GB2215009A - Composite tubular structure - Google Patents
Composite tubular structure Download PDFInfo
- Publication number
- GB2215009A GB2215009A GB8803362A GB8803362A GB2215009A GB 2215009 A GB2215009 A GB 2215009A GB 8803362 A GB8803362 A GB 8803362A GB 8803362 A GB8803362 A GB 8803362A GB 2215009 A GB2215009 A GB 2215009A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sleeve
- tubular member
- ribs
- slots
- tubular
- 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 description 26
- 229920005989 resin Polymers 0.000 claims description 24
- 239000011347 resin Substances 0.000 claims description 24
- 210000002105 tongue Anatomy 0.000 claims description 19
- 239000000835 fiber Substances 0.000 claims description 16
- 238000004804 winding Methods 0.000 claims description 15
- 239000002657 fibrous material Substances 0.000 claims description 9
- 229910052751 metal Inorganic materials 0.000 claims description 8
- 239000002184 metal Substances 0.000 claims description 8
- 230000001154 acute effect Effects 0.000 claims description 7
- 229920001187 thermosetting polymer Polymers 0.000 claims description 7
- 238000004519 manufacturing process Methods 0.000 claims description 3
- 238000000034 method Methods 0.000 claims 6
- 101150106671 COMT gene Proteins 0.000 claims 1
- 238000004026 adhesive bonding Methods 0.000 claims 1
- 230000004323 axial length Effects 0.000 claims 1
- MYWUZJCMWCOHBA-VIFPVBQESA-N methamphetamine Chemical compound CN[C@@H](C)CC1=CC=CC=C1 MYWUZJCMWCOHBA-VIFPVBQESA-N 0.000 claims 1
- 230000000630 rising effect Effects 0.000 claims 1
- 229910000831 Steel Inorganic materials 0.000 description 10
- 239000010959 steel Substances 0.000 description 10
- 239000000853 adhesive Substances 0.000 description 5
- 230000001070 adhesive effect Effects 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 230000007797 corrosion Effects 0.000 description 1
- 238000005260 corrosion Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000008030 elimination Effects 0.000 description 1
- 238000003379 elimination reaction Methods 0.000 description 1
- 239000003822 epoxy resin Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 229920000647 polyepoxide Polymers 0.000 description 1
- 229920001225 polyester resin Polymers 0.000 description 1
- 239000004645 polyester resin Substances 0.000 description 1
- 239000013585 weight reducing agent Substances 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
-
- 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)
- Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
Description
t 1 1 .4 -1 2 2 it 51 u -! ' ' 9
COMPOSITE TUBULAR STRUCTURE Background of the Invention
Traditionally, vehicle drive shafts have been formed of a steel tube having a high flexural modulus with a forged yoke welded to each end of the steel tube. With both the tube and the yokes formed of steel the drive shaft is a relatively heavy structure.
At certain rotational speeds, a drive shaft can become dynamically unstable. The critical speed at which the instability occurs is generally proportional to the flexural modulus of the shaft and its moment of inertia and generally inversely proportional to the weight of the shaft and its length. To maintain an acceptably high critical speed with a tubular steel drive shaft, the drive shaft in many instances is formed of short multiple sections and shaft support bearings are utilized along the'length of the drive shaft which act to rotationally support the shaft sections.
Recently there has been considerable activity in the development of composite drive shafts which are composed of a fiber reinforced resin tube or shaft and light weight metal, such as aluminum, yokes. The composite'drive shaft achieves a substantial weight reduction as compared to a steel drive shaft and due to the lighter weight, a one piece composite shaft can replace the multi-section steel shafts, with the resultant elimination of the shaft support bearings which are utilized with a multi-section steel shaft.
However, a problem in the production of a composite drive shaft has been the lack of an adequate connection between the fiber reinforced resin tubular member and the yokes. In one approach to providing an adequate connection between the tube or shaft and the yokes, the ends of the tube. which surround the sleeve 1 portion of the yoke, are connected to the sleeve portion by rivets. In another approach, as shown in United States Patent 4,279,275, the sleeve portion of the yoke is provided with a plurality of longitudinally extending grooves and the resin impregnated fibrous material, when producing the tubular member, is wound circumferentially over the grooves to provide an improved mechanical connection between the tube and the yokes.
