity may be produced by the actual centre of mass of the shaft member not lying on the geometrical axis of the shaft member, i.e. being offset radially therefrom.
In many cases the universal joint and shaft assembly is required to transmit drive to the input element of a combined : ~ ~r~
~ 2 ~ e~
\
108337~L
reduction and differential gear, the output elements of which are connected respectively to drive shafts which in turn are connected to the driving wheels of the vehicle, usually but not invariably at the rear thereof.
In such cases the shaft member which forms part of said assembly is normally termed the propeller shaft and rotates at an appreciably higher speed than does either of the drive shafts, typically three or four times as high, and consequently the elimination or minimisation of eccentricity giving rise to vibration is especially important.
Whilst continuous research and development has been directed -~to the elimination of the first cause of eccentricity referred to above, it is still necessary to accept that because of -production tolerances a significant number of assemblies will present some eccentricity arising from the first cause but -within said production tolerances. Furthermore, although normal methods of joining the shaft member to the universal joint member to which it is required to be connected, and in particular welding methods, have been carefully designed to avoid or minimise the second cause of eccentricity, here again it has to be accepted that in mass production some of the assemblies produced will exhibit eccentricity through this second cause.
With regard to the third cause of eccentricity, minimisation of this is often somewhat beyond the control of a manufacturer of assemblies of the kind specified in that reliance has to be placed upon the adherence to accurate tolerances by the suppliers of tubular stock from which such shaft members are made.
Accuracy in this respect is closely related to price and for the price which is acceptable, having regard to the product to be produced and its intended use, for example in mass produced motor vehicles, it is clearly necessary to tolerate some `
eccentricity from this third cause. ' The present invention is based upon the concept that _3_ ~. . , -` 11)83371 :
vibration arising from all three causes of eccentricity is capable of being reduced if the overall mass of the assembly, -~
and in particular the shaft member, can be reduced.
Conventional practice is to make the shaft member and the universal joint member to which it is to be connected of a ferrous metal such as steel or cast ironj and to join these member to each other by welding. ;
The use of welding technique for this purpose does represent a design constraint by reason of the fact that the 10 metals employed for two members must then necessarily be selec- -~
ted to have welding compatability. Further, the use of a fer-rous metal for the manufacture of the universal joint member (or indeed the universal joint as a whole) is consequent upon the necessity in a large number of applications, such as propeller shaft in universal joint assemblies for motor vehi-cles, to comply with strength requirements which have to be ;
met.
The present invention is based on the concept of reducin~ the overall mass of the assembly and involves the 20 provision of a mode of securement of the shaft member to the ~-universal joint member which overcomes the compatability constraint.
The present invention resides in a method of making an assembly of a shaft member and a universal joint member characterized in that it comprises the steps of~
A. providing a shaft member of tubular form and a universal joint member with a part which interfits with the shaft member, B. forming at least one of said parts to define, in `- 30 combination with the other of said parts, a cavity for recei-` ving an adhesive substance, said cavity being of elongate form and extending a plurality of times around the circumference of the interface between the interfitting parts of the shaft and - .
. ~", ~ `
1~8337~
universal joint member, ana having first and second openings communicating with it at opposite ends of the cavity, C. fitting such shaft member and the universal joint member together, D. injecting the adhesive substance through the first said opening into the cavity, thus expelling air from the cavity until the cavity is full of the adhesive substance, E. subjecting the assembly to treatment to cure the adhesive substance and establish a bond between the shaft and 10 universal joint member. -The invention also extends to an assembly of a shaft member and a universal joint member, characterized in that the members have axially interfitting parts with overlapping cir- :
cumferentially extending faces, said faces defining a ca~ity :
which is of elongate form extending a plurality of times around said circumferentially extending faces and in which is received an adhesive substance which secures said members:to~
gether, said cavity having an inlet opening and a vent opening communicating with it at spaced positions, said adhesive sub-stance having been injected through said inlet opening.
Embodiments of assemblies in accordance with the invention and methods of making such embodiments will now be described, by way of example, with reference to the accompany-ing drawings wherein:-Figure 1 is a view in vertical diametral section of a portion of a shaft and universal joint assembly showing the connection of the shaft member to one of the members of the universal joint and forming a first embodiment of the inven-tion;
Figures 2 and 3 are transverse cross-sectional views in the planes B D and A C respectively shown in Figure l;
Figure 4 is a view similar to Figure 1 illustrating a second embodiment and method of making same;
~S~
8337~ .
Figure 5 iS a vieW illustrating the application of material to a mandrel for making the shaft member of the embodiment of Figure 4 and forming an internal cavity therein. .
Referring firstly to Figure 1, the assembly comprises a universal joint yoke member 112 and a shaft member 111. For -5a-`` 1083371 convenience only one end portion of the shaft member is shown.
A like universal joint member may be provided at the opposite end or according to requirements this other end may have other means for connecting it in the drive or transmission line. The universal joint member forms part of a universal joint of the Hookes type comprising yoke members (of which only member 112 is shown) including respective laterally spaced axially projecting yoke arms 114, connected by base parts 116, and coupled together by a connecting member (not shown) having two pairs of radially projecting spigots engaged in openings in the yoke arms through the intermediary of bearings.
All of the members of the universal joint may be formed of a ferrous metal by casting, forging or fabricating methods in order to provide the necessary strength for applications such `
as propeller shaft and universal joint assemblies for motor vehicles.
