Emergency Gravity Free-fall Deployment Systems For Retractable Aircraft Landing Gear Assemblies
A deployment system, landing gear technology, applied in the direction of the chassis, etc., which can solve problems such as lack of harmonious movement, ineffective structure and/or equipment, jamming of landing gear doors, etc.
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[0021] According to an embodiment of the present invention, figure 1 The layout of an emergency aircraft landing gear deployment system 10 installed in a transport category aircraft AC is depicted. In this regard, aircraft AC will include conventional port and starboard main and nose gear assemblies, indicated by reference numerals 10-P, 10-S and 10-N, respectively. As is conventional, when each of these assemblies 10-P, 10-S, and 10-N is in a retracted (i.e., flight) state, fuselage grooves (the assemblies retract into these fuselage groove) will be closed by one (or more) landing gear doors 12-P, 12-S and 12-N, respectively, so as to minimize contact with the landing gear assemblies 10-P, 10-S and 10-S during aircraft flight. 10-N and their associated air drag relative to fuselage grooves.
[0022] System 10 includes a pilot-actuated emergency gear deployment lever 14 positioned in a forward crew cab FCC of aircraft AC. The lever is operatively connected to the hydraulic ...
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