An airfoil having a trailing edge flap assembly comprising a flap member which in its stowed position is located above a fixed mounting structure. There is a rear pivot link connected at its lower end to the mounting structure and by its upper end to an aft portion of the flap. There is a forward sl
An airfoil having a trailing edge flap assembly comprising a flap member which in its stowed position is located above a fixed mounting structure. There is a rear pivot link connected at its lower end to the mounting structure and by its upper end to an aft portion of the flap. There is a forward slideway by which the forward part of the flap is mounted for longitudinal slide motion relative to the fixed mounting structure. The flap has a stowed position in the rear portion of the wing, and is movable rearwardly with substantial Fowler motion to an intermediate position for take-off, and movable further rearwardly to a fully extended position where the flap extends rearwardly and downwardly for take-off.
대표청구항▼
1. A flap assembly for an airfoil having upper and lower surfaces, a forward end and a rearward end, a longitudinal axis and a transverse axis, said flap assembly comprising: a mounting structure located at a first lower location at the rearward end of the airfoil; a flap member having a stowed firs
1. A flap assembly for an airfoil having upper and lower surfaces, a forward end and a rearward end, a longitudinal axis and a transverse axis, said flap assembly comprising: a mounting structure located at a first lower location at the rearward end of the airfoil; a flap member having a stowed first position above said mounting structure at the rearward end of said airfoil and movable rearwardly to a fully extended second position; a first link mounting means having a lower first pivot connecting means attached to said mounting structure at a first connecting location and an upper second pivot connecting means mounted to said flap member at an upper second connecting location; a track mounting means comprising track means and a third connecting means connected to said flap member and also operatively connected to said track means at a third connecting location positioned forwardly of said second connecting location; said track mounting means being characterized in that relative forward and rearward movement of said third connecting means is constrained to be along said track means on a forward and rearward first path of travel having a substantial longitudinal path component; said first link mounting means being characterized in that with said flap member in its stowed first position, initial rearward movement of said flap member causes said second pivot connecting means to move in a rearward path having a substantial longitudinal path component so as to provide substantial Fowler motion for said flap member, and further movement of said flap member to its fully extended position causes said flap member to deflect to a substantially downwardly and rearwardly extending position; a second flap having a third stowed position adjacent said flap member and movable rearwardly to a fourth fully deployed position, where said second flap is spaced from said flap member; said second flap being pivotally connected to said first link mounting means by fourth connecting means at a fourth connecting location, whereby rearward movement of said link mounting means moves said second flap toward its fourth position; and said fourth connecting location being spaced from said first connecting location at a distance greater than a distance which said second connecting location is spaced from said first connecting location, whereby rearward movement of said link mounting means moves said second flap rearwardly a greater distance than said flap member is moved. 2. The flap assembly as recited in claim 1, wherein said second flap member is mounted to said first flap member by second track mounting means comprising track means mounted to said flap member; and a fifth connecting means connected to said second track means so as to be movable along said second track means. 3. A flap assembly for an airfoil having upper and lower surfaces, a forward end and a rear end, a longitudinal axis and a transverse axis, said flap assembly comprising: a mounting structure located at a first lower location at the rearward end of the airfoil; a flap member having a stowed first position above said mounting structure at the rearward end of said airfoil and movable rearwardly to a fully extended second position; a first link mounting means having a lower first pivot connecting means attached to said mounting structure at a first connecting location and an upper second pivot connecting means mounted to said flap member at an upper second connecting location; a track mounting means comprising track means and a third connecting means connected to said flap member and also operatively connected to said track means at a third connecting location positioned forwardly of said second connecting location; said track mounting means being characterized in that relative forward and rearward movement of said third connecting means is constrained to be along said track means on a forward and rearward first path of travel having a substantial longitudinal path component; said first link mounting means being characterized in that said flap member in its stowed first position, initial rearward movement of said flap member causes said second pivot connecting means to move in a rearward path having a substantial longitudinal path component so as to provide substantial Fowler motion for said flap member, and further movement of said flap member to its fully extended position causes said flap member to deflect to a substantially downwardly and rearwardly extending position; a second flap having a third stowed position adjacent said flap member and movable rearwardly to a fourth fully deployed position, where said second flap is spaced from said flap member; said second flap being pivotally connected to said first link mounting means by a fourth connecting means at a fourth connecting location, whereby rearward movement of said link mounting means moves said second flap toward its fourth position; said second flap member being mounted to said first flap member by second track mounting means comprising track means mounted to said flap member; and a fifth connecting means connected to said second track means so as to be movable along said second track means. 