The shaft member 111 is formed of a light weight material, for example aluminium alloy, such shaft member being of tubular `;
form.
The shaft member 111 and the member 112 are secured in assembled relationship by the provision of respective axially interfitting parts llla and 112a, the former comprising a non-tapering, i.e. cylindrical, integral end portion of the shaft, and the latter comprising a spigot part 112a integral with the -. .; .
base part 116 and having a cylindrical external face.
Between respective portions the internal face of the part llla and the external face of the part 112a is interposed an adhesive substance 124.
This may be in the form of thermo-setting epoxy resin which is caused to set, after assembly of the parts, by subjecting it to a high temperature, typically 170C.
The shaft is assembled with its part llla over the spigot 112a.
, ;
.. . . . .
~08337~L
It will be noted that portions lllg, 112g and lllh, 112h of the adjacent axially and circumferentially extending surface of the parts llla, 112a are in direct contact with each other, i.e. without the intervention of any adhesive substances, and thereby provide accurate location of the parts llla, 112a in coaxial relation.
As a safeguard against axial separation of the parts llla, 112a these are formed with mutually cooperative formations to prevent such separation. Thus, the member 112 of the universal `
joint is formed with a groove 125 between the spigot 112a and the base 116, such groove presenting an axially facing shoulder ; 125a directed away from the main length of the shaft member 111 and which is engaged by a lip 126 at the free end of the tubular shaft member produced by acting mechanically onthe extremity of the shaft member by a pair of radially inwardly movable tools ;
such as 126a to produce permanent inward deformation.
The deformation of the shaft may be effected after heat treatment to effect setting of the adhesive substance, or during, or before such heat treatment as may be convenient.
If the shaft member 111 is made of an aluminium alloy there will be a temperature limit above which it should not be raised in order to avoid impairment of the mechanical properties, e.g.
strength of the shaft, typically this temperature would be in the region of 200C.
Heating, therefore, would then be in the range 170C to a temperature representing a suitable margin below 200C, such as 190C.
The heat treatment may be effected by a batch process, i.e.
~; placing a quantity of the universal joint and shaft assemblies in a chamber in which the atmospheric temperature is in the range appropriate to the adhesive and materials employed, or by passing the assemblies in succession through the chamber in which the atmosphere is raised to the appropriate temperature.
: 1083371 In the embodiment of Figure 1 the internal face of the part llla, and the external face of the part 112a, is of plane-faced form, but one or both of these parts could incorporate a system of depressions or channels as by knurling if desired.
The external face of the spigot part 112a incorporates a passageway system for the reception of the adhesive in liquid ;`
or other flowable form. Such passageway system may comprise a series of axially spaced circumferentially extending grooves 112c to 112f. The grooves 112e, 112f and 112c, 112 are connected at their lower sides by axially extending grooves such as 127 in Figure 2, while grooves 112d and 112e are connected ;
at their upper sides by an axially extending groove such as 128a in Figure 3. Grooves 128_, 128c aligned with groove 128a also exist in the planes A and B to provide respectively for the admission of adhesive to the groove system through an injection passageway 129, and for venting to the interior of the tubular shaft 111. Such injection can be effected by engaging an : ~
'~ injection nozzle 129c in the entrance of the passageway 129 and operating a pump forming part of the injection means. r`
The end part llla of the shaft 111 is a close sliding fit on the spigot part 112a and is coaxially located by direct contact over portions of the adjacent internal and external faces '~
between the grooves.
Alternatively the groove system may comprise a single `~
helical groove extending along the outer face of the spigot part 112a communicating at one end with the passageway 129 and at the . . .
opposite end with a venting groove such as 128 in the plane A.
In the embodiment illustrated in Figure 4 and the method of ~` making it illustrated in Figure 5, parts corresponding to those already described in preceding embodiment are designated by like reference numbers with the prefix 2 instead of 1 and the preceding description is to be deemed to apply, reference being made now principally to the differences.
1083371 ;
The tubular shaft member 211 which is made of an epoxy resin mixture reinforced with longitudinally extending fibres, for example carbon fibres, incorporates in its end part 211a a relatively wide shallow groove 230 of helical form for the reception of the adhesive substance 224, the latter being injected through an opening 229 in the opposite end of the groove 230 providing venting to the interior of khe shaft member 211.
As seen in Figure 5, the groove 230 is formed by winding a strip 231 of a material helically around a part of mandrel 232 upon which the shaft member 211 is moulded.
A suitable material for the helical strip 231 is a tape woven of "nylon", "terylene" or "dacron". These materials are capable of withstanding temperatures involved in curing the resin ~ ;~
component of the shaft member. ~ possible alternative to form the tape would be a metal foil.
The shaft member 211 may be formed by winding reinforcing fibres, for example glass fibres or carbon fibres 233, helically around the mandrel and over the strip 231, alternate layers being preferably wound helically in opposite hands or directions.
This step of the method is continued until a thickness nearly equal to the desired thickness of the shaft member is achieved and then axially extending reinforcement materials such as carbon fibres or glass fibres 234 are laid axially over the helical winding 233 already referred to and the whole is impregnated with the epoxy resin mixture, for example by applying it in flowable form by means of a brush 236.
The shaft member thus formed, and still retained on the mandrel 232, is then subjected to heating, e.g. by passing through an oven heated to a temperature of the order of 180C
to effect curing. The mandrel 232 is then removed axially leaving the strip 231 in place.
