ELECTRICAL INTERCONNECT ARRANGEMENTS

Abstract

An electrical interconnect arrangement for coupling a contactor with a bus bar includes a post, a bus bar connected electrically to the post, and a joint coupling the bus bar to the post. The joint has two or more interfaces defined between the post and the bus bar to reduce resistive heat generation within the electrical interconnect arrangement.

Claims

1. An electrical interconnect arrangement, comprising: a post; a bus bar electrically connected to the post; and a joint coupling the bus bar to the post, wherein the joint has a plurality of interfaces defined between the post and the bus bar to limit resistive heat generation in the joint.

2. An electrical interconnect arrangement as recited in claim 1, wherein the joint is an interdigitated joint.

3. An electrical interconnect arrangement as recited in claim 1, wherein the joint includes at least three electrically conductive interfaces defined between the post and the bus bar.

4. An electrical interconnect arrangement as recited in claim 1, wherein the joint includes five electrically conductive interfaces defined between the post and the bus bar.

5. An electrical interconnect arrangement as recited in claim 1, wherein the bus bar has a planar body defining a bus bar axis, wherein the post defines a post axis, and wherein the bus bar axis is angled relative the post axis at an oblique or 90-degree angle.

6. An electrical interconnect arrangement as recited in claim 1, wherein the bus bar has first and second terminations, the first termination and the second termination defining a gap therebetween.

7. An electrical interconnect arrangement as recited in claim 6, wherein the post has a prong, wherein the prong is seated in the gap and is bounded by a pair of electrically conductive interfaces.

8. An electrical interconnect arrangement as recited in claim 6, wherein the post has a prong, wherein the prong is seated against the first termination and bounded by a single electrically conductive interface.

9. An electrical interconnect arrangement as recited in claim 6, further including a void bounded by the bus bar and the prong.

10. An electrical interconnect arrangement as recited in claim 1, wherein the bus bar has a first termination, a second termination adjacent to the first termination, and a third termination adjacent to the second termination and on a side of the second termination opposite the first termination.

11. An electrical interconnect arrangement as recited in claim 10, wherein the first termination and the second termination define a gap therebetween, wherein the post has a prong seated in the gap and bounded by a pair of electrically conductive interfaces.

12. An electrical interface arrangement as recited in claim 10, wherein the second termination and the third termination define a gap therebetween, wherein the post has a prong seated in the gap and bounded by a pair of electrically conductive interfaces.

13. An electrical interconnect arrangement as recited in claim 10, wherein the post includes a prong, the prong being seated against the first termination and bounded by a single electrically conductive interface.

14. An electrical interconnect arrangement as recited in claim 1, wherein the joint includes a fastener received within the bus bar and the post.

15. An electrical interconnect arrangement as recited in claim 1, wherein the bus bar has a plurality of terminations, wherein the post has a plurality of prongs, and wherein the plurality of terminations are interleaved with the plurality of prongs.

16. An electrical interconnect arrangement as recited in claim 1, wherein the post is a single piece of material.

17. An electrical interconnect arrangement as recited in claim 1, wherein the bus bar is a single piece of material.

18. An interconnect arrangement for a power distribution panel, comprising: a contactor with a lead; a post with a plurality of prongs electrically connected to the lead; a bus bar with a plurality of terminations electrically connected to the post; and an interdigitated joint coupling the bus bar to the post, wherein the plurality of prongs of the post are interleaved with the plurality of terminations of the bus bar such that at least three electrically conductive interfaces are defined between the bus bar and the post.