4. A flap assembly for an airfoil having upper and lower surfaces, a forward end and a rearward end, a longitudinal axis and a transverse axis, said flap assembly comprising: a mounting structure located at a first lower location at the rearward end of the airfoil; a flap member having a stowed first position above said mounting structure at the rearward end of said airfoil and movable rearwardly to a fully extended second position; a second flap having a third stowed position adjacent said flap member, and movable rearwardly to a fourth fully deployed position, where said second flap is spaced from said flap member; a first link mounting means having a lower first pivot connecting means attached to said mounting structure at a first connecting location, and an upper second pivot connecting means mounted to said flap member at an upper second connecting location; a track mounting means comprising track means and a third connecting means connected to said flap member and also operatively connected to said track means at a third connecting location positioned forwardly of said second connecting location; said track mounting means being characterized in that relative forward and rearward movement of said third connecting means is constrained to be along said track means on a forward and rearward first path of travel having a substantial longitudinal path component; said first link mounting means being characterized in that with said flap member in its stowed first position, initial rearward movement of said flap member causes said second pivot connecting means to move in a rearward path having a substantial longitudinal path component so as to provide substantial Fowler motion for said flap member and said second flap, and further movement of said flap member to its fully extended position causes said flap member and said second flap each to deflect to a substantially downwardly and rearwardly extending position; said second flap being pivotally connected to said first link mounting means by fourth connecting means at a fourth connecting location, whereby rearward movement of said link mounting means moves said second flap toward its fourth position; said fourth connecting location being spaced from said first connecting location at a distance greater than a distance which said second connecting location is spaced from said first connecting location, whereby rearward movement of said link mounting means moves said second flap rearwardly a greater distance than said flap member is moved. 5. The flap assembly as recited in claim 4, wherein said second flap is mounted to said first flap member by second track mounting means comprising track means mounted to said flap member; and a fifth connecting means connected to said second track means so as to be movable along said second track means. 6. A flap assembly for an airfoil having upper and lower surfaces, a forward end and a rearward end, a longitudinal axis and a transverse axis, said flap assembly comprising: a mounting structure located at a first lower location at the rearward end of the airfoil; a flap member having a stowed first position above said mounting structure at the rearward end of said airfoil and movable rearwardly to a fully extended second position; a second flap having a third stowed position adjacent said flap member and movable rearwardly to a fourth fully deployed position, where said second flap is spaced from said flap member; a first link mounting means having a lower first pivot connecting means attached to said mounting structure at a first connecting location, and an upper second pivot connecting means mounted to said flap member at an upper second connecting location; a track mounting means comprising track means and a third connecting means connected to said flap member and also operatively connected to said track means at a third connecting location positioned forwardly of said second connecting location; said track mounting means being characterized in that relative forward and rearward movement of said third connecting means is constrained to be along said track means on a forward and rearward first path of travel having a substantial longitudinal path component; said first link mounting means being characterized in that with said flap member in its stowed first position; initial rearward movement of said flap member causes said second pivot connecting means to move in a rearward path having a substantial longitudinal path component so as to provide substantial Fowler motion for said flap member and said second flap, and further movement of said flap member to its fully extended position causes said flap member and said second flap each to deflect to a substantially downwardly and rearwardly extending position; said second flap being pivotally connected to said first link mounting means by a fourth connecting means at a fourth connecting location, whereby rearward movement of said link mounting means moves said second flap toward its fourth position; and said second flap member being mounted to said first flap member by a second track mounting means comprising track means mounted to said flap member; and a fifth connecting means connected to said second track means so as to be movable along said second track means.
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이 특허에 인용된 특허 (2)
Thornburg Francis L. (Canoga Park CA), Aileron segment control for a flaperon system.
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