The strip 231 may be left in place until the shaft member is actually required to be assembled with its end part 211a in ,,,,, . . , , , , : ~
--` 1083371 axially interfitting relationship with the part 212a of the ~-associated universal joint. The tape is then effective to prevent contamination of the groove 230 by air borne dirt and/or moisture or other contaminants.
Immediately preparatory to axially interfitting assembly of said parts, the strip 231 is removed to expose a helical passageway 231a and axial interfitment is effected with the end of the shaft member abutting a flange portion 235 of the universal joint member 212. An adhesive substance 224, as previously mentioned, is then injected through the passageway 229a, air being expelled through vent opening 229_ at the opposite end of the passageway 231 and the resultant assembly subjected to suitable treatment, e.g. heating, to set the adhesive and secure the shaft member and universal joint member together.
Instead of a woven tape, any suitable strip material capable of holding its shape under the conditions of moulding and after ~ winding onto the mandrel may be employed, provided it is ;~ sufficiently flexible to permit it to be removed after the shaft member has been formed. Again, whilst the helical winding of the 20 strip material is especially convenient, removable material ;~
applied in a configuration to produce`a passageway system of some configuration other than helical may be employed if desired.
Furthermore, alternatively or in addition the part 212a of the universal joint member may incorporate a groove in its exterior surface.
Although the foregoing description reference has been made to the formation of the universal joint members from a ferrous metal, e.g. cast iron or steel, it is to be understood that where the torque to be transmitted admits the universal joint member could itself be formed of a light weight (low density) material. This could be an aluminium alloy. The universal joint member may be formed as a casting, and the joint between the shaft member and the universal joint member could be effected - : - ., ,, : ,, , ; , , ~ ;
as shown in any one of the preceding embodiments. `~
Further, the invention is of application to an assembly of a shaft with some other form of universal joint member, e.g.
one from a constant velocity universal joint having inner and outer members and torque transmitting rotary elements such as balls engaging in formations such as grooves in the inner and ;
outer members.`
A possible modification which may be made to the embodiment ~ ..is`
illustrated in Figures 1 to 3 relates to the arrangement by which the system of adhesive receiving grooves is vented to provide for egress of air from the grooves as adhesive is introduced. In the embodiment depicted in Figures 1 to 3, it is ;~
possible that adhesive escaping into the interior of the shaft i from groove 128c could become detached from the adhesive remaining in the groove and be free to move around inside the shaft, providing a potential source of noise in service. To ~-overcome this, venting may be arranged to occur to atmosphere ; outside the shaft. This may be done by extending the passageway 129 to open into the groove 112c most remote from the end of the shaft, whilst a vent groove communicates with groove 112f.
Alternatively, the same arrangement of passageway 129 could be employed as in Figure 1, with groove 112c communicating with a small aperture extending radially through the tubular end part llla of the shaft 111.
It is to be understood that, when we refer to the shaft member being made of a material having a substantially lower density than ferrous metals of which such member is normally made, we refer to the average density of the shaft member as a whole. In the case of a shaft member formed of a compositive material, a component or componenks of the shaft may, taken individually, present a density of the order of, or even greater than, the density of ferrous metals, and yet the shaft member as a whole have an average density less than that of such 10833~
ferrous metals. ~;
In the embodiment shown in Figure 4, a sealing component , of suitable form may be provided, if neceSsary, between the end of the shaft part 211a and the flange portion 235 of the .
universal joint member 212, to prevent leakage of adhesive at this point.
-12- ~: -.
,, , . , , , , . " . ~ , .. . ... . . ... . . . . . . .
It is desirable to avoid or minimise vibration due to an out-of-balance mass in such assembly, a condition which exists when the combined centre of mass of the universal joint and the shaft member is offset radially from, i.e. is eccentric with respect to, the axis about which the shaft member and the member of the universal joint to which the shaft is secured rotate.
Such eccentricity can be brought about by the following causes. Firstly, the axis about which the assembly of shaft -member and the member of the universal joint connected thereto actually rotates is determined by the axis of rotation of the other member of the universal joint, and eccentricity may be produced by the dimensional tolerances in the universal joint 20 itself and the accuracy of fit of the universal joint members F-with respect to each other, i.e. presence or absence of any radial play or lost motion. Secondly, eccentricity may be -produced by reason of lack of accuracy with which the shaft member is connected to that part of the universal joint member ; to which it is connected and which usually is in the form of a stub shaft or spigot (of which the geometrical axis should ideally be coaxial with the actual axis of rotation of the universal joint). Thirdly, eccentricity may be produced by the actual centre of mass of the shaft member not lying on the geometrical axis of the shaft member, i.e. being offset radially therefrom.
In many cases the universal joint and shaft assembly is required to transmit drive to the input element of a combined : ~ ~r~
~ 2 ~ e~
\
108337~L
reduction and differential gear, the output elements of which are connected respectively to drive shafts which in turn are connected to the driving wheels of the vehicle, usually but not invariably at the rear thereof.
In such cases the shaft member which forms part of said assembly is normally termed the propeller shaft and rotates at an appreciably higher speed than does either of the drive shafts, typically three or four times as high, and consequently the elimination or minimisation of eccentricity giving rise to vibration is especially important.