19. A method of electrically connecting a bus bar to a post, comprising: interleaving a plurality of terminations of the bus bar with a plurality of prongs of the lead post; and compressing the interleaved plurality of terminations and the plurality of prongs.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0012] So that those skilled in the art to which the subject disclosure appertains will readily understand how to make and use the devices and methods of the subject disclosure without undue experimentation, embodiments thereof will be described in detail herein below with reference to certain figures, wherein:

[0013] FIG. 1 is a schematic view of an exemplary embodiment of an aircraft electrical system, showing an electrical interconnect arrangement connecting a power source to a power-consuming device through a contactor;

[0014] FIG. 2 is a plan view of the power distribution panel of FIG. 1, showing the contactor connected to a bus bar by the electrical interconnect arrangement;

[0015] FIG. 3 is a schematic side elevation view of the electrical interconnect arrangement of FIG. 1, showing the electrical interconnect arrangement connecting the bus bar to the contactor;

[0016] FIGS. 4A and 4B is are side elevation views of the bus bar and electrical interconnect arrangement of FIG. 1, respectively showing the bus bar and an interleaved joint including the bus bar according to a first embodiment;

[0017] FIGS. 5A and 5B is are side elevation views of another embodiment bus bar and electrical interconnect arrangement, respectively showing a bus bar an interleaved joint according to a second embodiment; and

[0018] FIG. 6 is joint loss table, showing joint loss for the electrical interconnect arrangements of FIGS. 4A-4B and FIGS. 5A-5B compared to an interconnect having a single interface.

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0019] Reference will now be made to the drawings wherein like reference numerals identify similar structural features or aspects of the subject disclosure. For purposes of explanation and illustration, and not limitation, a partial view of an exemplary embodiment of an electrical interconnect arrangement in accordance with the disclosure is shown in FIG. 1 and is designated generally by reference character 100. Other embodiments of electrical interconnect arrangements are provided in FIGS. 2-6, as will be described. The electrical interconnect arrangements can be used to connect contactors and bus bars in primary power panels and/or high-voltage direct current (HVDC) power panels for aircraft electrical systems, though the present disclosure is not limited to power panels or to aircraft electrical systems in general.

[0020] With reference to FIG. 1, an aircraft 10 is shown. Aircraft 10 includes a power distribution system 12 with a power distribution panel 14, a primary power bus 16, an HVDC power bus 18, and one or more power-consuming device 20. A main engine 24 is operatively connected to a main generator 22. Main generator 22 is connected to primary power bus 16 and is configured to receive mechanical rotation from main engine 24, convert the rotation into electrical power, and apply the power to primary power bus 16. A direct current power source, such as battery 26, is connected to a HVDC power bus 18 and is configured to apply HVDC power to HVDC power bus 18. One or more of HVDC power bus 18 and primary power bus 16 are connected to a contactor 50 disposed in power distribution panel 14, contactor 50 begin connected to one or more power-consuming device 20 through electrical interconnect arrangement 100.

[0021] With reference to FIG. 2, power distribution panel 14 is shown. Power distribution panel 14 includes contactor 50, a source bus bar 102, and a supply bus bar 104. Source bus bar 102 is electrically connected to a primary power bus 16 (shown in FIG. 1) (shown in FIG. 1). Supply bus bar 104 is connected to one or more power-consuming device 20 (shown in FIG. 1). Electrical interconnect arrangement 100 connects contactor 50 with source bus bar 102 and provides electrical connectivity between source bus bar 102 and contactor 50. Contactor 50 may include a mechanical or solid-state switch device having an on state and an off state, provides electrical communication between source bus bar 102 and supply bus bar 104 when in the on state, and electrically separates source bus bar 102 and supply bus bar 104 when in the off state. Although described herein as connecting contactor 50 with source bus bar 102, it is to be understood and appreciated that an electrical interconnect arrangement as described herein can also connect contactor 50 with supply bus bar 104. Although illustrated and herein an interconnect arrangement for a primary power bus, it is to be appreciated that interconnect arrangements such as HVDC power bus will also benefit from the present disclosure.

[0022] With reference to FIG. 3, electrical interconnect arrangement 100 is shown. Electrical contactor 50 includes a source lead 52. Source lead 52 is connected to a post 106. Post 106 is connected to source bus bar 102 by a joint 108, may be an interdigitated joint having interleaved connected conductive elements. Either or both of bus bar 102 and post 106 can be a single piece of material fabricated using an additive manufacturing technique. Fabricating either or both of bus bar 102 and post 106 as a single piece of material reduces the number of interfaces within the respective structure, reducing resistance and associated resistive heating of the structure.