In the United States Patent 4,358,284 the sleeve portion of the yoke is provided with circumferential extending grooves or threads and the fibrous material is wound in the grooves to provide an improved attachment, while in United States Patent 4,380,443 a plurality of angularly extending pins are employed to interconnect the wound tube with the sleeve portion of the yoke.
United States Patent 4,248,062 proposes to increase the bond between the wound tube and the sleeve portion of the yoke by employing a specific winding pattern including longitudinal helical and circumferential windings.
Summary of the Invention
The invention is directed to a composite tubular structure, such as a drive shaft having an improved attachment between the fiber reinforced resin tubular member or shaft and the metal yokes. In accordance with the invention, the sleeve portion of each yoke is provided with a plurality of longitudinally extending raised ribs or bosses which are received in slots formed in the respective ends of the fiber reinforced resin tubular member. windings of a fibrous material impregnated with the thermosetting resin can be applied over the joint between the yokes and the tubular member. With this construction the 1 torsional load is transmitted through the ribs and slots rather than through an adhesive bonded interface between the tubular member and the yokes.
In a modified form of the invention, the portion of the yoke sleeve extending between the bases of adjacent ribs is formed with a groove that extends at acute angle to the axis of the yoke. The end portions of the tubular member located between adjacent slots define flexible tongues, and the end of each tongue is bent inwardly and received within one of the grooves in the sleeve portion of the yoke. An adhesive bond is employed to secure the tips of the tongues within the grooves, as well as to bond the contiguous portions of the tubular member to the sleeve of the yoke.
The invention provides an improved mechanical connection between the fiber reinforced resin tubular member or shaft and the yokes in which the torsional load is transmitted through the ribs and slots.- The composite drive shaft of the invention has a substantially reduced weight over a conventional steel drive shaft and reduces operational noise and vibration.
The composite drive shaft of the invention can be used for relatively long drive shafts and eliminates the need for shaft support bearings which are required in multi-section steel drive shafts. Due to the lesser weight, the drive shaft produces less stress on the supporting bearings.
By use of the fiber reinforced resin tubular member along with forged aluminum yokes, the drive shaft is corrosion resistant.
Other objects and advantages will appear in the course of the following description.
-1 1 Description of the Drawings
The drawings illustrate the best mode presently contemplated of carrying out the invention.
In the drawings:
Fig. 1 is a side elevation ofa composite drive shaft In accordance with one example of the Invention with parts broken away in section, Fig. 2 is an exploded perspective view showing an end of the fiber reinforced resin tubular member and the yoke; Fig. 3 is an exploded perspective view of a modified form of shaft showing the ends of the tubular member and the yoke; Fig. 4 is a longitudinal section of the connected members as illustrated in Fig. 3; and Fig. 5 is a transverse section taken along line 5-5 of Fig. 4.
Description of the Illustrated Em bodiment
Fig. 1 illustrates a composite drive shaft composed of a fiber reinforced resin shaft or tubular member 1 and a pair of metal yokes 2, formed of aluminum or the like, each of which is connected to an end of the tubular member 1.
Tubular member 1 is formed of a fibrous material such as glass fibers, or a combination of glass and graphite fibers, which are wound in a pattern to provide the desired mechanical properties in the tubular member. A combination of different winding patterns can be used, such as substantially circumferential windings, helical windings and substantially longitudinal windings. The particular winding pattern and fibrous material employed in forming tubular member 1 is conventional and in itself forms no part of the invention.
f -1; - 1 41 k_ The fibrous material in tubular member 1 is bonded together by a cured thermosetting resin, such as an epoxy or polyester resin.
As best illustrated in Fig. 2, each yoke 2 is provided with a generally cylindrical sleeve portion 3 and a plurality of longitudinal raised ribs or bosses 4 are formed on the outer surface of the sleeve 3. As shown, four ribs 4 are utilized, but depending upon the particular application, one or more such ribs can be employed. Each rib is provided with a generally curved or rounded outer end 5 as shown in Fig. 2.
As shown in Fig. 2, the ends of the tubular member 1 are provided with longitudinal slots 6 which receive the ribs 4 on yoke 2. Each slot 6 is bordered by a pair of generally parallel walls 7 and a generally curved or rounded base 8 which engages the rounded end 5 of the respective rib 4. When tubular member 1 is applied over the sleeve 3, the ends 5 of ribs 4 bottom out against the bases 8 of slots 6 so that the end of the tubular member 1 is spaced out of contact with the shoulder 9 on the outer surface of yoke 2.
