CN205044993U - Carry formula interferometer that goes up to air - Google Patents
Carry formula interferometer that goes up to air Download PDFInfo
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- CN205044993U CN205044993U CN201520824290.1U CN201520824290U CN205044993U CN 205044993 U CN205044993 U CN 205044993U CN 201520824290 U CN201520824290 U CN 201520824290U CN 205044993 U CN205044993 U CN 205044993U
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- carry
- antenna
- lower cover
- locating part
- formula lift
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Abstract
The utility model discloses a carry formula interferometer that goes up to air, it includes interconnect lower cover (1) and upper cover (2), the both sides of lower cover (1) are provided with one or more hanging scroll (3) of carry on unmanned aerial vehicle of being convenient for, the bottom of lower cover (1) still is equipped with the antenna fixed connection port that is used for connecting the antenna, antenna fixed connection port and antenna connection spare (5) fixed connection. The utility model discloses well carry formula interferometer that goes up to air's both sides accessible hanging scroll and install the carry spare on unmanned aerial vehicle, carry to the unmanned aerial vehicle on, its bottom accessible antenna connection spare and interferometer direction -finding antenna connection to the fast assembly interferometer direction -finding equipment that becomes to go up to the air. The utility model discloses simple structure, the carry mode is convenient and reliable.
Description
Technical field
The utility model relates to aircraft and carries monitoring equipment field, particularly relates to a kind of carry formula lift-off interferometer.
Background technology
Due to surface em circumstance complication, the transmission of ultrashort waves (VHF/UHF) radio signal, by the impact of landform, atural object, high tension cord and industrial traffic etc., causes that propagation path is changeable, the not pure and mild phase fluctuation of polarization.And the transmission environment of airwaves is comparatively clean, aerial monitoring is more much better than the effect of ground monitoring.Therefore, we have proposed the new ideas of " stereoscopic monitoring ", namely on the basis of ground continental rise stationary monitoring or mobile monitoring, increase airborne aerial monitoring technology means, by realizing aerial high-precision monitoring and DF and location, to make up the deficiency of ground monitoring at the upper monitoring equipment of installing of aircraft (as: unmanned plane).But current carry mode has carry inconvenience, the various problems such as stability, poor reliability.
Utility model content
The purpose of this utility model is to overcome the deficiencies in the prior art, provides a kind of carry formula lift-off interferometer, overcomes carry inconvenience, the problem of carry instability.
The purpose of this utility model is achieved through the following technical solutions: a kind of carry formula lift-off interferometer, and it comprises interconnective lower cover and upper cover, and the both sides of described lower cover are provided with one or morely is convenient to the hanging scroll of carry on unmanned plane.
Further, described hanging scroll comprises the first locating part, the second locating part and axis body, described axis body is connected with the first locating part through the second locating part, and the axial line of the first locating part, the second locating part and axis body is same axial line, the axis body between described first locating part and the second locating part is formed is convenient to the carry portion of carry on unmanned plane.
In the utility model, described hanging scroll is connected with unmanned plane by carry part.
Further, one end of described carry part offers the groove of bending, and one end of described groove is open end, and the other end of described groove is carry end, described carry portion slips into carry end by open end, and the other end of described carry part is provided with the carry connecting panel for being fixedly connected with unmanned plane.
Further, described groove comprises at least two direct through groove be communicated with, and forms at least one kink.
In the utility model, the bottom of the described lower cover also antenna that can arrange for connecting antenna is fixedly connected with port, and described antenna is fixedly connected with port and is fixedly connected with antenna connection.
Further, described antenna is fixedly connected with port and is connected with antenna by antenna connection, the middle part of described antenna connection is provided with locking big nut, one end of described antenna connection is fixedly connected with port match by adapter plate and antenna and is connected, the described antenna connection other end is provided with antenna docking port, described antenna docking port starts there is positioning groove, in described antenna docking port, is provided with antenna electrical interface.
Further, described antenna electrical interface comprises radio frequency interface and control interface, and described radio frequency interface comprises BMA adaptor union, and described control interface comprises J adaptor union.
Further, the side of described lower cover is also provided with and one or morely wears wall joint.
Further, the bottom interior wall of described lower cover is also provided with one or more reinforced rib.
Further, the side of described lower cover and upper cover is also provided with heat abstractor.
Further, described lower cover internal fixtion is provided with master board and the adaptor for being electrically connected master board.
Further, be also fixedly installed battery by battery cover board in described lower cover, described battery is electrically connected by adaptor and master board.
The beneficial effects of the utility model are: the utility model proposes a kind of carry formula lift-off interferometer, its both sides are by hanging scroll and the carry part that is arranged on unmanned plane, carry is on unmanned plane, be connected with interferometer direction finding antenna by antenna connection bottom it, thus rapid-assembling becomes lift-off interferometer direction finding equipment.The utility model structure is simple, and carry mode is convenient and reliable.
