Mechanical position indicators for aircraft landing gear
A technology for aircraft landing gear and indicators, which is applied in the field of aircraft landing gear and mechanical position indicators, and can solve problems such as difficult to determine equipment by trial
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[0033] figure 1 A schematic partial view of an aircraft landing gear 1 is shown. The landing gear 1 comprises a bogie beam 3 pivotally coupled to a slider 5 at a bogie pivot 7 . These aspects of the undercarriage 1 are conventional and are therefore not described in any detail here.
[0034] A mechanical position indicator 9 according to an embodiment of the invention is coupled to the bogie beam 3 . The position indicator 9 has a first state and a second state and is arranged to change from the first state to the second state when the bogie beam 3 assumes a predetermined position relative to the slider. The position indicator 9 is arranged such that it inhibits a transition from the second state back to the first state. Thus, the position indicator 9 provides an indication that the bogie beam 3 has assumed a predetermined position relative to the slider 5 . In some embodiments, this enables omission of stop pads (which are normally provided on the bogie beam 3 at location...
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