As an alternate construction, the ribs 4 can be formed on the inner surfce of the sleeve 3, and the sleeve inserted over the tubular member 1, so that the ribs are received in slots 6.
The contiguous surfaces of tubular member 1 and yokes 2 are bonded together, preferably by a thermosetting resin or an adhesive system.
To provide additional attachment between tubular member 1 and each yoke 2, a fibrous material impregnated with a thermosetting resin can be wound around the outer surface of tubular member 1 and yoke 2 and across the joint therebetween, as indicated by 10. The outer surfaces of ribs 4 are substantialIv 1-lush with the outer surface of the tubular membe- 1 so that the resulting windings 10 will have a smooth outer surface or contour. Alternately, a metal clamping band can be clamped over the joint in place of the fibrous windings 11.
Each yoke 2 is provided with an axial bore which is normally enclosed by a plug 11. During the application of the windings 10, the composite structure, including tubular member 1 and yokes 2, can be supported by a central shaft that extends through the axial openings in yokes 2. The shaft serves to properly align the two yokes 2 and tubular member 1 during winding of the layer 10. After the windings have been applied, the shaft is removed from the composite structure and the axial bores are closed by the plugs 11.
1-5 illustrate a modified form of the Figs. invention in which the composite drive shaft includes a fiber reinforced resin shaft or tubular member 12 and a pair of metal yokes 13. The cylindrical sleeve portion 14 of each yoke 13 is formed with a plurality of longitudinally extending raised ribs or bosses 15. As illustrated in Fig. 5, sleeve portion 14 includes six ribs 15 but it is contemplated that any number of ribs can be utilized.
Each rib 15 is bordered by a pair of angularly extending sides 16 which are connected together by a generally square end 17. As best illustrated in Fig. 4, the portions of sleeve 14 extending between the bases of adjacent ribs 15 are formed with grooves 18 which extend at an acute angle of about 10 to 200 with respect to the axis of sleeve 14.
As best shown in Fig. 3 each end of tubular member 12 is provided with a plurality of tongues 19 which border slots 20. Tongues 19 taper or converge inwardly, as illustrated in Fig. 3, and are received in the spaces between ribs 15 on sleeve 14. The tongues r, A 19 are relatively flexible and the tips 21 of the tongues are bent or deformed inwardly and are received within the angular grooves 18 in sleeve 14. In this construction, the bases of slots 20 bottom out against the ends 17 of ribs 15 and the contiguous surfaces of the tubular member 12 and sleeve 14 are bonded together by an adhesive such as a thermosetting resin. Bonding of the bent ends 21 of tongues 19 within grooves 18 serves to enhance the connection between the tubular member 12 and yokes 13..
As in the case of the first embodiment, windings 22 of a fibrous material impregnated with a thermosetting resin can be applied over the outer surface of the tubular member 12 and yokes 13 to bridge the joint between the members.
The invention provides an improved mechanical interlock between the fiber reinforced resin tubular member or shaft and the metal yokes in which the torsional load is transmitted between the ribs and slots rather than through an adhesive bonded interfacE between the members.
The composite drive shaft has a substantially reduced weight over a conventional steel drive shaft and provides reduced operational noise in service.
While the above description has illustrated the invention as applied to a composite drive shaft, it is contemplated that the composite tubular member can be used in other load transmitting applications.
Ar.Q k -8
Claims (17)
- CLAIMS - 1. A composite tubular structure, comprising a fiber reinforcedresin tubular member, a yoke secured to an end of the tubular member and including a sleeve disposed in lapping relation with an end of said tubular member, a plurality of longitudinal circumferentially spaced ribs on said sleeve, said ribs projecting radially outward from said sleeve, said end of said tubular member having a plurality of longitudinal circumferentially spaced slots to receive-the corresponding ribs and having a tongue disposed between each pair of adjacent slots, said slots opening at said end of the tubular member and extending connletely through the wall of said tubular member, said tongues being in contiguous overlapping relation with said sleeve, and clamping rneans disposed on the outer surface of said tubular member and snid sleeve extending across the joint therebetween.
- 2. The structure of claim 1, wherein said ribs have a shorter axial length than said sleeve to provide a sleeve portion extending between the inner end of each rib and the inner end of said sleeve, said -ion tubular nenber being in contiguous overlapping rela, with said sleeve portions.
