CN202153740U - Airborne equipment structure for airplane wireless communication - Google Patents
Airborne equipment structure for airplane wireless communication Download PDFInfo
- Publication number
- CN202153740U CN202153740U CN2011202829529U CN201120282952U CN202153740U CN 202153740 U CN202153740 U CN 202153740U CN 2011202829529 U CN2011202829529 U CN 2011202829529U CN 201120282952 U CN201120282952 U CN 201120282952U CN 202153740 U CN202153740 U CN 202153740U
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- cabinet
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- airborne equipment
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- wireless communication
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- 238000004891 communication Methods 0.000 title claims abstract description 40
- 230000005855 radiation Effects 0.000 claims description 10
- 238000000926 separation method Methods 0.000 claims 1
- 238000012827 research and development Methods 0.000 abstract 1
- 210000000515 tooth Anatomy 0.000 description 8
- 238000000034 method Methods 0.000 description 7
- 238000013461 design Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 2
- 230000010354 integration Effects 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 230000005670 electromagnetic radiation Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000010295 mobile communication Methods 0.000 description 1
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Abstract
The present utility model relates to an airborne equipment structure for airplane wireless communication. The structure comprises a power supply module and a wireless communication module arranged inside a cabinet of airborne equipment, a power supply interface for connecting with a power supply, an antenna interface for connecting with an antenna and a network interface for connecting with an airborne network, and the three interfaces are arranged outside the cabinet. The power supply interface is connected with the power supply module through a conducting wire, and the antenna interface and the network interface are respectively connected with the wireless communication module through conducting wires. The cabinet is an aviation standard cabinet. In the structure, modules used by ground communication equipment are combined with the aviation standard cabinet, thus the equipment cost is reduced, and the equipment research and development period is accelerated.
Description
Technical field
The utility model relates to avionic device, particularly is used for the structure of the airborne equipment of aircraft radio communication.
Background technology
The design of traditional avionic device and the module, components and parts, the parts that make to use all be special use, cost an arm and a leg, the R&D cycle is long.
In addition, aircraft industry is in order to guarantee aircraft navigation safety, be provided with can electromagnetic radiation shielding the air standard cabinet, but this air standard cabinet just is used for the electronic equipment of aircraft industry regulation.
In addition, the module that is used for terrestrial wireless communication at present is very ripe, and particularly the LTE communication module has been suitable for remote-wireless communication, but so far, these modules also just are used for land mobile communication.
Summary of the invention
The purpose of the utility model provides a kind of airborne equipment structure that is used for the aircraft radio communication, so that the module that ground communication facilities is used combines with the air standard cabinet, thereby reduces equipment cost, the R&D cycle of accelerating equipment.
The airborne equipment structure that is used for the aircraft radio communication of the utility model comprises:
Power module and wireless communication module are installed in the cabinet of airborne equipment;
On the outside of said cabinet, install and be used to connect the power supply interface of power supply, the network interface that is used to connect the antennal interface of antenna and is used for network on the junctor;
Said power supply interface connects said supply module through lead, and said antennal interface is connected said wireless communication module through lead respectively with network interface.
Wherein, said cabinet is the air standard cabinet.
Wherein, said power supply interface, antennal interface and network interface are integrated in the connector, and said connector is fixed on the rear portion of said cabinet.
Wherein, said connector is divided into three zones, first area to the, and wherein first area and second area comprise a plurality of contacts that are used for antennal interface and radio network interface respectively, and the 3rd zone comprises a plurality of contacts that are used for power supply interface and wired network interface.
Wherein, the quantity of a plurality of contacts of first area and second area is 10.
Wherein, the quantity of a plurality of contacts in the 3rd zone is 64.
Wherein, one or two sidewall of said cabinet is the radiation tooth sidewall.
Wherein, said power module and wireless communication module are close to the inboard of said radiation tooth sidewall respectively.
Wherein, said wireless communication module is the general module of ground communication facilities.
Wherein, said wireless communication module and power module can be integrated into a module.
The technique effect of the utility model is, makes full use of the module of existing ground installation, reasonably interconnects, and is assemblied in to constitute complete machine in the air standard cabinet, helps fast integration and reduces cost.
Below in conjunction with accompanying drawing the utility model is elaborated.
Description of drawings
Fig. 1 shows that the utility model is used for the sketch map of the airborne equipment structure of aircraft radio communication;
Fig. 2 is the sketch map that shows the utility model airborne equipment cabinet;
Fig. 3 is the sketch map of cabinet left side wall shown in Figure 2;
Fig. 4 is the sketch map of cabinet right side wall shown in Figure 2;
Fig. 5 is the sketch map of cabinet rear wall connector shown in Figure 2;
Fig. 6 is the sketch map that shows first embodiment that is the utility model airborne equipment structure;
Fig. 7 is the sketch map that shows second embodiment that is the utility model airborne equipment structure.
