CN105109702A - Side cabinet - Google Patents
Side cabinet Download PDFInfo
- Publication number
- CN105109702A CN105109702A CN201510496360.XA CN201510496360A CN105109702A CN 105109702 A CN105109702 A CN 105109702A CN 201510496360 A CN201510496360 A CN 201510496360A CN 105109702 A CN105109702 A CN 105109702A
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- side cabinet
- bolt
- main body
- cable lead
- attaching parts
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Abstract
The invention discloses a side cabinet used for being installed in a storage bin of an aircraft. The side cabinet comprises a side cabinet body (2), a bottom installation piece (1), a cable channel (3) and a top installation piece (4). The bottom installation piece (1) is arranged between the side cabinet body (2) and a floor and used for connecting the side cabinet body (2) with the floor. One end of the cable channel (3) is connected with the upper end of the side cabinet body (2). The top installation piece (4) is arranged between the cable channel (3) and a sound insulation cabin ceiling and used for connecting the cable channel (3) with the sound insulation cabin ceiling. According to the side cabinet, the cable channel (3) is connected with the upper end of the side cabinet body (2) through a first connecting piece (21) and connected with the top installation piece (4) through a second connecting piece (5), the connecting manner is bolt connection, the installation structure is simple, and the requirements that a base frame of the side cabinet is fixedly connected with the floor of the storage bin of the aircraft, and a cable inside the side cabinet needs to penetrate the sound insulation cabin ceiling to be linked with the aircraft are met.
Description
Technical field
The present invention relates to air transport air-drop design field, particularly relate to a kind of side cabinet be arranged in aircraft cargo bay.
Background technology
Generally 4 communication cabinets are all designed with in the shipping cabin of existing aircraft, be respectively R1 communication cabinet, R2 communication cabinet, R4 (ESM) and R5 (ESM), wherein need between R1 communication cabinet and R2 communication cabinet SR1 side cabinet is installed, accordingly, need between R4 (ESM) and R5 (ESM) SR4 side cabinet is installed.For SR1/SR4 side cabinet, this side cabinet needs the assigned address being arranged on aircraft, and requires that side cabinet bedframe will be connected with aircraft cargo bay floor, and side cabinet inside cable will be cross-linked by cargo hold top ceiling and other cable of aircraft.
For this reason, in existing aircraft shipping cabin, should determine that designed SR1/SR4 side cabinet can be arranged on aircraft specified location more easily, to meet SR1/SR4 side cabinet operating needs aboard, promote Aircraft Survivability.
Summary of the invention
In order to solve the problem, the invention provides a kind of side cabinet, comprise side cabinet main body;
End fabricated section, is arranged between described side cabinet main body and floor, in order to connect described side cabinet main body and described floor;
Cable lead-through, the upper end of its one end connection side cabinet main body, the upper end of described side cabinet main body is described side cabinet main body one end away from fabricated section of the described end;
Top fabricated section, is arranged between described cable lead-through and soundproofed cabin top ceiling, in order to connect described cable lead-through and described soundproofed cabin top ceiling,
Wherein, described cable lead-through is by the upper end of the first attaching parts connection side cabinet main body, and described cable lead-through connects described top fabricated section by the second attaching parts, and the upper end of described top fabricated section and described side cabinet main body lays respectively at the two ends of described cable lead-through.
Preferably, Gui WeiSR1 side, described side cabinet, it is arranged between two communication cabinets; Or Gui WeiSR4 side, described side cabinet, it is arranged between two ESM racks.
In such scheme preferably, open hole in the middle of the fabricated section of described top, be connected with described first attaching parts bolt, and be connected with described soundproofed cabin top ceiling bolt.
In such scheme preferably, open hole in the middle of described first attaching parts, be connected with described top fabricated section bolt, and be connected with described cable lead-through bolt.
In such scheme preferably, have the through hole of energising cable in the middle of described cable lead-through, be connected with described second attaching parts bolt, and be connected with described first attaching parts bolt.
, in described second attaching parts, have through hole in such scheme preferably, be connected with described cable lead-through bolt, and be connected with the upper terminal bolt of described side cabinet main body.
The side cabinet that the present invention proposes is installed as the assigned address newly-designed SR1/SR4 side cabinet being arranged on aircraft, meets side cabinet bedframe and aircraft cargo bay floor is fixedly linked simultaneously, side cabinet inside cable will by soundproofed cabin top ceiling and aircraft crosslinked.This mount scheme mentality of designing is ingenious, simple and practical, and corresponding side cabinet is easy to process, produces assembly technology and realizes easily, meeting SR1/SR4 side cabinet operating needs aboard, promote Aircraft Survivability.
Accompanying drawing explanation
Fig. 1 is side cabinet schematic diagram according to an embodiment of the invention.
Fig. 2 is the second attaching parts scheme of installation embodiment illustrated in fig. 1.
Fig. 3 is the first attaching parts scheme of installation embodiment illustrated in fig. 1.
Fig. 4 is end fabricated section scheme of installation embodiment illustrated in fig. 1.
