This application relates to composite drive shafts and methods of repair.
Drive shafts are utilized in any number of modern industrial applications. As one example, drive shafts are utilized to drive components in an aerospace environment. One specific application might be driving propellers associated with a helicopter, as an example.
Drive shafts might have some bending flexure along the length during operation. Thus, it is known to position dampers or other structures along the length of the drive shaft to limit this bending deflection. The dampers are often associated with a “rub ring” which is an element extending radially outwardly of the drive shaft to contact the damper and protect, therefore, the outer surface of the shaft in case of contact with the damper.
Historically, drive shafts were formed of metal and, in particular, often aluminum, titanium or steel. More recently, it has been proposed to provide drive shafts formed of composite materials.
Drive shafts may also become damaged. They are often replaced once damaged instead of being repaired.
A drive shaft has a central tubular portion formed of a polymer composite with imbedded fibers. It extends between a first end and a second end. The central tubular portion has an outer peripheral surface. There is at least one ring on the outer peripheral surface of the central tubular portion.
A method of repairing a composite material tube includes the steps of (a) identifying a damaged area on a composite tube, and (b) placing a patch on a surface of the tube and over the damaged area.
These and other features may be best understood from the following drawings and specification.
Rub rings 32 are shown on an outer peripheral surface 19 of the central tubular portion 30. The rub rings 32 are axially aligned with static components such as a damper 34. During operation, there may be flexing along the length of the central tubular portion 30 and the rub rings 32 may contact the damper 34 to limit that flexing.
The central tubular portion 30 is formed of a fiber-reinforced thermoplastic material. The components of the central tubular portion and the rings may be formed of the same or different fiber-reinforced polymer matrix composite materials. In one embodiment, the matrix 100 can be a thermoplastic polymer. In another embodiment, the matrix can be a thermoset polymer. Different types of reinforcing fibers 101, such as, for example, carbon fibers, glass fibers, organic fibers, or their combinations can be used in different embodiments. In different embodiments, the same or different fabrication processes, such as for example, automated fiber placement, filament winding, braiding, wrapping, etc. can be used to make separate composite tubes, flanges and, if applicable, diaphragms.
In embodiments, the ring could be formed of polymer material, with, or without, embedded fibers.
When central tubular portion 42 and ring 44 are formed of the same material, they may be bonded together during formation.
The ring 50 in the embodiment 46 may be formed of a different material than the central tubular portion 42. Ring 50 might be a distinct thermoplastic, a thermoset, or even a metallic component. Here too the same material may be used.
In other embodiments, layer 60 is not limited to elastomers. This layer 60 may be of a low friction material, such as for example Teflon, to provide efficient interaction with damping ring 34. Layer 60 could be generically called a cushioning member.
A drive shaft according to this disclosure could be said as having a central tubular portion formed of a thermoset resin with imbedded fibers, and extending between a first end and a second end. The center tubular portion has an outer peripheral surface and there is at least one ring on the outer peripheral surface of the central tubular portion.
A method of repairing a composite material tube could be said to include the steps of (a) identifying a damaged area on a composite tube; and (b) placing a patch(s) on a surface of the tube and over the damaged area.
When considering the drive shaft embodiments of
Although an embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this disclosure. For that reason, the following claims should be studied to determine the true scope and content of this disclosure.
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20200224711 A1 | Jul 2020 | US |