Apparatus for compensating for airflow blockage in aircraft slotted flap assemblies

Claim 2

In an airplane flap assembly including a flap having an upper surface and a lower surface and an airplane wing wherein said flap is attached to said wing by at least one support means, said flap being positionable relative to said wing to define an airflow slot between said wing and the upper surface of said flap for directing air over the upper surface of said flap, said flap being retractable to define a substantially continuous aerodynamic surface with said airplane wing, said flap including a first recess in the upper surface thereof, said first recess extending rearwardly from the leading edge of said flap for receiving a portion of said support means when said flap is retracted, an improvement to compensate for the blockage of airflow caused by said support means over a region of the upper surface of said flap contiguous to said support means, said improvement comprising: an airflow duct of predetermined cross-sectional area, said airflow duct including an air inlet opening in the lower surface of said flap in communication with an air outlet opening positioned to direct air over said blocked airflow region of said upper flap surface; and means defining a second recess in a portion of said upper surface of said flap, said second recess being immediately adjacent and substantially parallel to said first recess, the boundary surfaces of said first and second recesses being contoured to form aerodynamically smooth surfaces for directing airflow to said blocked airflow region on the upper surface of said flap is positioned to define said airflow slot between said wing and said upper surface of said flap.

Claim 3

The improvement of claim 1, further comprising a pivotable cove panel for covering said second recess when said flap is in the retracted position, said pivotable cove panel being pivotably connected to the upper surface of said airplane wing, said cove panel swinging downwardly about said pivotable connection when said flap is extended to define an airflow slot between the trailing edge of said cove panel and the lower boundary surface of said second recess for regulating airflow through said second recess.

Claim 4

The improvement of claim 2, wherein said air outlet opening of said airflow duct is located immediately aft of said support member.

Claim 5

The improvement of claim 1, further comprising a door means for closing said inlet opening of said air flow duct when said flap is in its retracted position.

Claim 6

The improvement of claim 4 wherein said door means includes means for forming a portion of said airflow duct when said flap is in its extended position.

Claim 7

The improvement of claim 5, wherein said door means further includes means for forming a portion of the upper surface of said flap when said flap is in its retracted position.

Claim 8

The improvement of claim 6, further comprising a rotatable sidewall for forming one sidewall of said airflow duct when said flap is in an extended position, said sidewall hinged about a predetermined point on the upper surface of said flap, said sidewall rotating into the interior region of said flap when said flap is retracted.

Claim 9

In an airplane flap having an upper surface and a lower surface, said flap being attachable to an airplane wing by at least one flap support member extending rearwardly from said wing such that said flap is extendable from said airplane wing to define a spanwise slot between said wing and the upper surface of said flap for directing airflow across the upper surface of said flap, said flap being retractable to define a continuous aerodynamic surface with said wing, said upper surface of said flap including a first recess extending a predetermined distance from the leading edge of said flap toward the trailing edge of said flap for receiving and containing said flap support member when said flap is retracted, the improvement comprising: an airflow duct having an air inlet located in the lower surface of said flap and an air outlet located across the terminating portion of said first recess; and a rampway for directing an airstream flowing from said airflow duct air outlet to a portion of the upper surface of said flap aft of said first recess, said rampway defining an inclined surface between the aft edge of said airflow duct outlet and said portion of said upper surface of said flap, said airflow duct and said rampway directing said airstream across said portion of said upper flap surface aft of said recess to compensate for airflow blockage caused by said flap support member.

Claim 10

In an airplane flap having an upper surface and a lower surface, said flap being attachable to an airplane wing by at least one flap support member extending rearwardly from said wing such that said flap is extendable from said airplane wing to define a spanwise slot between said wing and the upper surface of said flap for directing airflow across the upper surface of said flap, said flap being retractable to define a continuous aerodynamic surface with said wing, said upper surface of said flap including a first recess extending a predetermined distance from the leading edge of said flap toward the trailing edge of said flap for receiving and containing said flap support member when said flap is retracted, the improvement comprising: an airflow duct having an air inlet located in the lower surface of said flap and an air outlet located across the terminating portion of said first recess; and a rampway for directing an airstream flowing from said airflow duct air outlet to a portion of the upper surface of said flap aft of said first recess, said rampway defining an inclined surface between the aft edge of said airflow duct outlet and said portion of said upper surface of said flap, said airflow duct and said rampway directing said airstream across said portion of said upper flap surface aft of said recess to compensate for airflow blockage caused by said flap support member.

Claim 11

The improvement of claim 8 further comprising means defining a second recess for directing additional airflow across the upper surface of said flap, said second recess located contiguous to said first recess, said second recess extending from the leading edge of said flap for a predetermined distance toward the trailing edge thereof, said second recess of decreasing depth relative to the direction of said airflow, said first and second recesses contoured to direct the airstream through said airflow duct to that portion of said flap upper surface located aft of said first and second recesses for maintaining laminar airflow across said portion of said flap upper surface aft of said first and second recesses.

Claim 12

The improved flap of claim 9 further comprising a closure door for sealing said air inlet when said flap is retracted.

Claim 13

The improved flap of claim 10, wherein said closure door defines a portion of the wall surface of said airflow duct when said flap is extended.

