GB2051304A - Fibre-reinforced composite shaft with metallic connector sleeves - Google Patents
Fibre-reinforced composite shaft with metallic connector sleeves Download PDFInfo
- Publication number
- GB2051304A GB2051304A GB8017398A GB8017398A GB2051304A GB 2051304 A GB2051304 A GB 2051304A GB 8017398 A GB8017398 A GB 8017398A GB 8017398 A GB8017398 A GB 8017398A GB 2051304 A GB2051304 A GB 2051304A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- sleeve
- pins
- fibers
- mandrel
- 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.)
- Granted
Links
- 239000002131 composite material Substances 0.000 title claims abstract description 10
- 239000000835 fiber Substances 0.000 claims abstract description 29
- 229910052751 metal Inorganic materials 0.000 claims abstract description 16
- 239000002184 metal Substances 0.000 claims abstract description 16
- 239000012260 resinous material Substances 0.000 claims abstract description 15
- 239000002657 fibrous material Substances 0.000 claims abstract description 5
- 238000000034 method Methods 0.000 claims description 12
- 239000003733 fiber-reinforced composite Substances 0.000 claims description 10
- 239000010410 layer Substances 0.000 description 24
- 229920005989 resin Polymers 0.000 description 14
- 239000011347 resin Substances 0.000 description 14
- 239000003365 glass fiber Substances 0.000 description 8
- 229920000049 Carbon (fiber) Polymers 0.000 description 7
- 239000004917 carbon fiber Substances 0.000 description 7
- 238000004804 winding Methods 0.000 description 6
- 230000002787 reinforcement Effects 0.000 description 5
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 3
- 230000001070 adhesive effect Effects 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 3
- 229920001187 thermosetting polymer Polymers 0.000 description 3
- 229910052799 carbon Inorganic materials 0.000 description 2
- 239000011521 glass Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000011159 matrix material Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- 239000004593 Epoxy Substances 0.000 description 1
- 244000187656 Eucalyptus cornuta Species 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 238000007792 addition Methods 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 238000004873 anchoring Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000012217 deletion Methods 0.000 description 1
- 230000037430 deletion Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 210000003746 feather Anatomy 0.000 description 1
- 238000009730 filament winding Methods 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 238000011068 loading method Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 239000012783 reinforcing fiber Substances 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 239000002356 single layer Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 239000004634 thermosetting polymer Substances 0.000 description 1
- 238000009785 tube rolling Methods 0.000 description 1
- 238000004046 wet winding Methods 0.000 description 1
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
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
- B29C70/86—Incorporated in coherent impregnated reinforcing layers, e.g. by winding
-
- 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)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
A tubular fibre reinforced composite shaft integrally incorporates a metal sleeve 14 or connection at the end. Initially a metal sleeve having radially outwardly projecting pointed pins 26 is positioned upon a segment of a mandrel. Fibrous material bearing a non-solidified resinous material is applied around the mandrel and around the pins of the sleeve. The resinous material next is solidified to form a tubular composite shaft whereby a secure torsion-transmitting connection is made with the sleeve, and the mandrel is removed. <IMAGE>
Description
SPECIFICATION
Fiber reinforced composite shaft with metallic connector sleeves mounted by mechanical interlock
This invention relates to fiber reinforced composite shafts and, more especially, to vehicle drive shafts comprising a fiber reinforced resinous shaft body with metallic coupling sleeves mounted at the ends thereof.
Tubular fiber reinforced composites have been heretofore proposed, as demonstrated by U.S.
Patent Nos. 2,882,072 issued to Noland on April 14, 1959, and 3,661,670 issued to Pierpont on
May 9, 1972, and in British patent No. 1,356,393 issued on June 12, 1 974. In the Pierpont patent, for example, it has been proposed to form such composites from a resinous material which is reinforced by glass fibers. In particular, filaments bearing a non-hardened resinous material (i.e., an uncured thermosetting resin) are wound around a mandrel until the desired thickness has been established. The reinforcing fibers can be positioned within the wall of the tubular composite in varying angular relationships.
Thereafter, the resinous material is solidified (i.e. is cured). A premolded threaded end portion can be mounted at the ends of the tubular composite, such as by the winding of filaments directly around the end portion during the winding process.
It recently has been proposed to form vehicle drive shafts from tubular fiber reinforced composites, as demonstrated by U.S. Patent No.
4,041,599 issued to Smith on August 1 6, 1977, and published Japanese Application No.