[0023] Post 106 defines a post axis P and source bus bar 102 defines a bus bar axis B. Bus bar axis B is angled with respect to post axis P and has an angle 110 therebetween that is defined by electrical interconnect arrangement 100. In the illustrated exemplary embodiment angle 110 is about 90-degrees. It is contemplated that angle 110 can be a 180-degree angle or an oblique angle, as suitable for an intended application. Although the exemplary electrical interconnect arrangement 100 is shown connecting contactor 50 with source bus bar 102, it is to be understood and appreciated that a similar interconnect arrangement can connect a supply post with supply bus bar 104. Post 106 structurally supports contactor 50, and may be fixed within power distribution panel 14 (shown in FIG. 2) to an electrically insulative panel element, such as a backplane 32 by way on non-limiting example.

[0024] With reference to FIGS. 4A and 4B, electrical interconnect arrangement 100 is shown. Referring to FIG. 4A, source bus bar 102 is shown. Source bus bar 102 has a planar, plate-like body 114 extending between a first end 116 and a second end 118. Plate-like body 114 includes an electrically conductive material such as aluminum, copper, or alloys thereof, and defines a bus bar axis B spanning first end 116 and second end 118. First end 116 of source bus bar 102 has a split end with two or more terminations. In this respect first end 116 has a first termination 124 and a second termination 126 there define between one another a gap 122. Gap 122 is bounded by a surface of first termination 124 that faces a surface of second termination 126, gap 122 being configured and adapted to interleave with a portion of post 106.

[0025] Referring to FIG. 4B, joint 108 is shown. Joint 108 includes an interdigitated arraignment of bus bar terminations interleaved with post prongs. In the illustrated exemplary embodiment post 106 has a first prong 132 and a second prong 134, second prong 134 being spaced apart from first prong 132. First prong 132 overlays (relative to the top of FIG. 4A) first termination 124 of source bus bar 102 in joint 108 and is electrically connected with first termination 124 through a first interface 110A. First interface 110 A is defined by a lower surface of first prong 132 and an upper surface of first termination 124.

[0026] Second prong 134 is seated within gap 122 between first termination 124 and second termination 126 such that second prong 134 underlays first termination 124 and overlays second termination 126. Second prong 134 is electrically connected with first termination 124 through a second interface 110B defined by an upper surface of second prong 134 and a lower surface of first termination 124. Second prong 134 is also electrically connected to second termination 126 of source bus bar 102 by a third interface 110C defined by a lower surface of second prong 134 and an upper surface of second termination 126. First interface 110A, second interface 110B, and third interface 110C have substantially the same electrical resistance. A fastener 140 is received within joint 108, compressively seating source bus bar 102 against post 106. In the illustrated exemplary embodiment, fastener 140 includes a bolt received within first prong 132, first termination 124, second prong 134, and second termination 126 compressively engaging each of the terminations and prongs with one another. In the illustrated exemplary embodiment joint 106 defines a void 128. Void 128 is bounded by one or termination of source bus bar 102 and prong of post 106, void 128 providing additional area for heat transfer from coolant passively or actively flowing through joint 106.

[0027] As will be appreciated by those of skill in the art, current I.sub.102 entering joint 108 is substantially equivalent to current I.sub.106 exiting joint 106. As will be appreciated by those of skill in the art in view of the present disclosure, current I.sub.102 splits in a first termination current flow I.sub.124 and a second termination current flow I.sub.126 that are about one-half of current flow I.sub.102. Current flow I.sub.124 further divides into a first interface current flow I.sub.110A, which traverses first interface 110A, and second interface current flow I.sub.110B, which traverses second interface 110B—each of which are about one-quarter of current flow I.sub.202. Substantially all of current flow I.sub.126, i.e. about one-half of current flow I.sub.202, traverses third interface 110C.

