FAIL SAFE BEARING

Abstract

A rotating shaft assembly comprising a rotating shaft 1 mounted within a casing, and a primary bearing assembly in bearing engagement with the shaft and the casing and positioned between the shaft and the casing; the assembly further comprising a secondary bearing assembly comprising a secondary bearing normally radially spaced from the shaft and arranged to engage with or contact the shaft in the event of failure of the primary bearing normally in contact with the shaft, and means for insertion and/or removal of an inspection member to provide an indication of frictional engagement of the secondary bearing with the shaft.

Claims

1. A bearing assembly comprising a secondary bearing arranged to make contact with a rotating part in the event of failure of a primary bearing normally in contact with the rotating part, and means for insertion and/or removal of an inspection member to provide an indication of engagement of the secondary bearing with the rotating part.

2. A method of identifying failure of a primary bearing, in a bearing assembly, by examining a mechanical property of an inspection member inserted in the bearing assembly for an indication of engagement of a secondary bearing with a rotating part, wherein the primary bearing is normally in engagement with the rotating part and the secondary bearing is normally not in engagement with the rotating part, the secondary bearing coming into engagement with the rotating part in the event of failure of the primary bearing.

3. The method of claim 2, wherein the secondary bearing includes the removable inspection member such that a property of the inspection member changes due to engagement of the secondary bearing with the rotating part.

4. The method of claim 3, wherein the inspection member comprises a pin in the secondary bearing that also contacts the rotating member along with the secondary bearing and whose physical properties are changed by the contact.

5. The method of claim 3, wherein the bearing assembly is provided with one or more inspection ports via which a relative position and/or backlash of the rotating part with respect to the secondary bearing can be determined by insertion of an inspection member.

6. The apparatus of claim 1, wherein the secondary bearing includes the removable inspection member such that a property of the inspection member changes due to engagement of the secondary bearing with the rotating part.

7. The apparatus of claim 6, wherein the inspection member comprises a pin in the secondary bearing that also contacts the rotating member along with the secondary bearing and whose physical properties are changed by the contact.

8. The apparatus of claim 6, wherein the bearing assembly is provided with one or more inspection ports via which a relative position and/or backlash of the rotating part with respect to the secondary bearing can be determined by insertion of an inspection member.

9. A rotating shaft assembly comprising a rotating shaft mounted within a casing, and a primary bearing assembly in bearing engagement with the shaft and the casing and positioned between the shaft and the casing; the assembly further comprising a secondary bearing assembly comprising a secondary bearing normally radially spaced from the shaft and arranged to engage with the shaft in the event of failure of the primary bearing normally in contact with the shaft, and means for insertion and/or removal of an inspection member to provide an indication of engagement of the secondary bearing with the shaft.

Description

BRIEF DESCRIPTON OF THE DRAWINGS

[0016] FIG. 1 is a side section view of an embodiment of the fail safe bearing assembly of the present disclosure.

[0017] FIG. 2 is a schematic view of a detail of one embodiment of the fail safe bearing assembly.

[0018] FIG. 3 is a schematic view of another embodiment of the fail safe bearing assembly.

DETAILED DESCRIPTION

[0019] The bearing assembly will be described in relation to a shaft in an aircraft, e.g. in a flight control actuator, by way of example. The bearing assembly can, however, be used with any rotating parts having a bearing.

[0020] Referring to FIG. 1, part of an aircraft actuator is shown by way of an example of an application for the bearing assembly of the present disclosure.

[0021] The actuator includes a rotating shaft 1 mounted within a casing 2. The other components of the actuator are standard and will not be described herein.

[0022] A primary bearing 3 is provided between the rotating shaft 1 and the casing 2. The primary bearing 3 is, in normal operation, loaded—i.e. is in engagement with the shaft 1.

[0023] The assembly also comprises a secondary bearing assembly 4, axially displaced, with respect to the shaft longitudinal axis, from the primary bearing 3.

[0024] In the preferred arrangement, the rotating shaft 1 extends axially beyond the primary bearing 3. The secondary bearing is mounted in the casing surrounding this axially extended part of the shaft 1.

[0025] During normal operation, the primary bearing is in engagement with the shaft 1 and the casing and the secondary bearing assembly 4 is, in normal operation, unloaded—i.e. it is normally radially spaced from the shaft so that it is not in engagement with the shaft.

[0026] In the event of a failure in the primary bearing 3, the shaft 1 will move towards the casing 2 creating a backlash effect. The secondary bearing assembly acts as a fail safe bearing and ‘catches’ the shaft so that it can continue to rotate, thus avoiding a catastrophic failure. The secondary bearing is then in frictional engagement with the shaft.

[0027] In other words, when the primary bearing fails, the bearing or loading effect between the shaft 1 and the casing is removed and there is a backlash movement of the shaft 1 towards the casing. The secondary bearing assembly 4 is positioned on the casing such that the shaft 1 then comes into frictional engagement with the secondary bearing, rather than with the casing, and can continue to rotate using the secondary bearing assembly 4.

[0028] The secondary bearing assembly is, however, only an emergency solution for example while the aircraft is in flight, and it is important that failure of the primary bearing is notified so that this can be repaired as soon as possible.

[0029] According to the present disclosure, this notification is provided by means of a witness part or inspection member that indicates when the primary bearing has failed.

[0030] In the embodiment shown in FIG. 2, the witness part or inspection member is a pin 5 or the like positioned within the secondary bearing such that as the secondary bearing comes into engagement with the shaft 1, the pin 5 also engages with the rotating shaft. This engagement of the pin 5 causes, for example, wear or some other change in characteristic or property of the pin such as distortion of plastic distortion e.g. if the pin is made of a softer material. At an appropriate time (e.g. after the aircraft has landed) the pin 5 can be removed and examined for wear etc. which would indicate frictional engagement with the shaft and, therefore, indicate that the secondary bearing was in use, and, thus, failure of the primary bearing.

[0031] In an alternative embodiment shown in FIG. 3, an integrated witness part is not required; instead, the bearing assembly and/or casing is provided with one or more inspection ports 6. These are preferably closed, during normal operation, by e.g. a sealing plug 7 which can be removed for inspection purposes. During a maintenance check, the radial backlash of the shaft 1 can be measured through the port(s) 6 e.g. by insertion of a jig (not shown) or the like. In the embodiment shown in FIG. 3, the assembly is provided with two diametrically opposing inspection ports 6. The backlash can be measured by inserting jigs into the ports and pushing the shaft alternately from each side to identify the degree of backlash and thus identify whether the primary bearing has failed.

[0032] With the present arrangement, it is possible to detect engagement of the secondary bearing and, thus, failure of the primary bearing without needing to disassemble the entire unit in which the shaft rotates and without, therefore, needing to drain away lubricant etc. The secondary bearing allows the shaft etc. to continue to rotate safely in the event of failure of the primary bearing until inspection/maintenance is possible and then failure of the primary bearing can be easily identified during a simple inspection/maintenance routine.