Fig. 5 is side cabinet position relationship schematic diagram embodiment illustrated in fig. 1.
Wherein, 1 is end fabricated section, 2 is side cabinet, 3 is cable lead-through, 4 is top fabricated section, 5 is the second attaching parts, 6 is the first bolt, 7 is the first pad, 8 is the first nut, 9 is the second bolt, 10 is the second pad, 11 is the second nut, 12 is the 3rd bolt, 13 is the 3rd pad, 14 is the 3rd nut, 15 is the 4th bolt, 16 is the 4th pad, 17 is the 4th nut, 18 is the 5th bolt, 19 is the 5th pad, 20 is the 5th nut, 21 is the first attaching parts, 22 is R1 communication cabinet, 23 is R2 communication cabinet, 24 is R4 (ESM), 25 is R5 (ESM).
Detailed description of the invention
For making object of the invention process, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, same or similar label represents same or similar element or has element that is identical or similar functions from start to finish.Described embodiment is the present invention's part embodiment, instead of whole embodiments.Be exemplary below by the embodiment be described with reference to the drawings, be intended to for explaining the present invention, and can not limitation of the present invention be interpreted as.Based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.Below in conjunction with accompanying drawing, embodiments of the invention are described in detail.
In describing the invention; it will be appreciated that; term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear", "left", "right", " vertically ", " level ", " top ", " end " " interior ", " outward " etc. instruction orientation or position relationship be based on orientation shown in the drawings or position relationship; be only the present invention for convenience of description and simplified characterization; instead of instruction or imply indication device or element must have specific orientation, with specific azimuth configuration and operation, therefore can not be interpreted as limiting the scope of the invention.
The side cabinet that the present embodiment provides as shown in Figure 1, mainly comprises side cabinet main body 2;
End fabricated section 1, is arranged between described side cabinet main body 2 and floor, in order to connect described side cabinet main body 2 and described floor; At the bottom of two, fabricated section 1 is U-shaped material, and lower surface and aircraft cargo bay floor are fitted, and are fixedly linked by attaching parts and cargo deck, and upper surface and side cabinet bedframe are fixedly linked.Concrete structure, with reference to figure 4, two U-shaped side plates of end fabricated section 1 has bolt hole, and 18 is the 5th bolt, and 19 is the 5th pad, and 20 is the 5th nut, is bolted, and side cabinet main body 2 is fixed on floor.
The side cabinet of the present embodiment also comprises cable lead-through 3, the upper end of its one end connection side cabinet main body 2, and the upper end of described side cabinet main body 2 is described side cabinet main body 2 one end away from fabricated section of the described end 1; And,
Top fabricated section 4, is arranged between described cable lead-through 3 and soundproofed cabin top ceiling, in order to connect described cable lead-through 3 and described soundproofed cabin top ceiling,
Wherein, described cable lead-through 3 is by the upper end of the first attaching parts 21 connection side cabinet main body 2, as shown in Figure 2, described cable lead-through 3 connects described top fabricated section 4 by the second attaching parts 5, as shown in Figure 3, described top fabricated section 4 and the upper end of described side cabinet main body 2 lay respectively at the two ends of described cable lead-through 3.
It should be noted that, side Gui WeiSR1 side cabinet described in the present embodiment, it is arranged between two communication cabinets; Or Gui WeiSR4 side, described side cabinet, it is arranged between two ESM racks.Shown in figure 5, wherein, 22 is R1 communication cabinet, 23 is R2 communication cabinet, 24 is R4 (ESM), and 25 is R5 (ESM), and is SR1 side cabinet between R1 communication cabinet 22 and R2 communication cabinet 23, in like manner, between R4 (ESM) 24 and R4 (ESM) 25, be SR4 side cabinet.General, in aircraft cargo bay, existing SR1 side cabinet, has again SR4 side cabinet, and therefore in the present embodiment, first bolt of the following stated, the first nut, until the quantity such as the 5th bolt, the 5th nut is determined on a case-by-case basis, repeat no more bolt quantity afterwards.
In the present embodiment, it should be noted that, for ensureing that cable lead-through is smooth, described top fabricated section 4, first attaching parts 21, second attaching parts 5 and cable lead-through are all that hole is opened in centre, and all annexations are bolt and connect.Specifically, first with reference to figure 2, top fabricated section 4 is connected with described first attaching parts 21 bolt, and be connected with described soundproofed cabin top ceiling bolt, in the figure, 6 is the first bolt, 7 is the first pad, 8 be first nut will, this cover bolt in order to the upper end interface of the second attaching parts 5 and soundproofed cabin top ceiling are fixedly linked, in the figure, 9 is the second bolt, 10 is the second pad, and 11 is the second nut, and this cover bolt is in order to be connected the side plate of the side of the second attaching parts 5 with cable lead-through 3 upper end.
Similar to the above, with reference to figure 3, wherein, 12 is the 3rd bolt, and 13 is the 3rd pad, and 14 is the 3rd nut.This cover bolt is in order to be fixedly connected on the first attaching parts 21 by the lower end side of cable lead-through 3; 15 is the 4th bolt, and 16 is the 4th pad, and 17 is the 4th nut, and the first attaching parts 21 lower end horizontal positioned, the first attaching parts 21 is fixedly connected on the upper end of side cabinet main body 2 by this cover bolt assembly (15,16,17).