52-127542, entitled "Carbon Fiber Drive Shaft" which claims priority for the filing of U.S. Serial No. 676,856 on April 14, 1976 of Gordon Peter
Worgan et al (now United States Patent No.
4,089,190). In the Japanese application filaments bearing a non-hardened resinous material (e.g., an uncured thermosetting resin) are wound around a mandrel until the desired thickness has been established, whereupon the resinous material is cured. Zones or layers are positioned circumferentially within the wall of the shaft in the specific angular relationships there disclosed.
The above-mentioned Smith patent proposes the attachment of a carbon fiber reinforced epoxy drive shaft directly to a universal joint extension by a specific bonding technique.
Fiber reinforced composite shafts exhibit advantages over metallic shafts, i.e., they are lighter in weight, more resistant to corrosion, stronger, and more inert.
In copending application Serial No. 890,232 filed March 27, 1 978 of Derek N. Yates and David
B. Rezin entitled "Improved Carbon Fiber
Reinforced Composite Drive Shaft", a fiber reinforced composite drive shaft is disclosed which exhibits improved service characteristics and the necessary strength and durability to withstand the various stresses encountered during vehicle operation. The disclosure of that copending application is herein incorporated by reference as if set forth at length.
Since direct welding or bonding of a resin shaft to metal does not normally create a sufficiently strong and durable connection on a consistent and reliable basis, the use of metallic connector sleeves mounted at the ends of the shaft in accordance with the concept of the present invention provides a means for accomplishing a secure welded connection similar to that utilized with conventional metallic shafts.
The high torque loads which are to be transmitted by a vehicle drive shaft require that an extremely strong and durable torsional drive connection be established between the sleeves and shaft body. Previous proposals for mounting sleeves by employing adhesives or by wrapping the filament bundles around circumferential grooves on the sleeve periphery, cannot be relied upon to provide a connection of the requisite strength and durability.
It is, therefore, an object of the present invention to provide a novel, fiber reinforced resin shaft which minimizes or obviates problems of the types discussed above.
It is an additional object of the invention to provide a novel, fiber reinforced resin shaft suitable for use as a drive shaft in a vehicle power train.
It is a further object of the invention to provide novel methods and apparatus for securing metal connector sleeves to the ends of fiber reinforced resin shafts to enable the shafts to transmit high torsional loads.
BRIEF SUMMARY OF A PREFERRED
EMBODIMENT OF THE INVENTION
The objects of the present invention are achieved by a tubular fiber reinforced composite shaft, and a method for making same, wherein the shaft body comprises a plurality of integrally bonded circumferential plies of solidified fiber reinforced resinous material. A metal sleeve is mounted in at least one end of the shaft body. A plurality of substantially pointed pins project radially outwardly from the sleeve. The pins are encompassed by fiber reinforced resinous material to form a torsion-transmitting connection between the shaft body and the sleeve. The shaft is formed by anchoring the pins in the sleeve, positioning the sleeve on a segment of a mandrel, and applying the fibrous material around the mandrel and sleeves so as to encompass the pins. Thereafter, the resinous material is solidified and the mandrel is removed.
THE DRAWING
Other objects and advantages of the present invention will become apparent from the subsequent detailed description of a preferred embodiment thereof in connection with the accompanying drawings in which like numerals designate like elements and in which:
Figure 1 is a longitudinal sectional view of a drive shaft formed in accordance with the present invention;
Figure 2 is a cross-sectional view of the drive shaft taken along line 2-2 of Figure 1; and
Figure 3 is a fragmentary longitudinal sectional view of a sleeve portion of the drive shaft mounted on a mandrel.
DETAILED DESCRIPTION OF THE PREFERRED
EMBODIMENT OF THE INVENTION
A drive shaft 10 according to the present invention comprises a reinforced resin shaft body 12 of cylindrical cross-section, and a metal connector sleeve 14 secured preferably at each end of the shaft body.
The connector sleeve 14 is generally cylindrical and formed of an appropriate metal, such as steel or aluminum for example. The sleeve includes an inner annular surface 1 6 of constant diameter which is substantially contiguous with an inner surface 18 of the shaft body located longitudinally inwardly thereof, as is evident from Figure 1.
The inner end 20 of the sleeve 14 is tapered in a direction extending longitudinally and radially inwardly (Fig. 3) to provide a feather edge 24 for the reception of windings of reinforced resin material as will be discussed.
The sleeve 14 includes a plurality of radially outwardly projecting pins 26. The pins 26 are integral with the cylindrical body of the sleeve and thus are formed of the same metal. Formation of the sleeve and pins can be effected by any suitable technique, such as by stamping, machinery or welding for example.
