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GB2138921A - Shafts - Google Patents

Shafts Download PDF

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Publication number
GB2138921A
GB2138921A GB08310354A GB8310354A GB2138921A GB 2138921 A GB2138921 A GB 2138921A GB 08310354 A GB08310354 A GB 08310354A GB 8310354 A GB8310354 A GB 8310354A GB 2138921 A GB2138921 A GB 2138921A
Authority
GB
United Kingdom
Prior art keywords
shaft
end portions
intermediate portion
diameter
parts
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
GB08310354A
Other versions
GB8310354D0 (en
Inventor
Bertram Joseph Palmer
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BRD Co Ltd
Original Assignee
BRD Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BRD Co Ltd filed Critical BRD Co Ltd
Priority to GB08310354A priority Critical patent/GB2138921A/en
Publication of GB8310354D0 publication Critical patent/GB8310354D0/en
Publication of GB2138921A publication Critical patent/GB2138921A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C3/00Shafts; Axles; Cranks; Eccentrics
    • F16C3/02Shafts; Axles
    • F16C3/026Shafts made of fibre reinforced resin

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  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Ocean & Marine Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Shafts, Cranks, Connecting Bars, And Related Bearings (AREA)

Abstract

A shaft of a composite material, has a region 12 between the end portions 10, 11 thereof of greater diameter than the end portions. The shaft may be manufactured in two parts, secured together in its region of greater diameter. A higher bending stiffness is achieved to prevent whirling of the shaft, without increasing the space required for installation of the shaft at the ends thereof. <IMAGE>

Description

SPECIFICATION Shafts of composite material This invention relates to shafts made of composite, fibre reinforced resin, material. Ashaft made according to the invention may be used,for example, as the longitudinal drive shaft (propellor shaft) of a motor vehicle.
One problem encountered in design of shafts of composite material is that a shaft may have sufficient torque transmitting capability but not be sufficiently stiff in bending to avoid a phenomenon known as whirling. This occurs above a critical rotational speed, atwhich the shaft bends so that its central region rotates eccentrically. One way in which this problem can be overcome isforthe bending stiffness of the shaftto be increased by increasing its diameter, but in typical installations the space available at the ends of the shaft is very limited so that this expedient cannot be adopted. If the diameter ofthe shaft cannot be increased, its wall thickness must be increased which adds to its weight and cost of manufacture, or high modulus fibres such as carbon fibres can be incorporated in the shaft construction. This again adds to cost of manufacture.It is the object of the present invention to overcome or reduce these disadvantages.
According to the invention, we provide a shaft of composite material and including a portion, intermediate end portions thereof, of a diameter greater than that of said end portions.
A shaft according to the invention thus achieves, by virtue of its greater diameter in its intermediate portion, a greater bending stiffessthan if it were of the same diameteras its end portionsthroughout However, the end portions of the shaft remain of a conveniently small diameter for installation purposes.
The shaft may be of su bsta ntiallyconsta nt wal I thicknessthroughoyt its length and may taper uni- formlyfrom the intermediate portion to its end portions. Alternatively, its diameter may decrease in steps from its intermediate portion to its end portions.
Shafts of fibre reinforced resin material are normally made by winding fibres, impregnated with resin, over a mandrel. Because of the impossibility of removing a mandrel from the interiorofa one piece shaft according to the invention, the invention provides thatthe shaft may be in two parts, secured together at said intermediate portion. The two parts may be secured together, for example, by being adhesively secured to an internal or an external connecting sleeve.
Itwould, however, be possible forthe shaftto be made in one piece ifaformerwere used which remains in position in the interior of the shaft.
The invention will now be described by way of example with reference to the accompanying drawings; FIGURE 1 andFlGURE2,whicharediagramma- tic sections through embodiments of shaft according to the invention.
Referring firstly to Figure 1,there is shown a shaft comprising two end portions 10, 11 and an intermediate portion 12. The end portions 10, 11 are cylindrical, and the intermediate portion 12 is also cylindrical with a largerdiameterthan the end portions. Between the intermediate portion and the end portions,theshaft tapers uniformly.
The shaft is made in two parts, connected together at intermediate portion 12 by adhesively securing the two parts to an internal connecting sleeve 13. The parts would be manufactured by winding resin impregnated fibre on appropriately shaped mandrels, from which they are removed after the resin has been cured to form the finished shaft parts. The parts can subsequently be secured to the connecting sleeve 13 by use of suitable adhesives.
Figure 2 shows an alternative form of shaft, which again has short cylindrical end portions and uniformly increases in diameterto an intermediate portion therebetween. In this case, however, the shaft is made in one piece by winding fibres on a cylindrical mandrel which fits between the end portions thereof, and a former 14fitting on such mandrel and remaining in position in thefinished shaft. Theformer may,for example be made of a lightweight plastics material which does not unduly increase the weight of the finished shaft.
The illustrated tapered configurations of shaft are simplestto manufacture. However, it would be possibleforthe diameter of the shaftto increase in steps to its intermediate portion, or possibly even to vary in accordance with the bending moment diagram of an elongate element subjected to bending stress.
Byway of example only, the diameter of the intermediate portion of the shaft may be 3 to 4 times the diameter of the end portions thereof. The invention is of particular advantage when applied to relatively long shafts, where the phenomenon of whirling is a significant problem.
The shaft may incorporate at its end portions components forming part of or adapted for connec- tionto universal joints or shaft couplings.
1. Ashaftofa composite material including a portion, intermediate end portionsthereof, of a diametergreaterthan that of saidend portions.
2. Ashaft according to Claim 1 ofsubstantially constantwall thickness throughout its length.
3. A shaft according to Claim 1 orClaim 2wherein said diameter tapers uniformly from said intermediate portion to said end portions.
4. Ashaft according to Claim 1 or Claim 2 wherein said diameter decreases in steps from said intermediate portion to said end portions.
5. A shaft according to Claim 1 or Claim 2 wherein said diametervariesin accordancewiththe bending movement diagram of an elongate element subjected to bending stress.
6. Ashaftaccording to anyone ofthe preceding claims comprising two parts, secured together at said intermediate portion.
7. A shaft substantially as hereinbefore described with reference to Figure 1 or Figure 2 ofthe accom panying drawings.
The drawing(s) originally filed was (were) informal and the print here reproduced is taken from a later filed formal copy.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (7)

