CN205304802U - Signal transfer device and wireless communication system - Google Patents
Signal transfer device and wireless communication system Download PDFInfo
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- CN205304802U CN205304802U CN201521098402.6U CN201521098402U CN205304802U CN 205304802 U CN205304802 U CN 205304802U CN 201521098402 U CN201521098402 U CN 201521098402U CN 205304802 U CN205304802 U CN 205304802U
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- flight equipment
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- radio communication
- rotor arm
- communication system
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Abstract
The utility model discloses a signal transfer device and wireless communication system, signal transfer device include flight equipment, install the signal repeater on flight equipment and be used for controlling the remote controller of flight equipment. Wireless communication system is including receiving arrangement and emitter to and above -mentioned signal transfer device, signal transfer device is used for receiving the radio signal who is sent by emitter, and receiving arrangement is sent to in the merge, signal transfer device includes flight equipment, install the signal repeater on flight equipment and be used for controlling the remote controller of flight equipment. When for example having obstacle such as high buildings and large mansions between receiving arrangement and emitter, just can fly to the sky of high buildings and large mansions through the flight equipment ( unmanned aerial vehicle ) that remote controller control installed the signal repeater for the radio signal who is sent by emitter can directly be received to the signal repeater, and transmits immediately for receiving arrangement, and then can guarantee the normal communication between emitter and the receiving arrangement.
Description
Technical field
The utility model relates to the communication technology, and more specifically, it relates to a kind of signal transferring device and radio communication system.
Background technology
Usually, when carrying out radio communication, it is necessary to send wireless signal by a launching device, then receive by a receiving trap, such type of transmission, when accessible, very convenient. But, when there is bigger obstacle between launching device and launching device, such as high buildings and large mansions or high mountain etc., wireless signal can be stopped, have impact on the laser propagation effect of signal greatly.
Practical novel content
For realizing solving the problem, the utility model provides following technical scheme:
First, the utility model provides a kind of signal transferring device, the signal repeater for forwarding wireless signal, comprise flight equipment, being installed on described flight equipment and the telepilot for controlling described flight equipment.
Further, described flight equipment comprises without man-machine.
Further, described comprise body and multiple rotor arm being located on body and be symmetric without man-machine, each described rotor arm is provided with rotor assemblies in the one end away from body, described rotor assemblies comprises the power motor being arranged on rotor arm and the water screw being connected on power motor output shaft, described organism bottom is symmetrically installed with one pair of landing gear, in described body, treater is installed, power supply module, radio communication module and six axle gyrostats, described treater respectively with power supply module, radio communication module, power motor on six axle gyrostats and each rotor arm connects.
Further, between two landing gears, erection has an erecting frame; Described signal repeater can be dismantled with described erecting frame and be fixedly connected with.
In addition, the utility model also provides a kind of radio communication system, comprises receiving trap and launching device, also comprises signal transferring device, the wireless signal that described signal transferring device is sent by described launching device for receiving, and is forwarded to described receiving trap; The signal repeater that described signal transferring device comprises flight equipment, be installed on described flight equipment and the telepilot for controlling described flight equipment.
Further, described flight equipment comprises without man-machine.
Further, described comprise body and multiple rotor arm being located on body and be symmetric without man-machine, each described rotor arm is provided with rotor assemblies in the one end away from body, described rotor assemblies comprises the power motor being arranged on rotor arm and the water screw being connected on power motor output shaft, described organism bottom is symmetrically installed with one pair of landing gear, in described body, treater is installed, power supply module, radio communication module and six axle gyrostats, described treater respectively with power supply module, radio communication module, power motor on six axle gyrostats and each rotor arm connects.
Further, between two landing gears, erection has an erecting frame; Described signal repeater can be dismantled with described erecting frame and be fixedly connected with.
Compared with prior art, the utility model has the advantages that: by above technical scheme, when there is the obstacles such as such as high buildings and large mansions between receiving trap and launching device, the flight equipment (without man-machine) that just can control to be provided with by telepilot signal repeater flies to the overhead of high buildings and large mansions, signal repeater is made can directly to receive the wireless signal sent by launching device, and forwarding to receiving trap immediately, and then the normal communication that can ensure between launching device and receiving trap.
Accompanying drawing explanation
Fig. 1 is the principle of work figure of radio communication system of the present utility model;
Fig. 2 is without man-machine schematic diagram in the utility model.
Reference numeral: 1, without man-machine, 11, rotor arm, 12, rotor assemblies, 121, water screw, 122, power motor, 13, landing gear, 14, erecting frame, 2, signal repeater.
Embodiment
Referring to figs. 1 through Fig. 2, the utility model is described further.
First, the utility model provides a kind of signal transferring device, the signal repeater 2 for forwarding wireless signal, comprise flight equipment, being installed on flight equipment and the telepilot for controlling flight equipment. In the present embodiment, flight equipment comprises without man-machine, and 1. By above technical scheme, just can utilizing without man-machine, 1 Load Signal repeater 2, flies to the top of high building, receives the wireless signal sent by the launching device of high building side, and is forwarded to the receiving trap of another side of high building.