The pins are preferably arranged in longitudinally extending, circumferentially spaced rows although any suitable arrangement could be employed. Each pin tapers in a radially outward direction and is substantially pointed at its outer tip. The pins are not sharply pointed, but rather are slightly radiused, so as to be blunt and thereby prevent cutting of the fibers during winding. Thus, the tips of the pins are small enough to prevent a fiber from being hung-up thereon. Rather, as fibers forming the body 12 are wound around the sleeve, fibers contacting the pins 26 are displaced to one side thereof and slide radially inwardly along the side of the pin until contacting the surface of the sleeve or previously wound fibers. This assures that the fibers are tightly wound, without becoming hung-up on the pins themselves, as might occur in the case of pins having flat outer surfaces.
During fabrication of a preferred form of the shaft, a pair of connector sleeves 14 is positioned on segments of a cylindrical mandrel 41 in a longitudinally spaced relationship (Fig. 3), as discussed in copending applications Serial Nos.
890,230 and 890,231 of Derek N. Yates and John
C. Presta, both filed March 27, 1978 and assigned to the assignee of the present invention. Those copending applications are incorporated herein by reference as if set forth at length. The sleeves engage the mandrel somewhat snugly, but loosely enough to be removable therefrom. An appropriate clamping arrangement holds the sleeves 14 in place. The mandrel is coated with a release substance to resist the adherence thereto of resin or adhesives. Thereafter, the shaft body 12 is formed around both the mandrel and sleeves.
Construction of the shaft body 12 is preferably performed in a manner more fully described in the aforementioned application of Yates and Rezin.
Summarized briefly, layers of fiber reinforced resin-impregnated material are applied preferably in the form of bundles of substantially parallel continuous filaments bearing a non-solidified (i.e., liquid, soft and tacky, or molten) resinous material.
The bundles can be dipped in an uncured liquid thermosetting resin, such as an epoxy resin, oi.d then wound around the mandrel in multiple passes until a layer of desired thickness is established.
Attention is further directed to U.S. Patent Nos.
3,661,670, 3,202,560, and 3,231,442 for additional details concerning possible arrangements for the clamping of sleeves and winding of filament bundles. The disclosures of these patents are incorporated herein by reference as if set forth at length.
The term "layer" as used herein specifies a circumferential zone within the wall of the tubular drive shaft wherein the fibrous reinforcement is disposed in a specific configuration and differs from the adjacent zone(s) with respect to the configuration and/or composition of the fibrous reinforcement. A single layer may include a multiple pass alignment or buildup of fibrous reinforcement in a given configuration. The term layer encompasses an alignment wherein the fibrous reinforcement is disposed therein at both plus and minus a given angle which optionally can be built-up in multiple passes.
The fibers reinforce the thermoset resin matrix to impart necessary properties of strength and durability to the shaft. In this regard, glass fibers (e.g., E-glass or S-glass) and carbon fibers (i.e., either amorphous or graphitic) materials are preferred. The carbon fibers commonly contain at least 90 percent carbon by weight, and preferably at least 95 percent carbon by weight. Additionally preferred carbon fibers have a Young's modulus of elasticity of at least 25 million p.s.i. (e,g., approximately 30 to 60 million p.s.i.).
The piles of filament bundles are wound in various orientation relative to the longitudinal axis of the drive shaft, and can be built-up to different thicknesses, respectively. Preferably, an initial layer of glass fibers is applied at an angle of from +30 to +50 relative to a line parallel to the longitudinal axis of the shaft. Next, a layer of glass fibers is applied at an angle of from 0 to fl 50.
Thereafter, a layer of carbon fibers is applied at an angle of from 0 to +150. Then a layer of glass fibers is applied at about an angle of from about +60 to 900.
Of course the number and composition of layers, as well as their orientation and thickness may vary, depending upon the characteristics desired to be imparted to the shaft
Rather than utilizing filament winding (e.g., wet winding or prepreg winding), other tube forming procedures can be employed, such as tube rolling, tape wrapping, or pultrusion, for example. In the former step, comparatively wide sections of resin impregnated tape are precut to patterns, stacked in sequence, and rolled onto the mandrel.
After the layers have been applied, the nonsolidified resin is cured. In this regard, the resin may be of a self-curing type, or may be of a kind which cures in response to being subjected to heat and/or curing agent.