The side cabinet that the present invention proposes is installed as the assigned address newly-designed SR1/SR4 side cabinet being arranged on aircraft, meets side cabinet bedframe and aircraft cargo bay floor is fixedly linked simultaneously, side cabinet inside cable will by soundproofed cabin top ceiling and aircraft crosslinked.This mount scheme mentality of designing is ingenious, simple and practical, produces assembly technology and realizes easily, meeting SR1/SR4 side cabinet operating needs aboard, promote Aircraft Survivability.
Finally it is to be noted: above embodiment only in order to technical scheme of the present invention to be described, is not intended to limit.Although with reference to previous embodiment to invention has been detailed description, those of ordinary skill in the art is to be understood that: it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature; And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of various embodiments of the present invention technical scheme.
Claims (6)
1. a side cabinet, is characterized in that: comprise side cabinet main body (2);
End fabricated section (1), is arranged between described side cabinet main body (2) and floor, in order to connect described side cabinet main body (2) and described floor;
Cable lead-through (3), the upper end of its one end connection side cabinet main body (2), the upper end of described side cabinet main body (2) is described side cabinet main body (2) one end away from fabricated section of the described end (1);
Top fabricated section (4), is arranged between described cable lead-through (3) and soundproofed cabin top ceiling, in order to connect described cable lead-through (3) and described soundproofed cabin top ceiling,
Wherein, described cable lead-through (3) is by the upper end of the first attaching parts (21) connection side cabinet main body (2), described cable lead-through (3) connects described top fabricated section (4) by the second attaching parts (5), and described top fabricated section (4) lays respectively at the two ends of described cable lead-through (3) with the upper end of described side cabinet main body (2).
2. side as claimed in claim 1 cabinet, it is characterized in that: Gui WeiSR1 side, described side cabinet, it is arranged between two communication cabinets; Or Gui WeiSR4 side, described side cabinet, it is arranged between two ESM racks.
3. side as claimed in claim 1 cabinet, is characterized in that: open hole in the middle of described top fabricated section (4), be connected, and be connected with described soundproofed cabin top ceiling bolt with described first attaching parts (21) bolt.
4. side as claimed in claim 1 cabinet, is characterized in that: open hole in the middle of described first attaching parts (21), be connected, and be connected with described cable lead-through (3) bolt with described top fabricated section (4) bolt.
5. side as claimed in claim 1 cabinet, is characterized in that: the through hole having energising cable in the middle of described cable lead-through (3), is connected with described second attaching parts (5) bolt, and is connected with described first attaching parts (21) bolt.
6. side as claimed in claim 1 cabinet, is characterized in that: have through hole in described second attaching parts (5), be connected with described cable lead-through (3) bolt, and is connected with the upper terminal bolt of described side cabinet main body (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510496360.XA CN105109702A (en) | 2015-08-13 | 2015-08-13 | Side cabinet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510496360.XA CN105109702A (en) | 2015-08-13 | 2015-08-13 | Side cabinet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105109702A true CN105109702A (en) | 2015-12-02 |
Family
ID=54657895
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510496360.XA Pending CN105109702A (en) | 2015-08-13 | 2015-08-13 | Side cabinet |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105109702A (en) |
Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110194269A1 (en) * | 2010-02-05 | 2011-08-11 | Airbus Operations (S.A.S.) | Connection assembly with front cabling for at least one item of electronic equipment in an aircraft |
| CN103222142A (en) * | 2010-09-10 | 2013-07-24 | 凤凰接触股份有限及两合公司 | Frame for a cable penetration system, and bush therefor |
| US20140167500A1 (en) * | 2012-09-04 | 2014-06-19 | Airbus Operations Gmbh | Method for installing an electric system into an aircraft fuselage |
| CN204103389U (en) * | 2014-09-28 | 2015-01-14 | 中国航空工业集团公司西安飞机设计研究所 | Formula cable passage can be keeped in repair |
-
2015
- 2015-08-13 CN CN201510496360.XA patent/CN105109702A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110194269A1 (en) * | 2010-02-05 | 2011-08-11 | Airbus Operations (S.A.S.) | Connection assembly with front cabling for at least one item of electronic equipment in an aircraft |
| CN103222142A (en) * | 2010-09-10 | 2013-07-24 | 凤凰接触股份有限及两合公司 | Frame for a cable penetration system, and bush therefor |
| US20140167500A1 (en) * | 2012-09-04 | 2014-06-19 | Airbus Operations Gmbh | Method for installing an electric system into an aircraft fuselage |
| CN204103389U (en) * | 2014-09-28 | 2015-01-14 | 中国航空工业集团公司西安飞机设计研究所 | Formula cable passage can be keeped in repair |
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| Date | Code | Title | Description |
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| C06 | Publication | ||
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| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20151202 |
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| RJ01 | Rejection of invention patent application after publication |