Back to results
US 8,783,285 B2Granted
Method and apparatus for a smart valve
AssigneeThe Boeing Company
InventorRichard L. Kulesha
Life of this patent
Estimating the term…
Abstract
A smart drain valve comprises a support plate, a bolt passing through a center of the support plate, an outer plate connected to a first end of the bolt, an inner plate connected to a second end of the bolt, and a spring positioned between the inner plate and the support plate. The spring is made of a shape memory material.
Claims19
A drain valve comprising:
- a first plate fastened to an interior surface of an enclosure on an aircraft, the first plate and the surface each comprising a respective substantially planar segment, each planar segment being substantially parallel to the other substantially planar segment;
- a bolt passing through an extension of the first plate and configured to move linearly through and substantially orthogonal to the substantially planar segment of the first plate, the extension being substantially orthogonal to the substantially planar segment of the first plate;
- a second plate connected to a first end of the bolt, the second plate being:
- substantially planar, substantially parallel to the first plate, and configured to transition between a first position in direct contact with the first plate, and a second position separated from the first plate in response to a linear movement of the bolt, such that an opening in the first plate permits fluid to exit the enclosure with the second plate in the second position, the first position comprising a first surface of the second plate being flush with a second outer surface of the enclosure, the first surface being a substantially planar surface facing away from the enclosure;
- a third plate connected to a second end of the bolt such that the bolt, the third plate, and the second plate move linearly together, the third plate configured such that the third plate limits a distance the second plate can move away from the first plate, and
- a shape memory alloy spring directly connected to both the first plate and the third plate, the shape memory alloy spring configured to deform, into a first shape and a second shape to position the second plate in the first position and the second position respectively.
3 more elements
A drain valve positioned on an aircraft, the drain valve comprising:
- an outer plate configured to transition between a first position and a second position through a linear movement of a slider connected to the outer plate, the first position comprising a surface of the outer plate being substantially flush with an exterior surface of the aircraft, the surface facing away from an interior of the aircraft;
- an inner plate fastened to an interior surface of the aircraft, the inner plate and the outer plate being substantially planar such that direct contact between the inner plate and the outer plate in the first position restricts fluid flow through an opening in the inner plate, and a separation between the inner plate and the outer plate in the second position permits fluid flow through the opening in the inner plate;
- a slider stop connected to the outer plate, the slider stop configured to limit a distance the outer plate moves away from the inner plate;
- an extension of the inner plate configured to encircle the slider, a first end of the slider connected to the outer plate, and a second end of the slider connected to the slider stop, the outer plate, and the slider stop connected to each other and configured to move linearly as the slider moves through the extension;
- and
- a shape memory alloy spring surrounding the extension of the inner plate and contacting the inner plate and the slider stop, the shape memory alloy spring configured to hold the outer plate in the first position, and in response to a trigger event to push the outer plate away from the inner plate.
3 more elements
Dependencies are inferred from the claim text.