**WARNING** start of CLMS field may overlap end of DESC **. SPECIFICATION Shafts of composite material This invention relates to shafts made of composite, fibre reinforced resin, material. Ashaft made according to the invention may be used,for example, as the longitudinal drive shaft (propellor shaft) of a motor vehicle. One problem encountered in design of shafts of composite material is that a shaft may have sufficient torque transmitting capability but not be sufficiently stiff in bending to avoid a phenomenon known as whirling. This occurs above a critical rotational speed, atwhich the shaft bends so that its central region rotates eccentrically. One way in which this problem can be overcome isforthe bending stiffness of the shaftto be increased by increasing its diameter, but in typical installations the space available at the ends of the shaft is very limited so that this expedient cannot be adopted. If the diameter ofthe shaft cannot be increased, its wall thickness must be increased which adds to its weight and cost of manufacture, or high modulus fibres such as carbon fibres can be incorporated in the shaft construction. This again adds to cost of manufacture.It is the object of the present invention to overcome or reduce these disadvantages. According to the invention, we provide a shaft of composite material and including a portion, intermediate end portions thereof, of a diameter greater than that of said end portions. A shaft according to the invention thus achieves, by virtue of its greater diameter in its intermediate portion, a greater bending stiffessthan if it were of the same diameteras its end portionsthroughout However, the end portions of the shaft remain of a conveniently small diameter for installation purposes. The shaft may be of su bsta ntiallyconsta nt wal I thicknessthroughoyt its length and may taper uni- formlyfrom the intermediate portion to its end portions. Alternatively, its diameter may decrease in steps from its intermediate portion to its end portions. Shafts of fibre reinforced resin material are normally made by winding fibres, impregnated with resin, over a mandrel. Because of the impossibility of removing a mandrel from the interiorofa one piece shaft according to the invention, the invention provides thatthe shaft may be in two parts, secured together at said intermediate portion. The two parts may be secured together, for example, by being adhesively secured to an internal or an external connecting sleeve. Itwould, however, be possible forthe shaftto be made in one piece ifaformerwere used which remains in position in the interior of the shaft. The invention will now be described by way of example with reference to the accompanying drawings; FIGURE 1 andFlGURE2,whicharediagramma- tic sections through embodiments of shaft according to the invention. Referring firstly to Figure 1,there is shown a shaft comprising two end portions 10, 11 and an intermediate portion 12. The end portions 10, 11 are cylindrical, and the intermediate portion 12 is also cylindrical with a largerdiameterthan the end portions. Between the intermediate portion and the end portions,theshaft tapers uniformly. The shaft is made in two parts, connected together at intermediate portion 12 by adhesively securing the two parts to an internal connecting sleeve 13. The parts would be manufactured by winding resin impregnated fibre on appropriately shaped mandrels, from which they are removed after the resin has been cured to form the finished shaft parts. The parts can subsequently be secured to the connecting sleeve 13 by use of suitable adhesives. Figure 2 shows an alternative form of shaft, which again has short cylindrical end portions and uniformly increases in diameterto an intermediate portion therebetween. In this case, however, the shaft is made in one piece by winding fibres on a cylindrical mandrel which fits between the end portions thereof, and a former 14fitting on such mandrel and remaining in position in thefinished shaft. Theformer may,for example be made of a lightweight plastics material which does not unduly increase the weight of the finished shaft. The illustrated tapered configurations of shaft are simplestto manufacture. However, it would be possibleforthe diameter of the shaftto increase in steps to its intermediate portion, or possibly even to vary in accordance with the bending moment diagram of an elongate element subjected to bending stress. Byway of example only, the diameter of the intermediate portion of the shaft may be 3 to 4 times the diameter of the end portions thereof. The invention is of particular advantage when applied to relatively long shafts, where the phenomenon of whirling is a significant problem. The shaft may incorporate at its end portions components forming part of or adapted for connec- tionto universal joints or shaft couplings. CLAIMS
1. Ashaftofa composite material including a portion, intermediate end portionsthereof, of a diametergreaterthan that of saidend portions.
2. Ashaft according to Claim 1 ofsubstantially constantwall thickness throughout its length.
3. A shaft according to Claim 1 orClaim 2wherein said diameter tapers uniformly from said intermediate portion to said end portions.
4. Ashaft according to Claim 1 or Claim 2 wherein said diameter decreases in steps from said intermediate portion to said end portions.
5. A shaft according to Claim 1 or Claim 2 wherein said diametervariesin accordancewiththe bending movement diagram of an elongate element subjected to bending stress.
6. Ashaftaccording to anyone ofthe preceding claims comprising two parts, secured together at said intermediate portion.
7. A shaft substantially as hereinbefore described with reference to Figure 1 or Figure 2 ofthe accom panying drawings.
The drawing(s) originally filed was (were) informal and the print here reproduced is taken from a later filed formal copy.
GB08310354A 1983-04-16 1983-04-16 Shafts Withdrawn GB2138921A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB08310354A GB2138921A (en) 1983-04-16 1983-04-16 Shafts

