초록 ▼

An electrical resistance heating element of the sort suitable for use in de-icing an aircraft surface includes a foil patterned with a plurality of holes. The holes are in a first patterned region that extends in a first direction from a first end to an opposite second end. The holes define multiple

An electrical resistance heating element of the sort suitable for use in de-icing an aircraft surface includes a foil patterned with a plurality of holes. The holes are in a first patterned region that extends in a first direction from a first end to an opposite second end. The holes define multiple electrical paths between the two ends. The holes, which may vary in size, are configured and dimensioned such that the multiple electrical paths in areas away from lateral edges of said first patterned region are all non-parallel to the first direction. In other words, the electrical paths do not follow a straight line from the first and second ends, but rather must wend their way around the overlapping holes.

대표청구항 ▼

What is claimed is: 1. An aircraft electrothermal deicer heating element comprising: a foil sheet having a first patterned region extending in a first direction from a first portion to a second portion, the first patterned region being provided with a plurality of holes defining multiple electrical

What is claimed is: 1. An aircraft electrothermal deicer heating element comprising: a foil sheet having a first patterned region extending in a first direction from a first portion to a second portion, the first patterned region being provided with a plurality of holes defining multiple electrical paths extending from the first portion to the second portion, wherein: the holes overlap one another such that the first patterned region is devoid of continuous sections of foil material that: (a) extend in straight lines between the first and second portions, and (b) are parallel to said first direction; and the holes overlap one another such that the first patterned region is devoid of continuous sections of foil material that: (a) extend in straight lines between opposing lateral edges connecting the first and second portions, and (b) are perpendicular to said first direction. 2. An aircraft electrothermal deicer heating element comprising: a foil sheet having a first patterned region extending in a first direction from a first end to an opposite second end, the first patterned region being provided with a plurality of holes defining multiple electrical paths extending from the first end to the second end; wherein: the holes are configured and dimensioned such that said multiple electrical paths in areas away from lateral edges of said first patterned region are all non-parallel to said first direction; the holes in the first patterned region have more than one size; and the cross-sectional width of portions of the foil sheet between adjacent holes change along the first direction. 3. The aircraft electrothermal deicer heating element according to claim 2, wherein hole size in the first patterned region varies monotonically along said first direction. 4. The aircraft electrothermal deicer heating element according to claim 3, wherein hole size in the first patterned region increases along said first direction. 5. The aircraft electrothermal deicer heating element according to claim 1, wherein all holes in said first patterned region have a same shape. 6. The aircraft electrothermal deicer heating element according to claim 1, wherein each of said plurality of holes has a rectangular shape with rounded corners. 7. The aircraft electrothermal deicer heating element according to claim 1, wherein each of said plurality of holes has a circular shape. 8. The aircraft electrothermal deicer heating element according to claim 1, wherein each of said plurality of holes has a diamond shape with rounded corners. 9. The aircraft electrothermal deicer heating element according to claim 1, wherein each of said plurality of holes has a keyhole shape with rounded ends. 10. The aircraft electrothermal deicer heating element according to claim 9, wherein the holes with a keyhole-shape have a long axis that is perpendicular to said first direction. 11. The aircraft electrothermal deicer heating element according to claim 2, wherein breakage of one of said multiple electrical paths by foreign object damage or fatigue will result in only a minimal degradation to heating element functionality. 12. The aircraft electrothermal deicer heating element according to claim 1, wherein hole size in the first patterned region varies monotonically along said first direction. 13. The aircraft electrothermal deicer heating element according to claim 1, wherein the holes are configured and dimensioned such that said multiple electrical paths in areas away from lateral edges of said first patterned region are non-parallel to said first direction. 14. An aircraft electrothermal deicer heating element comprising: a foil sheet having a first patterned region extending in a first direction from a first portion that is connected to a power input to a second portion, the first patterned region being provided with a plurality of holes defining multiple electrical paths extending from the first portion to the second portion; wherein: the holes are configured and dimensioned such that said multiple electrical paths in areas away from lateral edges of said first patterned region are all non-parallel to said first direction; and the holes overlap one another such that the first patterned region is devoid of continuous sections of foil material that: (a) extend in straight lines between opposing lateral edges connecting the first and second portions, and (b) are perpendicular to said first direction. 15. The aircraft electrothermal deicer heating element according to claim 2, wherein: the cross-sectional width of portions of the foil sheet between adjacent holes change monotonically along the first direction. 16. The aircraft electrothermal deicer heating element according to claim 15, wherein: the cross-sectional width of portions of the foil sheet between adjacent holes monotonically decrease along the first direction. 17. The aircraft electrothermal deicer heating element according to claim 1, wherein: the cross-sectional width of portions of the foil sheet between adjacent holes change monotonically along the first direction. 18. The aircraft electrothermal deicer heating element according to claim 17, wherein: the cross-sectional width of portions of the foil sheet between adjacent holes monotonically decrease along the first direction. 19. The aircraft electrothermal deicer heating element according to claim 14, wherein: the cross-sectional width of portions of the foil sheet between adjacent holes change monotonically along the first direction. 20. The aircraft electrothermal deicer heating element according to claim 19, wherein: the cross-sectional width of portions of the foil sheet between adjacent holes monotonically decrease along the first direction.