Embodiment
The airborne equipment structure that is used for the aircraft radio communication of the utility model that Fig. 1 has shown, as shown in Figure 1, the structure of the airborne equipment of the utility model comprises: power module 3 and wireless communication module 4 are installed in the cabinet 1 of airborne equipment; On the outside of said cabinet 1, install and be used to connect the power supply interface 6 of power supply, the network interface 8 that is used to connect the antennal interface 7 of antenna and is used for network on the junctor; Power supply interface 6 connects supply module 3 through lead, and antennal interface 7 is connected wireless communication module 4 through lead respectively with network interface 8.
Characteristics of the utility model are, wireless communication module 4 is the general module of ground communication facilities, and for example wireless communication module 4 can adopt the corresponding module of LTE standard.
Another characteristics of the utility model are, with the cabinet of air standard cabinet as airborne equipment.
As stated, each module of the inside of traditional airborne equipment and interconnection thereof all are to design according to the special interface of air equipment, structural requirement, and the design cycle is long, and cost is high.The utility model uses the general module of existing ground installation, and each module is assemblied in the air standard cabinet, reaches the quick development of equipment and purpose cheaply, because adopt the air standard cabinet, also satisfies the requirement of aeronautical environment to the equipment complete machine simultaneously.
Particularly; Owing to adopt the air standard cabinet; Therefore complete machine can be installed on the aircraft on mechanical structure smoothly, and the air standard cabinet can protect internal module not receive the influence of flight environment of vehicle in addition, has also shielded wireless communication module to the issuable influence of aircraft simultaneously.
Fig. 2 has shown the cabinet of the airborne equipment that is used for the aircraft radio communication of utility model, and is as shown in Figure 2, and the left side wall of cabinet 1 and right side wall are radiation tooth sidewall 2.
Fig. 3 has shown the left side wall of cabinet shown in Figure 21, and Fig. 4 has shown the right side wall of cabinet 1 shown in Figure 2, and like Fig. 3 and shown in Figure 4, the left and right sides sidewall of cabinet 1 is the radiation tooth sidewall that comprises a plurality of radiation tooths 21.For example each sidewall comprises 16 complete black radiation tooths 21.
The inboard that power module 3 in the cabinet and wireless communication module 4 are close to said radiation tooth sidewall 21 respectively.
Fig. 5 has shown the rear wall of cabinet shown in Figure 21, and is as shown in Figure 5, and the rear wall of cabinet is provided with a connector 5, and above-mentioned power supply interface 6, antennal interface 7 and network interface 8 are integrated in this connector 5.
Fig. 6 has shown first embodiment of structure of the airborne equipment of the utility model, and in this embodiment, the communication module 4 in the cabinet 1 comprises radio-frequency module 41 and protocol process module 42.
In first embodiment of the utility model, power module 3 is used for obtaining electric power from aircraft, and converts the electric power that is fit to radio-frequency module and protocol process module use into.It is protocol process module 42 needed digital signals that radio-frequency module 41 is used for the electrical signal conversion on the communication antenna.Protocol process module 42 is realized the network of aircraft itself and the exchanges data of aircraft radio communication opposite end.
Fig. 7 has shown second embodiment of structure of the airborne equipment of the utility model, and in this embodiment, the power module 3 in the cabinet 1 is integrated into a module (chip) 9 with wireless communication module 4.
Because the utility model has adopted said structure, therefore have following technique effect:
1) makes full use of the module that has ground installation now, reasonably interconnect, be assemblied in formation complete machine in the air standard cabinet, be beneficial to fast integration and reduce cost;
2) the cabinet rear portion adopt connector that is divided into three zones integrated at least three interfaces, make the utility model can connect wired or wireless local area network (LAN) on external power source, antenna and the machine easily;
3) cabinet left and right sides outside adopts all black and radiation tooth structure, and internal module is close to cabinet left and right sides inside sidewalls when installing, and helps the internal module heat is distributed to the cabinet outside through cabinet left and right sides sidewall.
Although preceding text specify the utility model, the utility model is not limited thereto, and those skilled in the art of the present technique can carry out various modifications according to the principle of the utility model.Therefore, all modifications of being done according to the utility model principle all are to be understood that to falling into the protection range of the utility model.
Claims (10)
1. airborne equipment structure that is used for the aircraft radio communication is characterized in that:
Power module and wireless communication module are installed in the cabinet of airborne equipment;
On the outside of said cabinet, install and be used to connect the power supply interface of power supply, the network interface that is used to connect the antennal interface of antenna and is used for network on the junctor;
Said power supply interface connects said supply module through lead, and said antennal interface is connected said wireless communication module through lead respectively with network interface.