With reference to Fig. 2, without man-machine, 1 comprises body and multiple rotor arm being located on body and be symmetric, 11, each rotor arm, 11 are provided with rotor assemblies 12 in the one end away from body, rotor assemblies 12 comprises and is arranged on rotor arm, power motor 122 on 11 and the water screw 121 being connected on power motor 122 output shaft, organism bottom is symmetrically installed with one pair of landing gear 13, treater is installed in body, power supply module, radio communication module and six axle gyrostats, treater respectively with power supply module, radio communication module, six axle gyrostats and each rotor arm, power motor 122 on 11 connects.
With reference to Fig. 2, in the present embodiment, between two landing gears 13, erection has an erecting frame 14; Signal repeater 2 can be dismantled with erecting frame 14 and be fixedly connected with.
In addition, the utility model also provides a kind of radio communication system, comprises receiving trap and launching device, also comprises above-mentioned signal transferring device. The wireless signal that described signal transferring device is sent by described launching device for receiving, and it is forwarded to described receiving trap.
The above is only preferred implementation of the present utility model, and protection domain of the present utility model is also not only confined to above-described embodiment, and all technical schemes belonged under the utility model thinking all belong to protection domain of the present utility model. It is noted that for those skilled in the art, in the some improvements and modifications not departed under the utility model principle prerequisite, these improvements and modifications also should be considered as protection domain of the present utility model.
Claims (8)
1. a signal transferring device, for forwarding wireless signal, is characterized in that, the signal repeater (2) comprise flight equipment, being installed on described flight equipment and the telepilot for controlling described flight equipment.
2. signal transferring device according to claim 1, is characterized in that, described flight equipment comprises without man-machine (1).
3. signal transferring device according to claim 2, it is characterized in that, described comprise body and multiple rotor arm (11) being located on body and be symmetric without man-machine (1), each described rotor arm (11) is provided with rotor assemblies (12) in the one end away from body, described rotor assemblies (12) comprises the power motor (122) being arranged on rotor arm (11) and the water screw (121) being connected on power motor (122) output shaft, described organism bottom is symmetrically installed with one pair of landing gear (13), in described body, treater is installed, power supply module, radio communication module and six axle gyrostats, described treater respectively with power supply module, radio communication module, power motor (122) on six axle gyrostats and each rotor arm (11) connects.
4. signal transferring device according to claim 3, is characterized in that, between two landing gears (13), erection has an erecting frame (14); Described signal repeater (2) can be dismantled with described erecting frame (14) and be fixedly connected with.
5. a radio communication system, comprises receiving trap and launching device, it is characterized in that, also comprises signal transferring device, the wireless signal that described signal transferring device is sent by described launching device for receiving, and is forwarded to described receiving trap; Described signal transferring device comprises flight equipment, be installed on described flight equipment signal repeater (2) and the telepilot for controlling described flight equipment.
6. radio communication system according to claim 5, is characterized in that, described flight equipment comprises without man-machine (1).
7. radio communication system according to claim 6, it is characterized in that, described comprise body and multiple rotor arm (11) being located on body and be symmetric without man-machine (1), each described rotor arm (11) is provided with rotor assemblies (12) in the one end away from body, described rotor assemblies (12) comprises the power motor (122) being arranged on rotor arm (11) and the water screw (121) being connected on power motor (122) output shaft, described organism bottom is symmetrically installed with one pair of landing gear (13), in described body, treater is installed, power supply module, radio communication module and six axle gyrostats, described treater respectively with power supply module, radio communication module, power motor (122) on six axle gyrostats and each rotor arm (11) connects.
8. radio communication system according to claim 7, is characterized in that, between two landing gears (13), erection has an erecting frame (14); Described signal repeater (2) can be dismantled with described erecting frame (14) and be fixedly connected with.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN201521098402.6U CN205304802U (en) | 2015-12-25 | 2015-12-25 | Signal transfer device and wireless communication system |
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CN201521098402.6U CN205304802U (en) | 2015-12-25 | 2015-12-25 | Signal transfer device and wireless communication system |
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CN205304802U true CN205304802U (en) | 2016-06-08 |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106325298A (en) * | 2016-09-12 | 2017-01-11 | 珠海市杰理科技有限公司 | Unmanned plane range extension control system and unmanned plane range extension control method |
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2015
- 2015-12-25 CN CN201521098402.6U patent/CN205304802U/en active Active
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN106325298A (en) * | 2016-09-12 | 2017-01-11 | 珠海市杰理科技有限公司 | Unmanned plane range extension control system and unmanned plane range extension control method |
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TR01 | Transfer of patent right |
Effective date of registration: 20190529 Address after: 215000 No. 118 Nanyuan North Road, Gusu District, Suzhou City, Jiangsu Province Patentee after: Suzhou Bangyao Electronic Technology Co., Ltd. Address before: 215002 No. 18 East Second Road, Gusu District, Suzhou City, Jiangsu Province Patentee before: SUZHOU KANGHONG INTELLIGENT ENGINEERING CO., LTD. |