Accompanying drawing explanation
Fig. 1 is the front view of the carry formula lift-off interferometer after having assembled in the utility model;
Fig. 2 is the structural representation of hanging scroll in the utility model;
Fig. 3 is the structural representation of carry part in the utility model;
Fig. 4 is the upward view of carry formula lift-off interferometer in the utility model;
Fig. 5 is the lower cover bottom construction schematic diagram of carry formula lift-off interferometer in the utility model;
Fig. 6 is the lower cover inner structure schematic diagram of carry formula lift-off interferometer in the utility model;
In figure, 1-lower cover, 2-upper cover, 3-hanging scroll, 301-first locating part, 302-second locating part, 303-axis body, 4-carry part, 401-groove, 402-carry connecting panel, 5-antenna connection, 501-adapter plate, 502-antenna docking port, 503-positioning groove, 504-radio frequency interface, 505-control interface, 6-heat abstractor, 7-wears wall joint, 8-reinforced rib, 9-master board, 10-adaptor, 11-battery, 12-battery cover board.
Detailed description of the invention
Below in conjunction with accompanying drawing, the technical solution of the utility model is described in further detail, but protection domain of the present utility model is not limited to the following stated.
As shown in Figure 1, a kind of carry formula lift-off interferometer, it comprises interconnective lower cover 1 and upper cover 2, and the both sides of described lower cover 1 are provided with one or morely is convenient to the hanging scroll 3 of carry on unmanned plane.
As shown in Figure 2, further, described hanging scroll 3 comprises the first locating part 301, second locating part 302 and axis body 303, described axis body 303 is connected with the first locating part 301 through the second locating part 302, and the axial line of the first locating part 301, second locating part 302 and axis body 303 is same axial line, the axis body 303 between described first locating part 301 and the second locating part 302 is formed is convenient to the carry portion 304 of carry on unmanned plane.
As shown in Figure 3, further, described hanging scroll 3 is connected with unmanned plane by carry part 4, one end of described carry part 4 offers the groove 401 of bending, one end of described groove 401 is open end, the other end of described groove 401 is carry end, and described carry portion 304 slips into carry end by open end, completes carry action.The other end of described carry part 4 is provided with the carry connecting panel 402 for being fixedly connected with unmanned plane.
The groove 401 of described bending is as 7 font grooves, comprise at least two direct through groove be communicated with, form at least one kink, groove 401 shown in Fig. 3 is connected to form by three direct through groove, and has two kinks, the utility model restriction direct through groove and do not adopt the object of arc-shaped slot to be, the stability of further lifting carry and reliability, avoid lift-off interferometer in carry flight course, due to factors such as lifting and air-flows, hanging scroll is skidded off from groove 401.
Further, the antenna that the bottom of described lower cover 1 is also provided with for connecting antenna is fixedly connected with port, described antenna is fixedly connected with port and is fixedly connected with antenna connection 5, the middle part of described antenna connection 5 is provided with locking big nut, and described antenna connection 5 mates with the antenna of different frequency range type is compatible mutually.
As shown in Figure 4, further, described antenna is fixedly connected with port and is connected with antenna by antenna connection 5, one end of described antenna connection 5 is fixedly connected with port match by adapter plate 501 and antenna and is connected, described antenna connection 5 other end is provided with antenna docking port 502, described antenna docking port 502 starts there is positioning groove 503, in described antenna docking port 502, is provided with antenna electrical interface.
Further, described antenna electrical interface comprises radio frequency interface 504 and control interface 505, in the utility model, blindmate also can be adopted to design, as as described in radio frequency interface 504 can adopt BMA adaptor union, described control interface 505 can adopt the J30 adaptor union of micro-rectangle.
Further, the side of described lower cover 1 also can be established and one or morely be worn wall joint 7, wears knee-joint head, as radio frequency input adapter and antenna out splice going splice as arranged two.
Further, the bottom interior wall of described lower cover 1 also can establish one or more reinforced rib 8, as shown in Figure 5, adopt the reinforced rib of four distributions in X-type.
Further, heat abstractor 6 also can be established in the side of described lower cover 1 and upper cover 2, as arranged multiple breather port, natural wind is incorporated into device interior, thus is taken away by the heat of device interior, reduces the temperature of equipment.
As shown in Figure 6, further, described lower cover 1 internal fixtion is provided with master board 9 and the adaptor 10 for being electrically connected master board 9.Described master board 9 is connected with electronic compass, WiFi module, power supply processing module, aerial signal port etc. by adaptor 10.
Further, be also fixedly installed battery 11 by battery cover board 12 in described lower cover 1, described battery is electrically connected by adaptor 10 and master board 9.Described battery 11 can adopt 18650 lithium celies.
Describe in an illustrative manner according to a kind of carry formula lift-off interferometer of the present utility model above with reference to accompanying drawing.But; those skilled in the art are to be understood that; for a kind of carry formula lift-off interferometer that above-mentioned the utility model proposes; various improvement can also be made on the basis not departing from the utility model content; or equivalent replacement is carried out to wherein portion of techniques feature; all within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.Therefore, protection domain of the present utility model should be determined by the content of appending claims.
