초록 ▼

A deicer pad for use on an aircraft wing wherein the deicer pad is constructed to have an intermediate portion and two spaced apart portions. The pad is a composite member of at least two plies of materials stitched along the intermediate portion to provide two spanwise passageways, and stitched in

A deicer pad for use on an aircraft wing wherein the deicer pad is constructed to have an intermediate portion and two spaced apart portions. The pad is a composite member of at least two plies of materials stitched along the intermediate portion to provide two spanwise passageways, and stitched in a zig-zag pattern along the spaced apart portions to form chordwise passageways. Alternate chordwise passageways communicate directly with the spanwise passageways while the remaining chordwise passageways communicate with the adjacent spanwise passageways around the stitching. The remaining chordwise passageways also communicate with the adjacent alternate chordwise passageways around the stitching which stitching forms the separation between alternate chordwise passageways.

대표청구항 ▼

1. A pneumatic deicer pad for a wing of an aircraft having a leading edge, an inboard end and an outboard end; said pad having an intermediate portion with a centerline overlying said leading edge and also having a pair of spaced apart portions located rearward of said centerline when positioned on

1. A pneumatic deicer pad for a wing of an aircraft having a leading edge, an inboard end and an outboard end; said pad having an intermediate portion with a centerline overlying said leading edge and also having a pair of spaced apart portions located rearward of said centerline when positioned on said wing to provide a pair of rearwardly disposed edges; said centerline of said deicer pad coincides with said leading edge of said wing; said spaced apart portions defining an upper portion and a lower portion; said deicer pad having an inner ply for attachment to said wing; an outer extensible elastic ply overlying said inner ply; said plies being stitched on said intermediate portion to define at least a pair of spanwise passageways; said plies being stitched together at said respective rearwardly disposed spaced apart portions to define two groups of passageways, with each group having a plurality of adjacent chordwise extending passageways in side by side relationship that all terminate adjacent one of said spanwise passageways; one of said groups of passageways located in said upper portion and the other of said groups of passageways located in said lower portion; certain ones of said chordwise passageways in each group communicate directly with adjacent ones of said spanwise passageways; the remaining ones of said chordwise passageways in each group communicate with said spanwise passageways around said stitching with the adjacent ends of said spanwise passageways; said certain ones of said chordwise passageways in each group also communicate with adjacent ones of said remaining ones of said chordwise passageways around adjacent stitching; means for communicating said passageways with a pressure source which is operative upon pressurization to elastically distend the portions of said outer ply by inflating said passageways; and all of said plies being covered with an air impervious layer to retain pressurized air within said deicer pad. 2. A pneumatic deicer pad for a wing of an aircraft as set forth in claim 1 wherein said stitching on said inner ply and said outer extensible ply on said rearwardly disposed spaced apart portions are of a zig-zag design to provide said chordwise passageways in side by side relationship. 3. A pneumatic deicer pad for a wing of an aircraft as set forth in claim 2 wherein said means for communicating said passageways with a pressure source includes a means for pulling a vacuum on said passageways. 4. A pneumatic deicer pad for a wing of an aircraft as set forth in claim 3 wherein said spanwise passageways are of greater cross-sectional dimension than said chordwise passageways. 5. A pneumatic deicer pad for a wing of an aircraft as set forth in claim 4 wherein said chordwise passageways in said lower portion of said pads are greater in length than said chordwise passageways in said upper portion of said pad. 6. A pneumatic deicer for a wing of an aircraft, said wing having a leading edge, an inboard end, and an outboard end; a deicer pad with an upper portion, a lower portion and an intermediate portion; said intermediate portion disposed along said leading edge of said wing; one end of said deicer pad having an inboard end at said inboard end of said wing and the other end of said pad being an outboard end extending outwardly toward said outboard end of said wing; said deicer pad having a pair of laterally spaced side edges interconnecting said inboard end with said outboard end of said deicer pad; said pad being a composite layer of resilient air impervious material; said pad being stitched along said spaced side edges; said pad being stitched at said intermediate portion to define a pair of longitudinally extending spanwise passageways located along said leading edge of said wing; said spanwise passageways sharing a common seam disposed along said longitudinal center line of said pad; each of said passageways having a side edge that is spaced to either side of said intermediate portion; said upper portion of said pad and said lower portion of said pad each having a continuous stitching seam that extends in a zig zag pattern from said inboard end of said pad to said outboard end of said pad to define a series of closely spaced chordwise passageways that extend to said spanwise passageway; certain ones of said chordwise passageway communicating directly with adjacent ones of said spanwise passageways; the remaining one of said chordwise passageways communicating with adjacent ones of said first mentioned chordwise passageways that communicate directly with said spanwise passageway and said remaining chordwise passageways also communicate with adjacent ones of said spanwise passageways around said stitching seams separating their connection to said adjacent chordwise and spanwise passageways; means connected to one of said passageways that communicates directly with said spanwise passageway to pressurize and exhaust air from said deicer pad to provide a deicing action for said wing; and said composite layers of air impervious material being covered with a resilient rubber air impervious material.