This application claims priority to German Patent Application DE102010048926.3 filed Oct. 19, 2010, the entirety of which is incorporated by reference herein.
This invention relates to a high-speed drive shaft, in particular to a radial shaft for a gas-turbine engine, including a metallic and hollow shaft shank with load transfer elements integrally formed onto its ends.
The radial shaft of a gas-turbine engine provided for driving a generator is usually designed as hollow-bored and honed metallic component with load transfer elements integrally formed onto its two ends. The connection to the engine or the generator, respectively, is made via the load transfer elements, for example provided with toothing, with the interconnection of a transmission. The manufacture of the known metallic radial shafts for gas-turbine engines involves heavy cost, since their tube cross-section varies to achieve a high bending stiffness and a correspondingly high critical bending speed, requiring expensive boring and honing processes. To minimize production-related imbalances and the bending stresses involved, high-precision and hence expensive balancing is also necessary. In addition, the high costs set limits on the frequently desired use of radial shafts at higher operating speed and/or with greater length and also with correspondingly higher bending stiffness and critical bending speed.
The suggestion has already been made to produce the radial shaft of gas-turbine engines completely from fiber-composite material or in a hybrid design using a tube made of fiber-composite material with metallic load transfer elements attached to its ends. However, an effective increase of the critical bending speed is not assured due to the reduced bending stiffness compared with a radial shaft made of metal. In addition, the torsional loads that are effective particularly in the area of the load transfer lead to critical stress conditions in the fiber-composite material.
The present invention, in a broad aspect, provides a radial shaft with high bending stiffness and high critical bending speed which can be produced inexpensively and operated in an increased speed range even with greater length.
The underlying idea of the invention is to provide for decoupling of the torsional load transmission and flexural stiffening of the drive shaft in that the shaft shank provided at the ends with load transfer elements includes a metal tube prefabricated as a semi-finished part, designed only for transmission of torsional loads and having a constant wall thickness, and an outer or inner reinforcement intended only for ensuring the necessary bending stiffness on the outer or inner circumferential surface of the metal tube and made from a fiber-composite layer with fibers oriented in the longitudinal direction of the drive shaft, where the fiber-composite layer acting as the outer reinforcement is sheathed with an outer fiber-composite layer made from fibers oriented at an angle of 60° to 90° relative to the longitudinal direction.
The high-speed drive shaft thus formed and intended in particular as a radial shaft for a gas-turbine engine can be manufactured at low cost. The outer or inner reinforcement made of fiber-composite material for the metal tube designed only for torque transmission and hence slender ensures such a high flexural stiffening that longer drive shafts with higher operating speed can be used thanks to a resultant significant increase in the critical bending speed at the same torque. Its use as a radial shaft thus results in new possibilities for engine design.
In a further embodiment of the present invention, the fiber-composite layer formed out of axially oriented fibers is made of fiber-composite material compressed into half-shells, so that a high fiber density and hence an even higher bending stiffness can be achieved.
An intermediate layer designed as a sliding layer to compensate for heat-related longitudinal expansions is provided between the metal tube and the fiber-composite layer contacting the metal tube. The intermediate layer can also be designed as an adhesive layer, as an elastic layer and/or as a corrosion-preventing layer.
In accordance with yet another feature of the invention, the inner fiber-composite layer of the outer reinforcement is fixed in the longitudinal direction by a positioning ring provided centrally on the outer circumference of the metal tube.
In a further embodiment of the invention, the fiber-composite layer acting as inner reinforcement is fixed by covers fitted on both sides inside the metal tube which at the same time prevent any passage of liquid through the metal tube and protect the fiber-composite layer from external effects.
The fiber-composite layers are made of, in an advantageous embodiment of the invention, glass, carbon and/or aramide fibers embedded into a polymer matrix.
In a further embodiment, the metal tube is designed as a straight or conically tapering tube of circular cross-section.
The load transfer elements, for example provided with outer toothing, are preferably produced separately and connected to the ends of the metal tube by welding, in particular friction welding.
The present invention is more fully described in light of the accompanying drawings showing preferred embodiments. In the drawings,
The radial shaft shown in
The inner fiber-composite layer 13 includes, in accordance with the present embodiment, two prefabricated half-shells (see, for example,
Instead of the outer reinforcement 5, an inner reinforcement 8 can also be applied to the inner circumferential surface of the metal tube 3 which is like the outer reinforcement 5—however without fiber-composite layer 14—and therefore, has a fiber-composite layer 13 with axially oriented fibres.
Thanks to the formation of the previously described radial shaft from a prefabricated simple metal tube as a semi-finished part and from an outer or inner reinforcement, respectively, of fiber-composite material, and also thanks to the expensive balancing measures required for conventional radial shafts no longer being needed, the costs of manufacture are low. The metal tube is designed only for the transmission of torsional loads and has a correspondingly low mass and comparatively low diameter, whereas the bending stiffness required for a high speed is assured by the inner or outer reinforcement consisting of lightweight fiber-composite material. Thanks to the resultant significant increase in the critical bending speed, it is possible to manufacture also longer radial shafts inexpensively and in addition to operate them at higher speeds. For example, a radial shaft of 0.5 m length previously operated with 15,000 to 25,000 revolutions per second can in the embodiment described above be designed twice as long and operated at a speed of up to 45,000 revolutions per second.
Number | Date | Country | Kind |
---|---|---|---|
10 2010 048 926 | Oct 2010 | DE | national |
Number | Name | Date | Kind |
---|---|---|---|
5222296 | Doorbar et al. | Jun 1993 | A |
5731527 | Van Cleve | Mar 1998 | A |
6287209 | Nakajima et al. | Sep 2001 | B1 |
20080045348 | Shin | Feb 2008 | A1 |
20100109184 | Schreiber et al. | May 2010 | A1 |
20100113170 | Schreiber et al. | May 2010 | A1 |
20100113171 | Schreiber et al. | May 2010 | A1 |
Number | Date | Country |
---|---|---|
102008056017 | May 2010 | DE |
102008056018 | May 2010 | DE |
1083345 | Mar 2001 | EP |
1939395 | Jul 2008 | EP |
Number | Date | Country | |
---|---|---|---|
20120094777 A1 | Apr 2012 | US |