Seal assemblies for use with drooped spoilers and other control surfaces on aircraft

A seal assembly for use with an aircraft, the aircraft having a movable control surface spaced apart from a fixed airfoil portion to define a gap therebetween, the seal assembly comprising:

• a first seal member having a first proximal portion and a first distal portion, wherein the first proximal portion is fixedly attached to the fixed airfoil portion and the first distal portion extends outwardly from the fixed airfoil portion toward the movable control surface;
• and
• a second seal member having a second proximal portion and a second distal portion, wherein the second proximal portion is fixedly attached to the movable control surface and the second distal portion extends outwardly from the movable control surface toward the fixed airfoil portion, and wherein the second distal portion moveably contacts the first distal portion of the first seal member to at least partially cover the gap between the first airfoil portion and the movable control surface as the movable control surface rotates downwardly relative to the fixed airfoil portion;
• wherein the gap is uncovered between the movable control surface and the fixed airfoil portion as the movable control surface rotates upwardly relative to the fixed airfoil portion;
• wherein the first distal portion includes an outer-facing surface and the second distal portion includes an inner-facing surface, and wherein the inner-facing surface is configured to slide across the outer-facing surface as the movable control surface moves relative to the fixed airfoil portion.

A seal assembly for use with an aircraft, the aircraft having a movable control surface spaced apart from a fixed airfoil portion to define a gap therebetween, the seal assembly comprising:

• a first seal member having a first proximal portion and a first distal portion, wherein the first proximal portion is fixedly attached to the fixed airfoil portion and the first distal portion extends outwardly from the fixed airfoil portion toward the movable control surface;
• a second seal member having a second proximal portion and a second distal portion, wherein the second proximal portion is fixedly attached to the movable control surface and the second distal portion extends outwardly from the movable control surface toward the fixed airfoil portion, and wherein the second distal portion movably contacts the first distal portion of the first seal member to cover the gap between the fixed airfoil portion and the movable control surface as the movable control surface moves relative to the fixed airfoil portion;
• a damper support fixedly attached to the fixed airfoil portion;
• and
• a vibration damper directly attached to the first distal portion of the first seal member and carried by the damper support.

A Method for sealing a gap between a movable control surface and a fixed airfoil portion on an aircraft, the method comprising:

• fixedly attaching a first proximal portion of a first seal member to the fixed airfoil portion, whereby a first distal portion of the first seal member extends outwardly from the fixed airfoil portion toward the movable control surface;
• pressing inwardly against the first distal portion of the first seal member with a second distal portion of a second seal member;
• fixedly attaching a second proximal portion of the second seal member to the movable control surface;
• fixedly attaching a damper support to the fixed airfoil portion;
• and
• positioning a motion damper between the damper support and the first distal portion of the first seal member.

An aircraft having a system for sealing a gap between a spoiler and a fixed wing portion, the system comprising:

• first seal means fixedly attached to the fixed wing portion;
• second seal means fixedly attached to the spoiler;
• and
• means for pressing a first distal portion of the first seal means against a second distal portion of the second seal means to maintain contact between the first and second seal means and at least partially cover the gap as the spoiler rotates downwardly relative to the fixed wing portion, wherein the system further comprises means for uncovering the gap between the spoiler and the fixed wing portion as the spoiler rotates upwardly relative to the fixed wing portion, and
• means for dampening vibrations of the first seal means.

A seal assembly for use with an aircraft, the aircraft having a movable control surface spaced apart from a fixed airfoil portion to define a gap therebetween, the seal assembly comprising:

• a first seal member formed from resilient material, the first seal member having a first proximal portion and a first distal portion, wherein the first proximal portion is fixedly attached to the fixed airfoil portion, wherein the first distal portion extends outwardly from the fixed airfoil portion toward the movable control surface, and wherein the first distal portion includes an outer-facing surface;
• a second seal member formed from stiff material that is different than the resilient material, the second seal member having a second proximal portion and a second distal portion, wherein the second proximal portion is fixedly attached to the movable control surface, wherein the second distal portion includes an inner-facing surface that presses against the outer-facing surface of the first distal portion and deflects the first seal member into a decreased radius as the movable control surface rotates downwardly relative to the fixed airfoil portion, and wherein the second distal portion separates from the first distal portion to form a gap therebetween when the movable control surface rotates upwardly relative to the fixed airfoil portion;
• a damper support fixedly attached to the fixed airfoil portion;
• and
• a vibration damper carried by the damper support and operably coupled to the first distal portion of the first seal member.