1. Electronic circuit comprising at least one electronic component (6), a substrate (5), constituted by a flexible insulating material, on a first face of this substrate (5) an adhesive layer and a conductive layer including a plurality of tracks (4) are applied, said component (6) including at least two connection areas (7), at least one of these connection areas (7) being electrically linked to the conductive layer by a conductive bridge, characterized in that the substrate includes at least one sensibly rectangular strip (2, 3) made by incisions in the substrate (5) on three sides, the last side being attached to said substrate (5), and in that the bridge is formed by a conductive segment (1) delimited in the conductive layer only, said segment (1), free from any adhesive substance, traverses the substrate (5) through one of said strip (2, 3) incisions of and links the connection area (7).
2. Electronic circuit according to claim 1, characterized in that the substrate (5) includes a second face with a second adhesive layer and a second conductive layer, and in that said bridge is formed by a conductive segment (1) delimited in the second conductive layer only, said segment (1), free from any adhesive substance, traverses the substrate (5) by one of said strip (2, 3) incisions and links the connection area (7) andor the first conductive layer.
3. Electronic circuit according to claims 1 or 2, characterized in that a plurality of bridges formed by track segments (1) traverse the substrate (5) through a same incision.
4. Electronic circuit according to claim 1, characterized in that at least one bridge formed by a track segments (1) traverses the substrate (5) as many times as it is necessary to cross tracks (4) belonging to the conductive layer in order to reach the connection area (7).
5. Chip card or electronic label characterized in that it includes an electronic circuit according to claim 1.
6. Method for manufacturing an electronic circuit comprising a substrate (5), constituted by a flexible insulating material, at least one adhesive layer and a conductive layer including a plurality of tracks (4) and an electronic component (6), characterized in that the execution of a bridge between a zone of the conductive layer and a target connection area (7), includes the following steps:
prolonging a track in the conductive layer to constitute a conductive segment (1),
cutting in the substrate (5) a sensibly rectangular strip (2, 3), one of its sides being attached to the substrate (5),
temporarily freeing an opening by pressing the strip (2, 3), said strip (2, 3) curving along the side attached to the substrate (5),
passing the conductive segment (1) through said opening,
folding the conductive segment (1) against the opposite face of the substrate (5),
closing the opening after the passage of the conductive segment (1) by straightening the strip (2, 3) towards its initial position at the surface level of the substrate (5),
connecting the conductive segment (1) to the target connection area (7).
7. Method according to claim 6, characterized in that the target connection area is placed on the conductive layer, and in that the conductive segment (1) returns to said conductive layer by a second substrate passage by means of a supplementary strip (2, 3), said conductive segment (1) then being fixed to the substrate (5) by activating the glue originating from the adhesive layer.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. An aircraft brush seal comprising:
a first brush seal member; and
a second brush seal member comprising a channel that receives a plurality of interwoven brush fibers, wherein the channel is tapered in a radial direction.
2. The aircraft brush seal of claim 1, wherein the interwoven brush fibers are coupled to the first brush seal member.
3. The aircraft brush seal of claim 1, wherein the interwoven brush fibers extend into the second brush seal member.
4. The aircraft brush seal of claim 1, wherein the interwoven brush fibers do not couple to the second brush seal member.
5. The aircraft brush seal of claim 1, wherein the interwoven brush fibers form an air seal.
6. The aircraft brush seal of claim 1, wherein the brush fibers form a seal between a first air compartment and a second air compartment.
7. An aircraft brush seal comprising:
a first brush seal member; and
a second brush seal member comprising a channel that receives a plurality of brush fibers, wherein the second brush seal member comprises a tapered portion tapered in a radial direction and is configured to compact the brush fibers as the brush fibers extend into the channel.
8. The aircraft brush seal of claim 7, wherein the brush fibers are interwoven.
9. The aircraft brush seal of claim 7, wherein the brush fibers are coupled to the first brush seal member.
10. The aircraft brush seal of claim 7, wherein the brush fibers extend into the second brush seal member.
11. The aircraft brush seal of claim 7, wherein the brush fibers extend into a tapered portion of the second brush seal member.
12. The aircraft brush seal of claim 7, wherein the brush fibers do not couple to the second brush seal member.
13. The aircraft brush seal of claim 7, wherein the brush fibers form an air seal.
14. The aircraft brush seal of claim 7, wherein the brush fibers form a seal between a first air compartment and a second air compartment.
15. An aircraft brush seal comprising:
a first brush seal member comprising a first channel that receives a plurality of brush fibers;
a second brush seal member comprising a second channel that receives the plurality of brush fibers; and
a central shaft about which the plurality of brush fibers are wrapped.
16. The aircraft brush seal of claim 15, wherein the plurality of brush fibers wrap about the central shaft to intersect at a junction.
17. The aircraft brush seal of claim 15, wherein the plurality of brush fibers are held between the first brush seal member and the second brush seal member by a spring force of the plurality of brush fibers.
18. The aircraft brush seal of claim 15, wherein the plurality of brush fibers do not couple to the first channel.
19. The aircraft brush seal of claim 15, wherein the plurality of brush fibers do not couple to the second channel.
20. The aircraft brush seal of claim 15, wherein the plurality of brush fibers form a seal between a first air compartment and a secondary air compartment.