Whilst continuous research and development has been directed -~to the elimination of the first cause of eccentricity referred to above, it is still necessary to accept that because of -production tolerances a significant number of assemblies will present some eccentricity arising from the first cause but -within said production tolerances. Furthermore, although normal methods of joining the shaft member to the universal joint member to which it is required to be connected, and in particular welding methods, have been carefully designed to avoid or minimise the second cause of eccentricity, here again it has to be accepted that in mass production some of the assemblies produced will exhibit eccentricity through this second cause.
With regard to the third cause of eccentricity, minimisation of this is often somewhat beyond the control of a manufacturer of assemblies of the kind specified in that reliance has to be placed upon the adherence to accurate tolerances by the suppliers of tubular stock from which such shaft members are made.
Accuracy in this respect is closely related to price and for the price which is acceptable, having regard to the product to be produced and its intended use, for example in mass produced motor vehicles, it is clearly necessary to tolerate some `
eccentricity from this third cause. ' The present invention is based upon the concept that _3_ ~. . , -` 11)83371 :
vibration arising from all three causes of eccentricity is capable of being reduced if the overall mass of the assembly, -~
and in particular the shaft member, can be reduced.
Conventional practice is to make the shaft member and the universal joint member to which it is to be connected of a ferrous metal such as steel or cast ironj and to join these member to each other by welding. ;
The use of welding technique for this purpose does represent a design constraint by reason of the fact that the 10 metals employed for two members must then necessarily be selec- -~
ted to have welding compatability. Further, the use of a fer-rous metal for the manufacture of the universal joint member (or indeed the universal joint as a whole) is consequent upon the necessity in a large number of applications, such as propeller shaft in universal joint assemblies for motor vehi-cles, to comply with strength requirements which have to be ;
met.
The present invention is based on the concept of reducin~ the overall mass of the assembly and involves the 20 provision of a mode of securement of the shaft member to the ~-universal joint member which overcomes the compatability constraint.
The present invention resides in a method of making an assembly of a shaft member and a universal joint member characterized in that it comprises the steps of~
A. providing a shaft member of tubular form and a universal joint member with a part which interfits with the shaft member, B. forming at least one of said parts to define, in `- 30 combination with the other of said parts, a cavity for recei-` ving an adhesive substance, said cavity being of elongate form and extending a plurality of times around the circumference of the interface between the interfitting parts of the shaft and - .
. ~", ~ `
1~8337~
universal joint member, ana having first and second openings communicating with it at opposite ends of the cavity, C. fitting such shaft member and the universal joint member together, D. injecting the adhesive substance through the first said opening into the cavity, thus expelling air from the cavity until the cavity is full of the adhesive substance, E. subjecting the assembly to treatment to cure the adhesive substance and establish a bond between the shaft and 10 universal joint member. -The invention also extends to an assembly of a shaft member and a universal joint member, characterized in that the members have axially interfitting parts with overlapping cir- :
cumferentially extending faces, said faces defining a ca~ity :
which is of elongate form extending a plurality of times around said circumferentially extending faces and in which is received an adhesive substance which secures said members:to~
gether, said cavity having an inlet opening and a vent opening communicating with it at spaced positions, said adhesive sub-stance having been injected through said inlet opening.
Embodiments of assemblies in accordance with the invention and methods of making such embodiments will now be described, by way of example, with reference to the accompany-ing drawings wherein:-Figure 1 is a view in vertical diametral section of a portion of a shaft and universal joint assembly showing the connection of the shaft member to one of the members of the universal joint and forming a first embodiment of the inven-tion;
Figures 2 and 3 are transverse cross-sectional views in the planes B D and A C respectively shown in Figure l;
Figure 4 is a view similar to Figure 1 illustrating a second embodiment and method of making same;
~S~
8337~ .
Figure 5 iS a vieW illustrating the application of material to a mandrel for making the shaft member of the embodiment of Figure 4 and forming an internal cavity therein. .
Referring firstly to Figure 1, the assembly comprises a universal joint yoke member 112 and a shaft member 111. For -5a-`` 1083371 convenience only one end portion of the shaft member is shown.
A like universal joint member may be provided at the opposite end or according to requirements this other end may have other means for connecting it in the drive or transmission line. The universal joint member forms part of a universal joint of the Hookes type comprising yoke members (of which only member 112 is shown) including respective laterally spaced axially projecting yoke arms 114, connected by base parts 116, and coupled together by a connecting member (not shown) having two pairs of radially projecting spigots engaged in openings in the yoke arms through the intermediary of bearings.
All of the members of the universal joint may be formed of a ferrous metal by casting, forging or fabricating methods in order to provide the necessary strength for applications such `
as propeller shaft and universal joint assemblies for motor vehicles.
The shaft member 111 is formed of a light weight material, for example aluminium alloy, such shaft member being of tubular `;
form.
The shaft member 111 and the member 112 are secured in assembled relationship by the provision of respective axially interfitting parts llla and 112a, the former comprising a non-tapering, i.e. cylindrical, integral end portion of the shaft, and the latter comprising a spigot part 112a integral with the -. .; .
base part 116 and having a cylindrical external face.
Between respective portions the internal face of the part llla and the external face of the part 112a is interposed an adhesive substance 124.
This may be in the form of thermo-setting epoxy resin which is caused to set, after assembly of the parts, by subjecting it to a high temperature, typically 170C.
The shaft is assembled with its part llla over the spigot 112a.
, ;
.. . . . .