[0028] Since each of first interface 110A, second interface 110B, and third interface 110C have substantially equivalent resistance R, joint loss (shown in FIG. 6) is about 0.375 of the joint loss in a joint having a single interface with equivalent resistance. This reduces resistive heat generation in joint 108 in comparison with a single interface joint having the same electrical resistance of the interfaces of joint 108, reducing joint loss by about 62.5%, and commensurately reducing resistive heating on the joint between source bus bar 102 and post 106 in comparison to a single interface joint.

[0029] Referring to FIGS. 5A and 5B, an electrical interconnect arrangement 200 is shown. Electrical interconnect arrangement 200 is similar to electrical interconnect arrangement 100 (shown in FIG. 4B), and additionally includes a joint 208. Joint 208 includes three terminations of a source bus bar 202 and three prongs of a post 206, has two addition electrical interfaces defined between source bus bar 202 and post 206, and has still further joint loss that electrical interconnect arrangement 100.

[0030] As shown in FIG. 5A, source bus bar 202 is shown. Source bus bar 202 has a plate-like, planar body 214 defining a bus bar axis B and includes a first termination 224, a second termination 226, and a third termination 228. Second termination 226 extends along bus bar axis B. First termination 224 is disposed on a side of bus bar axis B opposite third termination 228, and a gap 222A is defined between first termination 224 and second termination 226. Third termination 228 is disposed on a side of second termination 226 opposite first termination 224, and gap 222B is defined between third termination 228 and second termination 226.

[0031] Referring to FIG. 5B, joint 208 is shown. Joint 208 includes first termination 224, second termination 226, and third termination 228. Joint 208 also includes a first pong 232, a second prong 234, and a third prong 236 of post 206. First prong 232 overlays first termination 224 and is connected electrically thereto through a first interface 110A. Second prong 234 underlays first termination 224, is seated within first gap 222A, is electrically connected to first termination 224 through a second interface 210B, and is also electrically connected to second termination 226 through a third interface 210C. Third prong 236 underlays second termination 226, is seated within second gap 222B, is electrically connected to second termination 226 through a fourth interface 210D, and is also electrically connected to third termination 228 through a fifth interface 210E. As with electrical interconnect arrangement 100 (shown in FIG. 4B), each interface has substantially the same electrical resistance. In the illustrated exemplary embodiment, a fastener 240 is received within joint 208, compressively seating the terminations of source bus bar 202 against the prongs of post 206.

[0032] Current I.sub.202 entering joint 208 is substantially equivalent to current I.sub.206 exiting joint 206. Current I.sub.202 divides into three current flows as it traverses joint 208, each termination of source bus bar 202 carrying about one-third of current flow I.sub.202. In this respect first termination 224 carries a first termination current flow I.sub.224, second termination 226 carries a second termination current flow I.sub.226, and third termination 228 carries a third termination current flow I.sub.226.

[0033] First termination current flow I.sub.224 divides into a first interface current flow I.sub.210A that is about one-sixth of current flow I.sub.202, which traverses first interface 210A, and second interface current flow I.sub.210B, also about one-sixth of current flow I.sub.202 and which traverses second interface 210B. Similarly, second termination current flow I.sub.226 divides into a third interface current flow I.sub.210C that is about one-sixth of current flow I.sub.202 and which traverses third interface 210C, and fourth interface current flow I.sub.210C, which is also about one-sixth of current flow I.sub.202 and which traverses fourth interface 210D. Third termination current flow I.sub.228 traverses fifth interface 210E in its entirety.

[0034] Since each of the five interfaces of joint 208, i.e. first interface 210A, second interface 210B, third interface 210C, fourth interface 210D, and fifth interface 210E, have substantially equivalent resistance R, joint loss (shown in FIG. 6) is about 0.222 times the joint loss in a joint having a single interface with equivalent resistance. This reduces resistive heat generation in joint 208 in comparison with a single interface joint having the same electrical resistance of the interfaces of joint 108, reducing joint loss by about 77.7%, and commensurately reducing resistive heating on the joint between source bus bar 202 and post 206 in comparison to a single interface joint.