2. airborne equipment structure according to claim 1 is characterized in that, said cabinet is the air standard cabinet.
3. airborne equipment structure according to claim 2 is characterized in that, said power supply interface, antennal interface and network interface are integrated in the connector, and said connector is fixed on the rear portion of said cabinet.
4. airborne equipment structure according to claim 3; It is characterized in that; Said connector is divided into three zones, first area to the; Wherein first area and second area comprise a plurality of contacts that are used for antennal interface and radio network interface respectively, and the 3rd zone comprises a plurality of contacts that are used for power supply interface and wired network interface.
5. airborne equipment structure according to claim 4 is characterized in that, the quantity of a plurality of contacts of first area and second area is 10.
6. airborne equipment structure according to claim 4 is characterized in that, the quantity of a plurality of contacts in the 3rd zone is 64.
7. airborne equipment structure according to claim 1 and 2 is characterized in that, one or two sidewall of said cabinet is the radiation tooth sidewall.
8. airborne equipment structure according to claim 7 is characterized in that, said power module and wireless communication module are the module of two separations, and is close to the inboard of said radiation tooth sidewall respectively.
9. airborne equipment structure according to claim 8 is characterized in that, said wireless communication module is the general module of ground communication facilities.
10. airborne equipment structure according to claim 7 is characterized in that, said wireless communication module and power module are integrated into a module.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011202829529U CN202153740U (en) | 2011-08-05 | 2011-08-05 | Airborne equipment structure for airplane wireless communication |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011202829529U CN202153740U (en) | 2011-08-05 | 2011-08-05 | Airborne equipment structure for airplane wireless communication |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202153740U true CN202153740U (en) | 2012-02-29 |
Family
ID=45694233
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011202829529U Expired - Lifetime CN202153740U (en) | 2011-08-05 | 2011-08-05 | Airborne equipment structure for airplane wireless communication |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202153740U (en) |
-
2011
- 2011-08-05 CN CN2011202829529U patent/CN202153740U/en not_active Expired - Lifetime
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| ASS | Succession or assignment of patent right |
Owner name: BEIJING WEIBANG YUANHANG WIRELESS TECHNOLOGY CO., Free format text: FORMER OWNER: FEITIAN XUNDA (BEIJING) AEROSPACE INFORMATION TECHNOLOGY CO., LTD. Effective date: 20121128 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 100086 HAIDIAN, BEIJING TO: 100088 HAIDIAN, BEIJING |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20121128 Address after: 100088 Beijing city Haidian District No. 6 Zhichun Road Jinqiu International Building area B 701B Patentee after: Beijing Weibang Yuanhang Wireless Technology Co., Ltd. Address before: 100086, Beijing, Zhichun Road, Haidian District No. 113 silver net center, block A, 703 Patentee before: Flying Schindler (Beijing) Aviation Information Technology Co., Ltd. |
|
| ASS | Succession or assignment of patent right |
Owner name: HANGTONG INTERNET INFORMATION SERVICE CO., LTD. Free format text: FORMER OWNER: BEIJING WEIBANG YUANHANG WIRELESS TECHNOLOGY CO., LTD. Effective date: 20130724 |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| COR | Change of bibliographic data |
Free format text: CORRECT: ADDRESS; FROM: 100088 HAIDIAN, BEIJING TO: 300300 DONGLI, TIANJIN |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20130724 Address after: 300300 Central Avenue, Tianjin Airport Economic Zone, east of four Avenue, Crowne Plaza, 2-2-1106 Patentee after: AEROER INTERNET INFORMATION SERVICE CO., LTD. Address before: 100088 Beijing city Haidian District No. 6 Zhichun Road Jinqiu International Building area B 701B Patentee before: Beijing Weibang Yuanhang Wireless Technology Co., Ltd. |
|
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160205 Address after: 401135 Chongqing Yubei District City Longxing Zhen Ying Long Road No. 19 Patentee after: Chongqing Airnet Science and Technology Co., Ltd. Address before: 300300 Central Avenue, Tianjin Airport Economic Zone, east of four Avenue, Crowne Plaza, 2-2-1106 Patentee before: AEROER INTERNET INFORMATION SERVICE CO., LTD. |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20180612 Address after: 100192 Room 308, a 3, Yongtai Zhuang North Road, Haidian District, Beijing, 9 Patentee after: Hang Guang satellite network limited liability company Address before: No. 19, Longxing Town, Yubei District, Chongqing, Chongqing Patentee before: Chongqing Airnet Science and Technology Co., Ltd. |
|
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: Airborne equipment structure for aircraft wireless communication Effective date of registration: 20201117 Granted publication date: 20120229 Pledgee: Tianyi smart Aviation Technology Co., Ltd Pledgor: Hang Guang satellite network LLC Registration number: Y2020990001354 |
|
| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20120229 |