- 3. A composite tubular structure, comprising a fiber reinforced resin tubular nenber (1) having a uniform internal diameter, a voke (2) secured to an end of the tubular nenber and including a sleeve (3) disposed in lapping relation with an end of said tubular member, a plurality of longitudinal circumferentially spaced ribs (4) on said sleeve, said ribs nrojecting radially outward from said sleeve, said end of- said tubular member havinc a plurality of longitudinal circu-nferentially snaced slots (6) to receive the corresnonding, ribs and having a tonnue rlisposed between each pair of adjacent slots, said slots opening at said t end of the tubular member and extending completely through the wall of said tubular member, said ribs (4) having a radial depth substantially equal to the thickness of said tubular member (1), said tongues being in contiguous overlapping relation with said sleeve, bonding means-for adhesively bonding said end of the tubular member to said sleeve, and clampinq means (10) disposed on the outer Eurface of said tubular member and said sleeve and extendiing across the joint therebetween.
- 4. The structure of claim 3, wherein said sleeve is formed with a recess between adjacent pair of ribs, said recess extending at an acute angle to the axis of said sleeve, the outer end of each tongue being bent inwardly at an acute angle to the axis of the tubular member and d'isposed within a corresponding recess in the sleeve, said adhesive bonding means serving to bond the outer ends of said tongues within said recesses.
- 5. The structure of claim 3, wherein each slot is provided with a generall-y rounded base and each rib is formed with a rounded end to mate with said base.
- 6. The structure of claim 3, wherein each rib is bordered by a pair of generally narallel sides and each rib has a rounded outer end, each slot having a rounded base disposed in engagement with said rounded end of the corresoonding rib.
- 7. A composite tubular structure, comT)rising a fiber reinforced resin tubular member, a yoke secured to an end of the tubular member and including a sleeve disnosed in lanping relation with an end of said tubular member, a plurality of longitudinal circur-,ferentially spaced ribs on said sleeve, said ribs projecting radially outward from said sleeve, said end 4, k of said tubular member having a plurality of longitudinal circumferentially spaced slots to receive the corresponding ribs and having a tongue disposed between each pair of adjacent slots, said slots opening at said end of the tubular member and extending completely through the wall of said tubular member, said sleeve having a recess between each adjacent pair of ribs, each recess extending at an acute angle to the axis of said sleeve, said tongues being in contiguous overlapping relation with said sleeve and the outer end of each tongue being bent inwardly at an acute angle to the axis of said sleeve and disposed within a corresponding recess in said sleeve, and clamping means disposed on the outer surface of said tubular member and said sleeve and extending across the joint therebetween.
- 8. A meth ' od of forming a composite tubular structure, comprising the stens of forming a metal yoke with a generally cylindrical sleeve, forming a fiber reinforced resin tubular member, forming a plurality of longitudinal circumferentially spaced ribs on the outer surface of said sleeve, said ribs projecting radially outward from said sleeve, forniiig a plurality of slots in an end of said tubular member with said slots extending completely through the wall of said tubular member and said slots opening at said end of the tubular nember with a tongue disposed between each pair of adiacent slots, moving the sleeve and the tubular menber longitudinally of each other to bring the ribs into registry with the slots and to bring the tonques into contiguous overlapping relation with said sleeve, and aDnlying a clamping force to the overlapping portions of the sle-ve and the tubular member.
- 9. The method of claim 8, and includina the sten of bondinn the overlapping portions of said sleeve and said tonaues.IV 0 f t- - 1 1 -
- 10. The method of claim 8, wherein the step of applying a clamping force comprises winding a fibrous material impregnated with an uncured thermosetting resin around the overlapping portions of said sleeve and said tubular member and curing the resin.
- 11. The method of claim 8, wherein the step of forming said slots includes forming each slot with a generally rounded base and forming each rib with a rounded end to mate with said base.
- 12. The method of claim 8, wherein said ribs are formed with a depth substantially equal to the thickness of said tubular member.
- 13. A method of forming a composite tubular structure, comprising the steps of forming a metal yoke with a generally cylindrical sleeve, forming a fiber reinforced resin tubular member, forming a plurality of longitudinal circumferentially spaced ribs on the outer surface of said sleeve with the ribs projecting radially outward of said sleeve, forming a plurality of slots in an end of the tubular nemher with a tongue disposed between each pair of ad.jacent slots and extending the slots to the end of the tubular member, forming a recess between each adjacent pair of ribs in said sleeve and extending each recess at an acute angle to the axis of said sleeve, moving the sleeve and tubular member longitudinally to bring the ribs into registry with the slots and to insert the ends of the tongues into said recesses, and applying a clamping force to the overlapping portions of said tubular member and said sleeve.