Relating more particularly to the present invention, after the sleeve(s) 14 has been positioned on the mandrel, an initial layer 32 of glass fibers is wound around the mandrel and sleeves at about a +45 degree angle. As they are wound, the fibers contact the pins 26. Due to the tapered shape of the pins, however, the fibers slide downwardly along the sides thereof to the radially inner end of the exposed portion of the pin.
Accordingly, the fibers encompass opposite sides of the pins in such fashion that relative rotational and longitudinal movement between the fibers and sleeve is prevented.
Thereafter, a layer 40 of glass fibers is wound around the layer 32 at about a zero degree angle.
These fibers encompass the pins 26 in a fashion which further resists relative rotational movement between the sleeve and fibers.
Next, a layer 42 of graphite fibers is wound around the layer 40 at about a zero degree angle. These fibers encompass the pins to still further effect a torsion or rotation transmitting connection between the sleeve and fibers. This layer 42 substantially covers the radially outer tips of the pins 26.
Finally, a layer 44 of glass fibers is wound at about a 90 degree angle around the layer 42. This layer 44 assures that the pins 26 are completely covered.
It will be understood that any number of layers can be applied and at various angles and thicknesses, depending upon desired shaft characteristics.
Therafter, the non-solidified resin is cured to bond the layers together to form an integral composite, and the shaft is removed from the mandrel.
The shaft 10 is ideally suited for use as a vehicle drive shaft. In this connection the pins 26 serve to mechanically lock the shaft body and sleeve together and prevent relative rotational and longitudinal movement therebetween. The pins 26 exhibit a high degree of shear strength capable of withstanding the high torque loadings occurring during the transmission of drive power in a vehicle.
As illustrated in Figure 1 an axially outer portion 36 of the sleeve 14 is exposed, preferably by removing portions of the layers.
The sleeves 14 facilitate connection of the shaft to metal components such as metal yokes in a vehicle power train, since direct metal-to-metal contact is possible.
Although not necessary, it might be desirable to apply an adhesive between the sleeve 14 and the initial layer 32 of fibrous material to augment the connection therebetween.
Although the mechanical lock concept of the present invention is disclosed in conjunction with a particular shaft body, it is to be understood that this concept has utility with composite shafts in general wherein fibrous reinforcement is present in a resinous matrix material.
Although the invention has been described in connection with a preferred embodiment thereof, it will be appreciated by those skilled in the art that additions, modifications, substitutions and deletions not specifically described may be made without departing from the spirit and scope of the invention as defined in the appended claims.
Claims (11)
1. A method of forming a tubular, fiberreinforced composite shaft comprising the steps of:
providing a metal sleeve having a plurality of
substantially pointed pins extending radially
outwardly therefrom;
positioning said metal sleeve upon a segment
of a mandrel;
applying fibrous material bearing a non
solidified resinous material upon said mandrel
and sleeve and in encompassing relation
around said pins;
solidifying said resinous material to create a
torsion-transmitting connection with said metal
sleeve; and
removing said mandrel.
2. A method according to claim 1, wherein the application of said fibrous material terminates short of a longitudinally outer end of said sleeve to expose the latter.
3. A method according to claim 1 or 2, wherein said applying step comprises applying a plurality of layers of fibers, with the fibers of at least some of said layers being oriented at mutually different angles relative to the longitudinal direction of the shaft.
4. A method according to claim 1,2 or 3 wherein said applying step comprises completely covering said pins by said fibers.
5. A method according to any of claims 1 to 4 wherein the pins are conically shaped, formed integral with said sleeve, and project therefrom, in circumferentially and longitudinally spaced relationship.
6. A method of forming a tubular, fiberreinforced composite shaft substantially as hereinbefore described with reference to the accompanying drawings.
7. A tubular fiber-reinforced composite shaft comprising
a shaft body comprising a plurality of integrally
bonded circumferential plies of solidified fiber
reinforced resinous material;
a metal sleeve mounted in at least one end of
said shaft body; and
a plurality of substantially pointed metal pins
connected to and projecting outwardly from
said sleeve;
said pins encompassed by fiber-reinforced
resinous material of said shaft body to form a
torsion-transmitting connection between said
sleeve and said shaft body.
8. A shaft according to claim 7, wherein said pins are of conical configuration.
9. A shaft according to claim 7 or 8, wherein a longitudinally outer portion of said sleeve projects from said shaft body.
10. A shaft according to claim 7, 8 or 9 wherein said shaft body comprises a plurality of layers of fibers with at least some of said layers being oriented at mutually different angles relative to the longitudinal direction of the shaft.