~08337~L
It will be noted that portions lllg, 112g and lllh, 112h of the adjacent axially and circumferentially extending surface of the parts llla, 112a are in direct contact with each other, i.e. without the intervention of any adhesive substances, and thereby provide accurate location of the parts llla, 112a in coaxial relation.
As a safeguard against axial separation of the parts llla, 112a these are formed with mutually cooperative formations to prevent such separation. Thus, the member 112 of the universal `
joint is formed with a groove 125 between the spigot 112a and the base 116, such groove presenting an axially facing shoulder ; 125a directed away from the main length of the shaft member 111 and which is engaged by a lip 126 at the free end of the tubular shaft member produced by acting mechanically onthe extremity of the shaft member by a pair of radially inwardly movable tools ;
such as 126a to produce permanent inward deformation.
The deformation of the shaft may be effected after heat treatment to effect setting of the adhesive substance, or during, or before such heat treatment as may be convenient.
If the shaft member 111 is made of an aluminium alloy there will be a temperature limit above which it should not be raised in order to avoid impairment of the mechanical properties, e.g.
strength of the shaft, typically this temperature would be in the region of 200C.
Heating, therefore, would then be in the range 170C to a temperature representing a suitable margin below 200C, such as 190C.
The heat treatment may be effected by a batch process, i.e.
~; placing a quantity of the universal joint and shaft assemblies in a chamber in which the atmospheric temperature is in the range appropriate to the adhesive and materials employed, or by passing the assemblies in succession through the chamber in which the atmosphere is raised to the appropriate temperature.
: 1083371 In the embodiment of Figure 1 the internal face of the part llla, and the external face of the part 112a, is of plane-faced form, but one or both of these parts could incorporate a system of depressions or channels as by knurling if desired.
The external face of the spigot part 112a incorporates a passageway system for the reception of the adhesive in liquid ;`
or other flowable form. Such passageway system may comprise a series of axially spaced circumferentially extending grooves 112c to 112f. The grooves 112e, 112f and 112c, 112 are connected at their lower sides by axially extending grooves such as 127 in Figure 2, while grooves 112d and 112e are connected ;
at their upper sides by an axially extending groove such as 128a in Figure 3. Grooves 128_, 128c aligned with groove 128a also exist in the planes A and B to provide respectively for the admission of adhesive to the groove system through an injection passageway 129, and for venting to the interior of the tubular shaft 111. Such injection can be effected by engaging an : ~
'~ injection nozzle 129c in the entrance of the passageway 129 and operating a pump forming part of the injection means. r`
The end part llla of the shaft 111 is a close sliding fit on the spigot part 112a and is coaxially located by direct contact over portions of the adjacent internal and external faces '~
between the grooves.
Alternatively the groove system may comprise a single `~
helical groove extending along the outer face of the spigot part 112a communicating at one end with the passageway 129 and at the . . .
opposite end with a venting groove such as 128 in the plane A.
In the embodiment illustrated in Figure 4 and the method of ~` making it illustrated in Figure 5, parts corresponding to those already described in preceding embodiment are designated by like reference numbers with the prefix 2 instead of 1 and the preceding description is to be deemed to apply, reference being made now principally to the differences.
1083371 ;
The tubular shaft member 211 which is made of an epoxy resin mixture reinforced with longitudinally extending fibres, for example carbon fibres, incorporates in its end part 211a a relatively wide shallow groove 230 of helical form for the reception of the adhesive substance 224, the latter being injected through an opening 229 in the opposite end of the groove 230 providing venting to the interior of khe shaft member 211.
As seen in Figure 5, the groove 230 is formed by winding a strip 231 of a material helically around a part of mandrel 232 upon which the shaft member 211 is moulded.
A suitable material for the helical strip 231 is a tape woven of "nylon", "terylene" or "dacron". These materials are capable of withstanding temperatures involved in curing the resin ~ ;~
component of the shaft member. ~ possible alternative to form the tape would be a metal foil.
The shaft member 211 may be formed by winding reinforcing fibres, for example glass fibres or carbon fibres 233, helically around the mandrel and over the strip 231, alternate layers being preferably wound helically in opposite hands or directions.
This step of the method is continued until a thickness nearly equal to the desired thickness of the shaft member is achieved and then axially extending reinforcement materials such as carbon fibres or glass fibres 234 are laid axially over the helical winding 233 already referred to and the whole is impregnated with the epoxy resin mixture, for example by applying it in flowable form by means of a brush 236.
The shaft member thus formed, and still retained on the mandrel 232, is then subjected to heating, e.g. by passing through an oven heated to a temperature of the order of 180C
to effect curing. The mandrel 232 is then removed axially leaving the strip 231 in place.
The strip 231 may be left in place until the shaft member is actually required to be assembled with its end part 211a in ,,,,, . . , , , , : ~
--` 1083371 axially interfitting relationship with the part 212a of the ~-associated universal joint. The tape is then effective to prevent contamination of the groove 230 by air borne dirt and/or moisture or other contaminants.
Immediately preparatory to axially interfitting assembly of said parts, the strip 231 is removed to expose a helical passageway 231a and axial interfitment is effected with the end of the shaft member abutting a flange portion 235 of the universal joint member 212. An adhesive substance 224, as previously mentioned, is then injected through the passageway 229a, air being expelled through vent opening 229_ at the opposite end of the passageway 231 and the resultant assembly subjected to suitable treatment, e.g. heating, to set the adhesive and secure the shaft member and universal joint member together.
