Latch pin inhibitor for folding wing-tip aircraft
AssigneeThe Boeing Company
InventorsMichael E. Renzelmann, Mark H. Smith
Life of this patent
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AssigneeThe Boeing Company
InventorsMichael E. Renzelmann, Mark H. Smith
Estimating the term…
A folding wing tip (14) on an aircraft (2) carries a lug (16) that moves into alignment with lugs (6, 10) on the inboard wing portion (4) as the wings spread. The lug (16) pivots an inhibitor (28) that is interconnected by linkage to a valve spool (122). The pivoting of the inhibitor (28) causes the spool (122) to shift its position so that a sense port is brought into communication with a return port. Return pressure in the sense port indicates a spread wing condition. When the wing tip (14) is folded, springs move the inhibitor (28) and the valve spool (122) back to their original positions. This communicates the sense port with a pressure port to indicate a folded wing condition. The spool (122) is preferably also biased into its original position by fluid pressure. In addition, the lug (16) has a cam (92) that engages a roller (84) carried by the inhibitor (28) when the wing tip (14) is moved into a folded position. Abutment of the cam (92) and roller (84) pivots the inhibitor (28) back into its original position.
In an aircraft folding wing system of a type having first and second wing portions hingedly connected to each other, said portions including first and second lugs, respectively, each said lug having an opening, and said lugs being movable relative to each other along a spread pathway between a folded position and a spread position in which said openings are aligned for receiving a latch pin, apparatus for sensing said spread position, comprising:
In a system of a type having first and second structures hingedly connected to each other, said structures including first and second lugs, respectively, each said lug having an opening, and said lugs being movable relative to each other along a spread pathway between a folded position and a spread position in which said openings are aligned for receiving a latch pin, apparatus for sensing said spread position, comprising:
In an aircraft folding wing system of a type having first and second wing portions hingedly connected to each other, said portions including first and second lugs, respectively, each said lug having an opening, and said lugs being movable relative to each other between a folded position and a spread position in which said openings are aligned for receiving a latch pin, apparatus for inhibiting premature extension of the latch pin, comprising:
Dependencies are inferred from the claim text.