Claim 14

In an airplane flap assembly including a flap having an upper surface and a lower surface and an airplane wing wherein said flap is attached to extend spanwise along the trailing edge of said wing by at least one support means that extends between said wing and said flap, said flap being positionable relative to said wing to define a spanwise airflow slot between said wing and the upper surface of said flap for directing air over the upper surface of said flap with said slot extending for substantially the full spanwise dimension of said flap and said support means being disposed in the airstream directed through said airflow slot, said flap being retractable to define a substantially continuous aerodynamic surface with said airplane wing, said upper surface of said flap including a recessed region extending rearwardly from the leading edge of said flap to an aft terminating edge located forwardly of the trailing edge of said flap, said recessed region for receiving at least a portion of said support means when said flap is retracted, wherein the improvement comprises airflow means for directing a stream of air to a predetermined rearwardly extending portion of said upper surface of said flap that is contiguous to said support means to compensate for airflow blockage through a portion of said slot between said flap and said wing that is caused by disposing said support means in said airflow slot, said airflow means including: a rampway for directing that portion of the airflow which passes through said slot and into said recessed region of said flap upper surface upwardly and rearwardly for passage across a first portion of said upper surface of said flap that is located aft of said recessed region, said rampway defining an aerodynamically smooth inclined surface between said aft terminating edge of said recessed region and said first portion of said upper surface of said flap; and an airflow duct extending between an air inlet opening in the lower surface of said flap and an air outlet opening in the upper surface of said flap, said air inlet opening being located rearwardly of said flap leading edge and having a spanwise dimension substantially less than the spanwise dimension of said flap, said air outlet opening being located outboard of and substantially adjacent to said recessed region at a position intermediate to said leading edge of said flap and said aft terminating edge of said recessed region, said outlet opening having a spanwise dimension substantially less than the spanwise dimension of said flap, said airflow duct being configured and arranged to discharge the airstream passing through said airflow duct for rearward flow along at least a portion of said predetermined region of said flap upper surface in which said airflow blockage occurs, said airflow duct and said rampway being further configured and arranged for supplying airflow of sufficient volume and velocity to cause the combined airflow provided to said blocked airflow region by said airflow duct and by said airflow slot to energize a boundary layer of air along said blocked airflow region of said upper surface of said flap.

Claim 15

In an airplane flap assembly including a flap having an upper surface and a lower surface and an airplane wing wherein said flap is attached to extend spanwise along the trailing edge of said wing by at least one support means that extends between said wing and said flap, said flap being positionable relative to said wing to define a spanwise airflow slot between said wing and the upper surface of said flap for directing air over the upper surface of said flap with said slot extending for substantially the full spanwise dimension of said flap and said support means being disposed in the airstream directed through said airflow slot, said flap being retractable to define a substantially continuous aerodynamic surface with said airplane wing, said upper surface of said flap including a recessed region extending rearwardly from the leading edge of said flap to an aft terminating edge located forwardly of the trailing edge of said flap, said recessed region for receiving at least a portion of said support means when said flap is retracted, wherein the improvement comprises airflow means for directing a stream of air to a predetermined rearwardly extending portion of said upper surface of said flap that is contiguous to said support means to compensate for airflow blockage through a portion of said slot between said flap and said wing that is caused by disposing said support means in said airflow slot, said airflow means including: a rampway for directing that portion of the airflow which passes through said slot and into said recessed region of said flap upper surface upwardly and rearwardly for passage across a first portion of said upper surface of said flap that is located aft of said recessed region, said rampway defining an aerodynamically smooth inclined surface between said aft terminating edge of said recessed region and said first portion of said upper surface of said flap; and an airflow duct extending between an air inlet opening in the lower surface of said flap and an air outlet opening in the upper surface of said flap, said air inlet opening being located rearwardly of said flap leading edge and having a spanwise dimension substantially less than the spanwise dimension of said flap, said air outlet opening being located outboard of and substantially adjacent to said recessed region at a position intermediate to said leading edge of said flap and said aft terminating edge of said recessed region, said outlet opening having a spanwise dimension substantially less than the spanwise dimension of said flap, said airflow duct being configured and arranged to discharge the airstream passing through said airflow duct for rearward flow along at least a portion of said predetermined region of said flap upper surface in which said airflow blockage occurs, said airflow duct and said rampway being further configured and arranged for supplying airflow of sufficient volume and velocity to cause the combined airflow provided to said blocked airflow region by said airflow duct and by said airflow slot to energize a boundary layer of air along said blocked airflow region of said upper surface of said flap.

Claim 16

The improvement of claim 12, further comprising a door means for closing said inlet opening of said airflow duct when said flap is in its retracted position.

Claim 17

The improvement of claim 13 wherein said door means includes means for forming a portion of said airflow duct when said flap is in its extended position.

Claim 18

The improvement of claim 14, wherein said door means further includes means for forming a portion of the upper surface of said flap when said flap is in its retracted position.

Claim 19

The improvement of claim 15, further comprising a rotatable sidewall for forming one sidewall of said airflow duct when said flap is in an extended position, said sidewall hinged about a predetermined point on the upper surface of said flap, said sidewall rotating into the interior region of said flap when said flap is retracted.