The present disclosure relates generally to selector levers and, more particularly, to a failure detection mechanism for selector levers that may be found, for example, in the cockpit of an aircraft.
Conventional aircraft are commonly equipped with a selector lever for manually controlling the actuation of flaps, ailerons, or other moveable features of the aircraft. The selector lever is mounted in the cockpit for the pilot to select the desired equipment configuration by moving the lever to a position corresponding to the desired equipment configuration. The conventional selector lever is typically constructed with a shaft rotatably arranged adjacent one or two detent plates. One or two detent pins corresponding to the detent plates are movably arranged on the shaft. This configuration provides a measure of redundancy that allows the selector lever to be functional after one detent pin has failed. The ability to detect the failure of one or both detent pins would reduce maintenance costs and improve aircraft safety. Accordingly, the industry is receptive to new developments that provide the capability to detect the failure of a detent pin.
Disclosed herein is a selector lever having a shaft with a proximal end disposed in a housing and a distal end extending from the housing. A slide arranged to be movable along the shaft with a first detent pin and a second detent pin operatively connected to the slide. A first detent plate is disposed in the housing and arranged to receive the first detent pin, having a first plurality connected by a first channel. The first channel containing one or more first obstructing features. A second detent plate is disposed in the housing and having a second plurality of slots for receiving the second detent pin, the second plurality of slots being connected by a second channel. The second channel contains one or more second obstructing features, wherein the second plurality of slots are arranged to align with the first plurality of slots. The one or more second obstructing features are arranged to be not aligned with the one or more first obstructing features
Another aspect of the disclosure provides a method of detecting the failure of a selector lever.
The following descriptions should not be considered limiting in any way. With reference to the accompanying drawings, like elements are numbered alike:
A detailed description of one or more embodiments of the disclosed apparatus and method are presented herein by way of exemplification and not limitation with reference to the Figures. It is to be understood that other embodiments may be utilized and changes may be made without departing from the scope of the present disclosure. In particular, the disclosure provides various examples related to a selector lever for aircraft, whereas the advantages of the present disclosure as applied in a related field would be apparent to one having ordinary skill in the art and are considered to be within the scope of the present invention.
The selector lever 5 further comprises a second detent plate 14, (having a second plurality of slots 15), arranged opposite from the first detent plate 11. Further, a second detent pin 16 is arranged on the shaft 6 to engage the second plurality of slots 15 of the second detent plate 14, the second detent pin 13 being operatively connected to a second slide 17, the second slide capable of being operated independently from the slide 10. The second detent plate 14 and second detent pin 16 mirror the first detent plate 11 and first detent pin 13.
The selector lever 5 further includes one or more obstructing features in the channel 17 of one or both detent plates to test for a detent pin failure. A first obstructing feature 18 is placed in the channel 17 of the first detent plate 11, shown at one end of the channel 17. A second obstructing feature 19 is placed in the channel 17 of the second detent plate 14. The obstructing features 18, 19 are placed at different locations in the channels 17 of the respective detent plates 11, 14. The obstructing features 18, 19 may, for example, be formed as force ramps at the ends of the channel 17 (as shown), but may also be gates, ramps at other locations in the channel 17, or tactile sections including bumps that would be felt by the operator while moving the shaft 6 through the obstructing features 18, 19 while the respective detent pins 13, 16 are intact. The selctor lever 5 may include a plurality of obstructing features 18, 19 on each detent plate 11, 14. The first obstructing feature 18 of the first detent plate 11 should not be aligned with the second obstructing feature 19 of the second detent plate 14. This arrangement allows the operator to test for a failure of the detent pins 13, 16 individually.
The selector lever 5 may also comprise one or more biasing elements. For example, a first biasing element biases the first slide towards an engaged position and a second biasing element biases the second slide towards an engaged position.
The selector lever 5 of the present disclosure may be used to test the whether the detent pins 13, 16 remain intact. The detent pins 13, 16 are tested individually, without removing the housing 8 or requiring other maintenance procedures. For example, when moving the shaft 6 from one position to another, the operator can judge the integrity of the detent pins 13, 16 by observing the respective indicators 20, 21, 22.
The same procedure may then be used to determine the integrity of the remaining detent pin. For example,
While the invention has been described with reference to an exemplary embodiment or embodiments, it will be understood by those skilled in the art that various changes may be made and equivalents may be substituted for elements thereof without departing from the scope of the invention. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the invention without departing from the essential scope thereof. Also, in the drawings and the description, there have been disclosed exemplary embodiments of the invention and, although specific terms may have been employed, they are unless otherwise stated used in a generic and descriptive sense only and not for purposes of limitation, the scope of the invention therefore not being so limited. Moreover, the use of the terms first, second, etc., do not denote any order or importance, but rather the terms first, second, etc. are used to distinguish one element from another. Furthermore, the use of the terms a, an, etc. do not denote a limitation of quantity, but rather denote the presence of at least one of the referenced item.