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08310354A GB2138921A (en) 1983-04-16 1983-04-16 Shafts

Publications (2)

Publication Number Publication Date
GB8310354D0 GB8310354D0 (en) 1983-05-18
GB2138921A true GB2138921A (en) 1984-10-31

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
GB08310354A Withdrawn GB2138921A (en) 1983-04-16 1983-04-16 Shafts

Country Status (1)

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GB (1) GB2138921A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3615858A1 (en) * 1985-05-24 1986-11-27 Volkswagen AG, 3180 Wolfsburg Wheel drive for motor vehicles
US4838833A (en) * 1986-08-15 1989-06-13 A. O. Smith Corporation Fiber reinforced resin drive shaft having improved resistance to torsional buckling
DE3740754A1 (en) * 1987-12-02 1989-06-22 Loehr & Bromkamp Gmbh Longitudinal shaft for power trains in motor vehicles
GB2215008A (en) * 1988-02-17 1989-09-13 Smith Corp A O Fiber reinforced resin drive shaft having improved resistance to torsional buckling
EP0356844A2 (en) * 1988-08-31 1990-03-07 BASF Aktiengesellschaft Hollow shaft made of fiber-reinforced plastics
GB2242960A (en) * 1990-04-04 1991-10-16 Gkn Automotive Ag Drive shaft for a motor vehicle
EP0471240A2 (en) * 1990-08-16 1992-02-19 Elastogran GmbH Hollow shaft made of fibre reinforced plastic
US5320579A (en) * 1990-06-23 1994-06-14 Gkn Automotive Ag Energy absorbing driveshaft connections
EP0621411A1 (en) * 1993-04-20 1994-10-26 Firma Carl Freudenberg Composite roll
DE19908604A1 (en) * 1999-02-27 1999-12-30 Daimler Chrysler Ag Driveshaft for motor vehicles