11. A tubular reinforced composite shaft substantially as hereinbefore described with reference to the accompanying drawings.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US4355879A | 1979-05-29 | 1979-05-29 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB2051304A true GB2051304A (en) | 1981-01-14 |
| GB2051304B GB2051304B (en) | 1983-01-12 |
Family
ID=21927767
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB8017398A Expired GB2051304B (en) | 1979-05-29 | 1980-05-28 | Fibre-reinforces composite shaft with metallic connector sleeves |
Country Status (4)
| Country | Link |
|---|---|
| JP (1) | JPS55159310A (en) |
| DE (1) | DE3020024A1 (en) |
| FR (1) | FR2458000A1 (en) |
| GB (1) | GB2051304B (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0169046A3 (en) * | 1984-07-16 | 1986-10-29 | Conoco Inc. | Composite mooring element for deep water offshore structures |
| US4867824A (en) * | 1982-07-08 | 1989-09-19 | Hercules Incorporated | Manufacture of filamentary composites |
| WO1989012759A1 (en) * | 1988-06-23 | 1989-12-28 | Siemens Aktiengesellschaft | Fibre-reinforced plastic push or traction rod |
| FR2637952A1 (en) * | 1988-10-13 | 1990-04-20 | Aerospatiale | DEVICE FOR BONDING THE END OF A COMPOSITE TUBE HAVING AXIALLY SOLIDITY WITH METALLIC FLANGES AND METHOD OF MANUFACTURING THE SAME |
| US5094567A (en) * | 1986-02-05 | 1992-03-10 | Techocompositi S.P.A. | Flexible column from composite material |
| EP1798429A1 (en) * | 2005-12-15 | 2007-06-20 | SKF Aerospace France | Composite material tube rod and manufacturing method of such rod |
| WO2009003207A1 (en) * | 2007-07-03 | 2009-01-08 | Teufelberger Gesellschaft M.B.H. | Arrangement for connecting an elongate element to a further component |
| WO2017117497A1 (en) * | 2015-12-31 | 2017-07-06 | Moog Inc. | Composite torque tube end fitting attachment method |
| CN118401757A (en) * | 2022-01-07 | 2024-07-26 | 特瑞堡密封系统德国有限公司 | Lightweight composite actuator |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2496836A1 (en) * | 1980-12-23 | 1982-06-25 | Maschf Augsburg Nuernberg Ag | Lightweight strut for framework or machine - has inner and outer tubes with glass fibre reinforced layers between end caps |
| CA1212529A (en) * | 1982-07-08 | 1986-10-14 | Dee R. Gill | Manufacture of filamentary composites |
| JPH0745198B2 (en) * | 1987-10-15 | 1995-05-17 | 東燃株式会社 | Fiber-reinforced composite resin pipe and method for producing the same |
| CN118494543A (en) * | 2024-07-12 | 2024-08-16 | 株洲时代新材料科技股份有限公司 | Torsion bar shaft, lightweight anti-roll torsion bar, and metal pipe hole processing technology |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1356393A (en) * | 1970-10-06 | 1974-06-12 | British Aircraft Corp Ltd | Composite structures |
| US4138285A (en) * | 1976-05-07 | 1979-02-06 | Fiber Glass Systems, Inc. | Filament rod construction and method of forming the same |
| US4185472A (en) * | 1978-03-27 | 1980-01-29 | Celanese Corporation | Fiber reinforced composite shaft with metallic connector sleeves mounted by radial pin interlock |
-
1980
- 1980-05-22 JP JP6721080A patent/JPS55159310A/en active Pending
- 1980-05-24 DE DE19803020024 patent/DE3020024A1/en not_active Withdrawn
- 1980-05-28 GB GB8017398A patent/GB2051304B/en not_active Expired
- 1980-05-28 FR FR8011838A patent/FR2458000A1/en not_active Withdrawn
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4867824A (en) * | 1982-07-08 | 1989-09-19 | Hercules Incorporated | Manufacture of filamentary composites |
| EP0169046A3 (en) * | 1984-07-16 | 1986-10-29 | Conoco Inc. | Composite mooring element for deep water offshore structures |
| US5094567A (en) * | 1986-02-05 | 1992-03-10 | Techocompositi S.P.A. | Flexible column from composite material |
| WO1989012759A1 (en) * | 1988-06-23 | 1989-12-28 | Siemens Aktiengesellschaft | Fibre-reinforced plastic push or traction rod |
| FR2637952A1 (en) * | 1988-10-13 | 1990-04-20 | Aerospatiale | DEVICE FOR BONDING THE END OF A COMPOSITE TUBE HAVING AXIALLY SOLIDITY WITH METALLIC FLANGES AND METHOD OF MANUFACTURING THE SAME |