Instead of a woven tape, any suitable strip material capable of holding its shape under the conditions of moulding and after ~ winding onto the mandrel may be employed, provided it is ;~ sufficiently flexible to permit it to be removed after the shaft member has been formed. Again, whilst the helical winding of the 20 strip material is especially convenient, removable material ;~
applied in a configuration to produce`a passageway system of some configuration other than helical may be employed if desired.
Furthermore, alternatively or in addition the part 212a of the universal joint member may incorporate a groove in its exterior surface.
Although the foregoing description reference has been made to the formation of the universal joint members from a ferrous metal, e.g. cast iron or steel, it is to be understood that where the torque to be transmitted admits the universal joint member could itself be formed of a light weight (low density) material. This could be an aluminium alloy. The universal joint member may be formed as a casting, and the joint between the shaft member and the universal joint member could be effected - : - ., ,, : ,, , ; , , ~ ;
as shown in any one of the preceding embodiments. `~
Further, the invention is of application to an assembly of a shaft with some other form of universal joint member, e.g.
one from a constant velocity universal joint having inner and outer members and torque transmitting rotary elements such as balls engaging in formations such as grooves in the inner and ;
outer members.`
A possible modification which may be made to the embodiment ~ ..is`
illustrated in Figures 1 to 3 relates to the arrangement by which the system of adhesive receiving grooves is vented to provide for egress of air from the grooves as adhesive is introduced. In the embodiment depicted in Figures 1 to 3, it is ;~
possible that adhesive escaping into the interior of the shaft i from groove 128c could become detached from the adhesive remaining in the groove and be free to move around inside the shaft, providing a potential source of noise in service. To ~-overcome this, venting may be arranged to occur to atmosphere ; outside the shaft. This may be done by extending the passageway 129 to open into the groove 112c most remote from the end of the shaft, whilst a vent groove communicates with groove 112f.
Alternatively, the same arrangement of passageway 129 could be employed as in Figure 1, with groove 112c communicating with a small aperture extending radially through the tubular end part llla of the shaft 111.
It is to be understood that, when we refer to the shaft member being made of a material having a substantially lower density than ferrous metals of which such member is normally made, we refer to the average density of the shaft member as a whole. In the case of a shaft member formed of a compositive material, a component or componenks of the shaft may, taken individually, present a density of the order of, or even greater than, the density of ferrous metals, and yet the shaft member as a whole have an average density less than that of such 10833~
ferrous metals. ~;
In the embodiment shown in Figure 4, a sealing component , of suitable form may be provided, if neceSsary, between the end of the shaft part 211a and the flange portion 235 of the .
universal joint member 212, to prevent leakage of adhesive at this point.
-12- ~: -.
,, , . , , , , . " . ~ , .. . ... . . ... . . . . . . .
Claims (8)
PROPERTY OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A method of making an assembly of a shaft member and a universal joint member characterized in that it compri-ses the steps of:-A. providing a shaft member of tubular form and a universal joint member with a part which interfits with the shaft member, B. forming at least one of said parts to define, in combination with the other of said parts, a cavity for recei-ving an adhesive substance, said cavity being of elongate form and extending a plurality of times around the circumference of the interface between the interfitting parts of the shaft and universal joint member, and having first and second openings communicating with it at opposite ends of the cavity, C. fitting such shaft member and the universal joint member together, D. injecting the adhesive substance through the first said opening into the cavity, thus expelling air from the cavity until the cavity is full of the adehsive substance, E. subjecting the assembly to treatment to cure the adhesive substance and establish a bond between the shaft and universal joint member.
2. A method according to Claim 1, further charac-terized in that at least one of said shaft member and universal joint member is provided with a plurality of circumferentially extending axially spaced grooves, interconnected by axially extending grooves, to define said cavity, said first and second openings communicating with respective ones of said grooves, and wherein said adhesive substance during injection thereof successively fills said grooves.
3. A method according to Claim 1, further charac-terized in that at least one of said shaft member and universal joint member is provided with a helical groove defining said cavity with said first and second openings communicating with respective ends of said groove, said adhesive substance during injection thereof filling said groove from one end to the other end thereof.
4. A method according to Claim 1 or Claim 3, further characterized by forming at least one of said shaft member and universal joint member by a moulding operation, and incorpora-ting in said member during such moulding a piece of material which is removed to define said cavity prior to assembly of said members.
5. A method according to Claim 4, further character-ized in that said shaft member is formed by applying reinfor-cing fibres to a mandrel impregnating such fibres with a syn-thetic resin material, and curing said resin to form the shaft member, a strip of material, constituting said removable material, being wound on the mandrel prior to the application of fibres thereto.
6. An assembly of a shaft member and a universal joint member, characterized in that the members have axially interfitting parts with overlapping circumferentially extending faces, said faces defining a cavity which is of elongate form extending a plurality of times around said circumferentially extending faces and in which is received an adhesive substance which secures said members together, said cavity having an in-let opening and a vent opening communicating with it at spaced positions, said adhesive substance having been injected through said inlet opening.
7. An assembly according to Claim 6, further charac-terized in that said cavity is defined by a plurality of axially spaced, circumferentially extending grooves intercon-nected by axially extending grooves, said inlet and vent open-ings communicating with end ones of said grooves.
8. An assembly according to Claim 6, further char-acterized in that said cavity is defined by a helically exten-ding groove, said inlet and vent openings communicating with opposite ends of said groove.