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1356393A (en) * 1970-10-06 1974-06-12 British Aircraft Corp Ltd Composite structures
GB2010446A (en) * 1977-12-02 1979-06-27 Exxon Research Engineering Co Composite Tubular Element
GB2017272A (en) * 1978-03-17 1979-10-03 Ici Australia Ltd Igniting incndiary fusecords
GB2017260A (en) * 1978-03-27 1979-10-03 Celanese Corp Carbon fibre reinforced composite drive shaft
GB2051303A (en) * 1979-05-29 1981-01-14 Celanese Corp Fibre-reinforced composite shaft with metallic connector sleeves
EP0030996A1 (en) * 1979-12-21 1981-07-01 Felten &amp; Guilleaume Energietechnik GmbH Driving shaft of fibre-reinforced synthetic material with lost mandril and tightly wound end pieces
EP0052077A1 (en) * 1980-11-06 1982-05-19 Colcon Anstalt Method of producing an axially symmetrical hollow shaft
GB2108630A (en) * 1981-11-05 1983-05-18 Ford Motor Co Driveshaft for a motor vehicle

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1356393A (en) * 1970-10-06 1974-06-12 British Aircraft Corp Ltd Composite structures
GB2010446A (en) * 1977-12-02 1979-06-27 Exxon Research Engineering Co Composite Tubular Element
GB2017272A (en) * 1978-03-17 1979-10-03 Ici Australia Ltd Igniting incndiary fusecords
GB2017260A (en) * 1978-03-27 1979-10-03 Celanese Corp Carbon fibre reinforced composite drive shaft
GB2051303A (en) * 1979-05-29 1981-01-14 Celanese Corp Fibre-reinforced composite shaft with metallic connector sleeves
EP0030996A1 (en) * 1979-12-21 1981-07-01 Felten &amp; Guilleaume Energietechnik GmbH Driving shaft of fibre-reinforced synthetic material with lost mandril and tightly wound end pieces
EP0052077A1 (en) * 1980-11-06 1982-05-19 Colcon Anstalt Method of producing an axially symmetrical hollow shaft
GB2108630A (en) * 1981-11-05 1983-05-18 Ford Motor Co Driveshaft for a motor vehicle

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3615858A1 (en) * 1985-05-24 1986-11-27 Volkswagen AG, 3180 Wolfsburg Wheel drive for motor vehicles
US4838833A (en) * 1986-08-15 1989-06-13 A. O. Smith Corporation Fiber reinforced resin drive shaft having improved resistance to torsional buckling
DE3740754A1 (en) * 1987-12-02 1989-06-22 Loehr & Bromkamp Gmbh Longitudinal shaft for power trains in motor vehicles
GB2215008A (en) * 1988-02-17 1989-09-13 Smith Corp A O Fiber reinforced resin drive shaft having improved resistance to torsional buckling
EP0356844A2 (en) * 1988-08-31 1990-03-07 BASF Aktiengesellschaft Hollow shaft made of fiber-reinforced plastics
EP0356844A3 (en) * 1988-08-31 1990-11-14 BASF Aktiengesellschaft Hollow shaft made of fiber-reinforced plastics
GB2242960A (en) * 1990-04-04 1991-10-16 Gkn Automotive Ag Drive shaft for a motor vehicle
GB2242960B (en) * 1990-04-04 1993-06-30 Gkn Automotive Ag Drive shaft
US5320579A (en) * 1990-06-23 1994-06-14 Gkn Automotive Ag Energy absorbing driveshaft connections
EP0471240A2 (en) * 1990-08-16 1992-02-19 Elastogran GmbH Hollow shaft made of fibre reinforced plastic
EP0471240A3 (en) * 1990-08-16 1993-03-10 Elastogran Kunststoff-Technik Gmbh Hollow shaft made of fibre reinforced plastic
EP0621411A1 (en) * 1993-04-20 1994-10-26 Firma Carl Freudenberg Composite roll
DE19908604A1 (en) * 1999-02-27 1999-12-30 Daimler Chrysler Ag Driveshaft for motor vehicles

Also Published As

Publication number Publication date
GB8310354D0 (en) 1983-05-18

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Legal Events

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