Hinged door for aircraft landing gear
a, baaa, bThe door comprises a panel formed from two rigid parts hinged to each other edge to edge. A first part of these two parts is connected to the aircraft structure through a pivot pin and a control means is inserted between this first part and the structure. A kinematic control mechanism conn...
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| Main Author | |
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| Format | Patent |
| Language | English |
| Published |
20.02.2007
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| Online Access | Get full text |
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| Summary: | a, baaa, bThe door comprises a panel formed from two rigid parts hinged to each other edge to edge. A first part of these two parts is connected to the aircraft structure through a pivot pin and a control means is inserted between this first part and the structure. A kinematic control mechanism connects the two parts to the aircraft structure, so as to enable progressive and controlled folding of these parts when opening the door. Thus the landing gear door can be opened and closed without any risk of it coming into contact with the wheels when the landing gear is extended. |
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