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB26244/76 | 1976-06-24 | ||
GB26244/76A GB1585163A (en) | 1976-06-24 | 1976-06-24 | Universal joint and shaft assemblies |
GB635477 | 1977-02-15 | ||
GB1335277 | 1977-03-30 | ||
GB13352/77 | 1977-03-30 |
Publications (1)
Publication Number | Publication Date |
---|---|
CA1083371A true CA1083371A (en) | 1980-08-12 |
Family
ID=27254811
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA281,251A Expired CA1068501A (en) | 1976-06-24 | 1977-06-23 | Joint structure and method of joining |
CA327,743A Expired CA1083371A (en) | 1976-06-24 | 1979-05-16 | Joint structure and method of joining |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA281,251A Expired CA1068501A (en) | 1976-06-24 | 1977-06-23 | Joint structure and method of joining |
Country Status (10)
Country | Link |
---|---|
JP (1) | JPS53361A (en) |
CA (2) | CA1068501A (en) |
DE (1) | DE2728306C2 (en) |
ES (2) | ES459998A1 (en) |
FR (1) | FR2356048A1 (en) |
GB (1) | GB1585163A (en) |
IN (1) | IN150877B (en) |
IT (1) | IT1083363B (en) |
NL (1) | NL7706993A (en) |
SE (1) | SE432133B (en) |
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US4187135A (en) * | 1978-03-27 | 1980-02-05 | Celanese Corporation | Fiber reinforced composite shaft with metallic connector sleeves mounted by longitudinal groove interlock |
DE2951629C2 (en) * | 1979-12-21 | 1985-03-14 | Felten & Guilleaume Energietechnik GmbH, 5000 Köln | Drive shaft made of fiber-reinforced plastic, with a lost mandrel and tightly wound end pieces |
DE3032370A1 (en) * | 1980-08-28 | 1982-04-08 | Robert Bosch Gmbh, 7000 Stuttgart | CONNECTION FOR TRANSMITTING TORQUE IN TORSIONAL SOFT PIPES |
DE3230116A1 (en) * | 1982-08-13 | 1984-02-16 | Arendts, Franz Joseph, Prof., 8000 München | Connection means for driving or driven hollow shafts of fibre composite material |
DE3331789A1 (en) * | 1982-09-29 | 1984-03-29 | Dana Corp., 43697 Toledo, Ohio | METHOD FOR PRODUCING A DRIVE SHAFT |
DE3479572D1 (en) * | 1983-01-05 | 1989-10-05 | Deutsche Forsch Luft Raumfahrt | Element for joining of two bars with circular cross-section |
US4527978A (en) * | 1984-02-13 | 1985-07-09 | Dana Corporation | Driveshaft |
DE3503194C2 (en) * | 1985-01-31 | 1987-02-19 | Uni-Cardan Ag, 5200 Siegburg | Shaft connection |
JPS6227380A (en) * | 1985-07-26 | 1987-02-05 | いすゞ自動車株式会社 | Method of joining axis of ceramic structure to boss of metalstructure |
FI74249C (en) * | 1986-05-20 | 1988-01-11 | Valmet Oy | FAESTOERA FOER ATT FAESTAS VID AENDAN AV ETT CYLINDERFORMIGT STYCKE, SPECIELLT EN ARBETSCYLINDER. |
DE3740908A1 (en) * | 1987-12-03 | 1989-06-22 | Uni Cardan Ag | ARRANGEMENT WITH ADHESIVE CONNECTION BETWEEN A HUB AND A TUBE |
JPH0291212U (en) * | 1988-12-29 | 1990-07-19 | ||
JPH0449220U (en) * | 1990-08-31 | 1992-04-27 | ||
DE4321986C2 (en) * | 1993-07-01 | 1999-02-18 | Zf Hurth Bahntechnik Gmbh | Tooth coupling, especially for a drive unit of a rail vehicle |
SE503705C2 (en) * | 1994-10-25 | 1996-08-05 | Volvo Ab | Load-bearing structure for use in a vehicle body |
GB9625065D0 (en) * | 1996-12-02 | 1997-01-22 | Mono Pumps Ltd | Flexible drive shaft and drive shaft and rotor assembly |
US6379254B1 (en) * | 1997-06-20 | 2002-04-30 | Spicer Driveshaft, Inc. | End fitting adapted to be secured to driveshaft tube by electromagnetic pulse welding |
DE19818632C2 (en) | 1998-04-25 | 2003-05-28 | Veka Ag | Device for a corner connection of hollow plastic profiles |
DE19930444C5 (en) * | 1999-07-02 | 2005-10-20 | Daimler Chrysler Ag | Stabilizer arrangement for a motor vehicle |
EP1213526A1 (en) * | 2000-12-06 | 2002-06-12 | Techspace Aero S.A. | Method and means for assembling a composite tube and a metallic end-fitting |
DE102004001386B3 (en) * | 2004-01-09 | 2005-07-21 | Universität Kassel | Method for creating a plug connection by means of adhesive injection, as well as a male member and a hollow joining member therefor |
DE102004025312B4 (en) * | 2004-05-19 | 2010-04-22 | Braun Gmbh | module |
BE1016715A3 (en) * | 2005-08-01 | 2007-05-08 | Technical Airborne Components | Aircraft rod, has central tube made of reinforced fibers that are impregnated with hard synthetic resin and has density that is lower than that of metallic material forming two nozzles |
US8157469B2 (en) | 2006-11-22 | 2012-04-17 | The Boeing Company | Composite structural member and method for producing the same |