[0035] Referring the FIG. 6, a table of joint loss from resistive heating is shown. As will be appreciated by those of skill in the art, ‘joint loss’ generally describes the tendency of conductive components coupled at a joint to generate heat while an electrical current traverses the joint. The energy loss from joint loss each second, or power, increases with the square of the current flow and in proportion. For single interface interconnect, joint loss for current I across a single interface having resistance R is according to Equation 1.

Loss=I.sup.2*R  (Equation 1)

[0036] Since I.sub.110A and I.sub.110B are about one-quarter I1.sub.02, and I.sub.110C is about one-half I.sub.202, joint loss is according to is according to Equation 2 (below); joint loss for second interface 110B is according to Equation 3 (below); and joint loss for the third interface 110C is according to Equation 4 (below).

First Interface Loss=I.sub.110A.sup.2*(R/16)  (Equation 2)

Second Interface Loss=I.sub.110B.sup.2*(R/16)  (Equation 3)

Third Interface Loss=I.sub.110C.sup.2*(R/4)  (Equation 4)

Since total joint loss for electrical interconnect arrangement 100 is the sum of the joint loss across each interface, i.e. across first interface 110A, second interface 110B, and third interface 110C, total joint loss for electrical interconnect arrangement 100 is according to Equation 5,

Total Loss−3*I.sub.102.sup.2*(R/8),  (Equation 5)

which is a joint loss reduction of about 62.5% compared to an electrical interconnect having a single interface.

[0037] With respect to electrical interconnect arrangement 200 (shown in FIG. 5B) joint loss is further reduced. Since I.sub.210A, I.sub.210B, I.sub.210C, and I.sub.210D are about one-quarter I.sub.202, and I.sub.210E is about one-third of I.sub.202, joint loss in first interface 210A is according to Equation 6 (below); joint loss for the second interface 210B is according to Equation 7 (below); joint loss for the third interface 210C is according to Equation 8 (below); joint loss for the fourth interface 210D is according to Equation 9 (below); and joint loss for the fifth interface 210E is according to Equation 10 (below).

First Interface Loss=I.sub.210A.sup.2*(R/36)  (Equation 6)

Second Interface Loss=I.sub.210B.sup.2*(R/36)  (Equation 7)

Third Interface Loss=I.sub.210C.sup.2*(R/36)  (Equation 8)

Fourth Interface Loss=I.sub.210D.sup.2*(R/36)  (Equation 9)

Fifth Interface Loss=I.sub.210E.sup.2*(R/9)  (Equation 10)

Summing the joint losses for the five interfaces, total joint loss for electrical interconnect arrangement 200 is according to Equation 11,

Total Loss−2*I.sub.202.sup.2*(R/9),  (Equation 11)

indicating that electrical interconnect arrangement 200 has a joint loss that is about 77.7% of joint loss in an electrical interconnect having a single interface.

[0038] A method of electrically connecting a bus bar, e.g., source bus bar 102 (shown in FIG. 4A), to a post, e.g., post 106 (shown in FIG. 4B) includes interleaving two or more terminations, e.g., first termination 124 and second termination 126 (shown in FIG. 4B) of the bus bar with two or more prongs, e.g., first prong 132 and second prong 134 (shown in FIG. 4B) of the lead post and compressing the interleaved terminations and prongs. Compressing the interleaved terminations and prongs can include seating a fastener, e.g., fastener 140 (shown in FIG. 4B), into a joint, e.g., joint 108 (shown in FIG. 4B) between the bus and the post formed by the interleaved terminations and prongs.

[0039] In embodiments described herein, bus bars include split ends. The split ends provide parallel terminations on either or both ends of the bus bars. In certain embodiments, the bus bars have two or more terminations on an end that provide reduced joint losses. In accordance with certain embodiments, the split ends provide additional contact area within the joint, thereby enabling improved heat transfer from the joint and into the bus bar.

[0040] The methods and systems of the present disclosure, as described above and shown in the drawings, provide for power distribution systems with superior properties including reduced contactor temperatures and/or contactor heat removal capability. While the apparatus and methods of the subject disclosure have been shown and described with reference to preferred embodiments, those skilled in the art will readily appreciate that changes and/or modifications may be made thereto without departing from the scope of the subject disclosure.