- 14. A composite tubular structure substantially as hereinbefore described with reference to.Figures 1 and 2 of the accompanying drawings.
- 15. A composite tubular structure substantially as hereinbefore described with reference to Figures 3, 4 and 5 of the accompanying drawings.
- 16. A method of manufacturing a composite tubular structure substantially as hereinbefore described with reference to Figures 1 and 2 of the accompanying drawings.
- 17. A method of manufacturing a composite tubular structure substantially as hereinbefore described with reference to Figures 3, 4 and 5 of the accompanying drawings.Published 1989 at The Patent Office, State House, 66.7 1 High Holborn, London WC 111 4TP. Further copiesmaybe obtainedfrom The Patent Office. Sales Branch, St Mary Cray, Orpington, Kent BR5 3RD. Printed by Multiplex techniques ltd, St Mary Cray, Kent, Con. 1187 t
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US77719185A | 1985-09-18 | 1985-09-18 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| GB8803362D0 GB8803362D0 (en) | 1988-03-16 |
| GB2215009A true GB2215009A (en) | 1989-09-13 |
| GB2215009B GB2215009B (en) | 1991-08-07 |
Family
ID=25109537
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB8803362A Expired - Lifetime GB2215009B (en) | 1985-09-18 | 1988-02-13 | Composite tubular structure |
Country Status (2)
| Country | Link |
|---|---|
| DE (1) | DE3804902A1 (en) |
| GB (1) | GB2215009B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009058583A1 (en) * | 2007-11-02 | 2009-05-07 | The Boeing Company | Joint for hybrid composite items |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102004063344A1 (en) * | 2004-12-23 | 2006-07-13 | Voith Turbo Gmbh & Co. Kg | Universal joint and universal joint arrangement |
| DE102012106120B4 (en) * | 2012-07-06 | 2014-10-16 | Xperion Gmbh | Method for producing a propeller shaft and propeller shaft |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4279275A (en) * | 1979-08-06 | 1981-07-21 | Ford Aerospace & Communications Corporation | Mechanical joinder of composite shaft to metallic end members |
| US4248062A (en) * | 1979-10-05 | 1981-02-03 | Shakespeare Company | Drive shaft assembly and method for making same |
| US4380443A (en) * | 1979-11-17 | 1983-04-19 | Felten & Guilleaume Carlswerk Aktiengesellschaft | Fiber-reinforced drive shaft |
| 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 |
| DE3007896C2 (en) * | 1980-03-01 | 1985-03-07 | Daimler-Benz Ag, 7000 Stuttgart | Connection connection for hollow shafts formed by fiber plastic pipes, in particular for motor vehicles |
| DE3032370A1 (en) * | 1980-08-28 | 1982-04-08 | Robert Bosch Gmbh, 7000 Stuttgart | CONNECTION FOR TRANSMITTING TORQUE IN TORSIONAL SOFT PIPES |
| DE3421191A1 (en) * | 1984-06-07 | 1985-12-12 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Hollow shaft made of plastic with a permanently connected flange made of metal |
| DD227203A1 (en) * | 1984-08-06 | 1985-09-11 | Ifa Gelenkwellenwerk Haldensle | DRIVE SHAFT OF FIBER-REINFORCED PLASTIC |
-
1988
- 1988-02-13 GB GB8803362A patent/GB2215009B/en not_active Expired - Lifetime
- 1988-02-17 DE DE3804902A patent/DE3804902A1/en not_active Ceased
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2009058583A1 (en) * | 2007-11-02 | 2009-05-07 | The Boeing Company | Joint for hybrid composite items |
| US8161619B2 (en) | 2007-11-02 | 2012-04-24 | The Boeing Company | Joint for hybrid composite items |
| US8430759B2 (en) | 2007-11-02 | 2013-04-30 | The Boeing Company | Joint for composite tube |
Also Published As
| Publication number | Publication date |
|---|---|
| GB8803362D0 (en) | 1988-03-16 |
| GB2215009B (en) | 1991-08-07 |
| DE3804902A1 (en) | 1989-08-31 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 732E | Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977) | ||
| PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 20000213 |