Claims (10)
1. a carry formula lift-off interferometer, it comprises interconnective lower cover (1) and upper cover (2), it is characterized in that: the both sides of described lower cover (1) are provided with one or morely is convenient to the hanging scroll of carry on unmanned plane (3).
2. a kind of carry formula lift-off interferometer according to claim 1, it is characterized in that: described hanging scroll (3) comprises the first locating part (301), second locating part (302) and axis body (303), described axis body (303) is connected with the first locating part (301) through the second locating part (302), and the first locating part (301), the axial line of the second locating part (302) and axis body (303) is same axial line, axis body (303) between described first locating part (301) and the second locating part (302) is formed is convenient to the carry portion (304) of carry on unmanned plane.
3. a kind of carry formula lift-off interferometer according to claim 1, is characterized in that: the antenna that the bottom of described lower cover (1) is also provided with for connecting antenna is fixedly connected with port, and described antenna is fixedly connected with port and is fixedly connected with antenna connection (5).
4. a kind of carry formula lift-off interferometer according to claim 3, it is characterized in that: described antenna is fixedly connected with port and is connected with antenna by antenna connection (5), described antenna connection (5) middle part is provided with locking big nut, one end of described antenna connection (5) is fixedly connected with port match by adapter plate (501) with antenna and is connected, described antenna connection (5) other end is provided with antenna docking port (502), described antenna docking port (502) starts there is positioning groove (503), in described antenna docking port (502), is provided with antenna electrical interface.
5. a kind of carry formula lift-off interferometer according to claim 4, it is characterized in that: described antenna electrical interface comprises radio frequency interface (504) and control interface (505), described radio frequency interface (504) comprises BMA adaptor union, and described control interface (505) comprises J30 adaptor union.
6. a kind of carry formula lift-off interferometer according to claim 2, it is characterized in that: described hanging scroll (3) is connected with unmanned plane by carry part (4), one end of described carry part (4) offers the groove (401) of bending, one end of described groove (401) is open end, the other end of described groove (401) is carry end, described carry portion (304) slips into carry end by open end, and the other end of described carry part (4) is provided with the carry connecting panel (402) for being fixedly connected with unmanned plane.
7. a kind of carry formula lift-off interferometer according to claim 1, it is characterized in that: the side of described lower cover (1) is also provided with one or morely wears wall joint (7), the bottom interior wall of described lower cover (1) is also provided with one or more reinforced rib (8), the side of described lower cover (1) and upper cover (2) is provided with heat abstractor (6).
8. a kind of carry formula lift-off interferometer according to claim 1, is characterized in that: described lower cover (1) internal fixtion is provided with master board (9) and the adaptor (10) for being electrically connected master board (9).
9. a kind of carry formula lift-off interferometer according to claim 8, it is characterized in that: be also fixedly installed battery (11) by battery cover board (12) in described lower cover (1), described battery is electrically connected by adaptor (10) and master board (9).
10. a kind of carry formula lift-off interferometer according to claim 6, is characterized in that: described groove (401) comprises at least two direct through groove be communicated with, and forms at least one kink.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520824290.1U CN205044993U (en) | 2015-10-23 | 2015-10-23 | Carry formula interferometer that goes up to air |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520824290.1U CN205044993U (en) | 2015-10-23 | 2015-10-23 | Carry formula interferometer that goes up to air |
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| CN205044993U true CN205044993U (en) | 2016-02-24 |
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| CN201520824290.1U Active CN205044993U (en) | 2015-10-23 | 2015-10-23 | Carry formula interferometer that goes up to air |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109374531A (en) * | 2018-11-09 | 2019-02-22 | 浙江海洋大学 | Sea area spilled oil monitoring device based on remote sensing |
| CN111348206A (en) * | 2018-12-24 | 2020-06-30 | 广州慧睿思通信息科技有限公司 | Unmanned aerial vehicle carries direction-finding device |
| CN112009706B (en) * | 2020-10-19 | 2021-01-08 | 南京开天眼无人机科技有限公司 | Unmanned aerial vehicle signal laser emitter |
-
2015
- 2015-10-23 CN CN201520824290.1U patent/CN205044993U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109374531A (en) * | 2018-11-09 | 2019-02-22 | 浙江海洋大学 | Sea area spilled oil monitoring device based on remote sensing |
| CN109374531B (en) * | 2018-11-09 | 2021-04-20 | 浙江海洋大学 | Sea area oil spilling monitoring devices based on remote sensing |
| CN111348206A (en) * | 2018-12-24 | 2020-06-30 | 广州慧睿思通信息科技有限公司 | Unmanned aerial vehicle carries direction-finding device |
| CN112009706B (en) * | 2020-10-19 | 2021-01-08 | 南京开天眼无人机科技有限公司 | Unmanned aerial vehicle signal laser emitter |
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