DE102009029657A1 (en) * | 2009-09-22 | 2011-03-24 | Deere & Company, Moline | Node element for a vehicle frame structure |
US9028164B2 (en) | 2012-03-08 | 2015-05-12 | Dana Automotive Systems Group, Llc | Magnetic pulse formed vehicle driveshaft and method of making same |
DE102012013843A1 (en) * | 2012-07-15 | 2014-01-16 | Thomas Heine | Borehole i.e. channel, for e.g. material-fit connection of pipes with bolts, is introduced from outer surface of components or semi-finished products to joint point/joint surface and serves to conduct auxiliary material on joint point |
DE102013213966B3 (en) * | 2013-07-17 | 2014-06-18 | Bayerische Motoren Werke Aktiengesellschaft | Torque transmission device and vehicle with a propeller shaft |
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JP6675325B2 (en) * | 2014-05-16 | 2020-04-01 | ダイバージェント テクノロジーズ, インコーポレイテッドDivergent Technologies, Inc. | Modularly formed nodes for vehicle chassis and methods of using them |
ES2684624B8 (en) * | 2017-03-29 | 2019-10-16 | Zenit Polimeros Y Composites Sl | System and procedure of union between elements of cylindrical type by means of adhesive |
EP3615822B1 (en) * | 2017-04-25 | 2021-06-02 | GKN Driveline Deutschland GmbH | Shaft connection and input shaft having a shaft connection of this kind |
WO2021076603A1 (en) * | 2019-10-15 | 2021-04-22 | Composite Drivelines, LLC | Composite vehicle driveshaft assembly with bondable end components |
CN114829183A (en) * | 2019-10-15 | 2022-07-29 | 复合材料传动系统有限责任公司 | Composite vehicle driveshaft assembly with integrated end yoke and method of producing the same |
EP4032755A1 (en) * | 2021-01-26 | 2022-07-27 | Volvo Construction Equipment AB | Support structure for a vehicle and method for assembling parts of a support structure for a vehicle |
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US2707694A (en) * | 1950-10-19 | 1955-05-03 | Standring Joseph Robert | Method of adhesively joining metal, wood and plastic parts |
DE1904823U (en) * | 1963-06-12 | 1964-11-19 | Ford Werke Ag | CARDAN SHAFT MADE OF SEVERAL PARTS. |
GB1330313A (en) * | 1970-09-23 | 1973-09-19 | British Aircraft Corp Ltd | Composite structures |
GB1356393A (en) * | 1970-10-06 | 1974-06-12 | British Aircraft Corp Ltd | Composite structures |
US3881973A (en) * | 1970-10-07 | 1975-05-06 | Boeing Co | Joint construction and method of fabrication |
FR2142171A5 (en) * | 1971-06-15 | 1973-01-26 | Vallourec | |
FR2254238A5 (en) * | 1973-12-07 | 1975-07-04 | Masson Claude | Assembly system for tubular motorbike frames - has tapering ends of tubes and junction piece clamped or glued together |
FR2313593A1 (en) * | 1975-06-05 | 1976-12-31 | Pitner Alfred | Vehicle steering system shaft assembly - has plastics retainers received in groove in enlarged dia. male element end |
US4041599A (en) * | 1976-04-14 | 1977-08-16 | Union Carbide Corporation | Method of concentric bonding of a rod in a tubular shaft |
-
1976
- 1976-06-24 GB GB26244/76A patent/GB1585163A/en not_active Expired
-
1977
- 1977-06-20 SE SE7707130A patent/SE432133B/en not_active IP Right Cessation
- 1977-06-20 IN IN922/CAL/77A patent/IN150877B/en unknown
- 1977-06-22 ES ES459998A patent/ES459998A1/en not_active Expired
- 1977-06-23 DE DE2728306A patent/DE2728306C2/en not_active Expired
- 1977-06-23 IT IT68464/77A patent/IT1083363B/en active
- 1977-06-23 CA CA281,251A patent/CA1068501A/en not_active Expired
- 1977-06-23 NL NL7706993A patent/NL7706993A/en not_active Application Discontinuation
- 1977-06-23 FR FR7719276A patent/FR2356048A1/en active Granted
- 1977-06-24 JP JP7539477A patent/JPS53361A/en active Granted
-
1978
- 1978-06-16 ES ES470893A patent/ES470893A1/en not_active Expired
-
1979
- 1979-05-16 CA CA327,743A patent/CA1083371A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
GB1585163A (en) | 1981-02-25 |
IN150877B (en) | 1983-01-08 |
NL7706993A (en) | 1977-12-28 |
JPS6154965B2 (en) | 1986-11-26 |
IT1083363B (en) | 1985-05-21 |
DE2728306C2 (en) | 1987-03-12 |
JPS53361A (en) | 1978-01-05 |
SE432133B (en) | 1984-03-19 |
FR2356048B1 (en) | 1983-12-02 |
CA1068501A (en) | 1979-12-25 |
ES470893A1 (en) | 1979-02-01 |
FR2356048A1 (en) | 1978-01-20 |
DE2728306A1 (en) | 1978-01-05 |
ES459998A1 (en) | 1978-09-01 |
SE7707130L (en) | 1978-02-10 |
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Legal Events
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MKEX | Expiry |