| US5082314A (en) * | 1988-10-13 | 1992-01-21 | Societe Nationale Industrielle Et Aerospatiale | Device for connecting the ends of a composite tube subjected to severe axial stress with metallic collars and manufacturing process therefor |
| EP0365391A1 (en) * | 1988-10-13 | 1990-04-25 | AEROSPATIALE Société Nationale Industrielle | Device for connecting the ends of a highly axially loaded compound tube by means of metallic flanges and process of manufacturing the same |
| EP1798429A1 (en) * | 2005-12-15 | 2007-06-20 | SKF Aerospace France | Composite material tube rod and manufacturing method of such rod |
| FR2895041A1 (en) * | 2005-12-15 | 2007-06-22 | Skf Aerospace France Soc Par A | TUBE ROD IN COMPOSITE MATERIAL AND METHOD FOR MANUFACTURING SUCH ROD |
| WO2009003207A1 (en) * | 2007-07-03 | 2009-01-08 | Teufelberger Gesellschaft M.B.H. | Arrangement for connecting an elongate element to a further component |
| AU2008271894B2 (en) * | 2007-07-03 | 2012-07-12 | Teufelberger Composite GES.M.B.H | Arrangement for connecting an elongate element to a further component |
| WO2017117497A1 (en) * | 2015-12-31 | 2017-07-06 | Moog Inc. | Composite torque tube end fitting attachment method |
| US10508682B2 (en) | 2015-12-31 | 2019-12-17 | Moog Inc. | Composite torque tube end fitting attachment method |
| CN118401757A (en) * | 2022-01-07 | 2024-07-26 | 特瑞堡密封系统德国有限公司 | Lightweight composite actuator |
Also Published As
| Publication number | Publication date |
|---|---|
| DE3020024A1 (en) | 1980-12-11 |
| JPS55159310A (en) | 1980-12-11 |
| FR2458000A1 (en) | 1980-12-26 |
| GB2051304B (en) | 1983-01-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4185472A (en) | Fiber reinforced composite shaft with metallic connector sleeves mounted by radial pin interlock | |
| US4236386A (en) | Fiber reinforced composite shaft with metallic connector sleeves mounted by a polygonal surface interlock | |
| US4238540A (en) | Fiber reinforced composite shaft with metallic connector sleeves mounted by connector ring interlock | |
| US4259382A (en) | Fiber reinforced composite shaft with metal connector sleeves secured by adhesive | |
| US4187135A (en) | Fiber reinforced composite shaft with metallic connector sleeves mounted by longitudinal groove interlock | |
| US4238539A (en) | Fiber reinforced composite shaft with metallic connector sleeves mounted by a knurl interlock | |
| US4265951A (en) | Fiber reinforced composite shaft with metallic connector sleeves mounted by longitudinal groove interlock | |
| GB2051303A (en) | Fibre-reinforced composite shaft with metallic connector sleeves | |
| US4421497A (en) | Fiber-reinforced drive shaft | |
| US4279275A (en) | Mechanical joinder of composite shaft to metallic end members | |
| US7731593B2 (en) | Composite transmission shaft joint | |
| US4248062A (en) | Drive shaft assembly and method for making same | |
| US5601493A (en) | Drive shaft made of fiber reinforced plastics, and method for connecting pipe made of fire-reinforced plastics | |
| US4211589A (en) | Shaft and universal joint assembly | |
| CA1130594A (en) | Power transmission shaft | |
| US4289557A (en) | Method for mass producing composite shafts | |
| US7874925B2 (en) | Transmission shaft joint design | |
| CA1120737A (en) | Composite drive shafts | |
| US4664644A (en) | Fiber reinforced plastic drive shaft and method of manufacturing thereof | |
| GB2051304A (en) | Fibre-reinforced composite shaft with metallic connector sleeves | |
| JPS6098233A (en) | Fiber reinforced plastic plate spring constitution | |
| US4854988A (en) | Process for the production of a fiber-reinforced synthetic resin container | |
| GB2406154A (en) | Composite shaft with metal sleeve | |
| JPH05106629A (en) | Load transmitting shaft made of fiber reinforced plastics | |
| JPH0742974B2 (en) | Manufacturing method of transmission shaft made of fiber reinforced plastic |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PCNP | Patent ceased through non-payment of renewal fee |