CN209016345U - Connecting cable mechanism applied to mooring unmanned aerial vehicle - Google Patents

Connecting cable mechanism applied to mooring unmanned aerial vehicle Download PDF

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Publication number
CN209016345U
CN209016345U CN201821593815.5U CN201821593815U CN209016345U CN 209016345 U CN209016345 U CN 209016345U CN 201821593815 U CN201821593815 U CN 201821593815U CN 209016345 U CN209016345 U CN 209016345U
Authority
CN
China
Prior art keywords
fixing end
unmanned plane
connection cables
connecting pin
pin
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CN201821593815.5U
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Chinese (zh)
Inventor
黄永明
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Guangzhou Guanghong Aerospace Technology Co ltd
Original Assignee
Guangzhou Guanghong Aerospace Technology Co ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Guangzhou Guanghong Aerospace Technology Co ltd filed Critical Guangzhou Guanghong Aerospace Technology Co ltd
Priority to CN201821593815.5U priority Critical patent/CN209016345U/en
Application granted granted Critical
Publication of CN209016345U publication Critical patent/CN209016345U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses an use connecting cable mechanism in mooring unmanned aerial vehicle, including the unmanned aerial vehicle main part, be equipped with connecting cable mechanism in the unmanned aerial vehicle main part, the welding of connecting cable mechanism both ends has optical fiber splice, connecting cable mechanism include detachable connection in the unmanned aerial vehicle main part the stiff end and with the link of the detachable limit of stiff end connecing, the inside equal electric connection of stiff end and link has the metal connecting piece, be equipped with the plug of taking the pin on the link, the stiff end be equipped with plug size assorted jack and with pin assorted pin notes hole, this kind of connecting cable mechanism connected mode is simple, firm, can convenience of customers's operation.

Description

It is a kind of to apply in the connection cables mechanism being tethered on unmanned plane
Technical field
The utility model relates to air vehicle technique field more particularly to a kind of apply in the connection cables being tethered on unmanned plane Mechanism.
Background technique
Captive unmanned plane is to provide DC power supply by ground, sends unmanned plane to as energy confession by being tethered at cable It answers, to maintain uninterrupted flight for a long time.It is additional under unmanned plane due to being tethered at cable, it is involved by own wt and high-altitude strong wind Effect can generate very big pulling force and unstable oscillatory forces, the so fixed very high requirement of proposition to cable is tethered at.
Existing technique for fixing is first to add a suspender member near cable ends, right to unmanned plane lower section for hanging The hanging answered hooks, and as hard point, then end is that cable connects the docking of male connector female.Such structure itself, which has no, asks Topic only requires two steps and could complete in outfield connection cables and disengaging cable, inefficiency.
CN202633889U discloses a kind of sealed quick connecting line cable end attachment device, this connector have sealing and The effect of waterproof, but the operating method of the attachment device connecting tube is cumbersome, and is not provided with error-proof structure, be easy to cause misplug hole The consequence of position.
Utility model content
The utility model is above-mentioned in order to solve the problems, such as, provides a kind of apply in the connection being tethered on unmanned plane Cable mechanism, this connection cables mechanism connection type is simple, secured, can facilitate the operation of user.
The technical scheme adopted by the utility model to solve the technical problem is as follows: the utility model provides a kind of apply The connection cables mechanism being tethered on unmanned plane, including unmanned plane main body, the unmanned plane main body are equipped with connection cables mechanism, institute It states connection cables mechanism both ends and is welded with fibre-optical splice, the connection cables mechanism includes detachable connection in unmanned plane main body On fixing end and the connecting pin that is connect with the detachable side of fixing end, the fixing end be electrically connected with inside connecting pin Metal connecting piece, the connecting pin are equipped with the plug with pin orifice, and the fixing end, which is equipped with, to match with plug size Jack and the pin to match with pin orifice.
Preferably, the plug side is evenly distributed with positioning protrusion, the position of jack side relative positioning protrusion Equipped with positioning groove.
Preferably, the fixing end is equipped with fixed block, and the fixed block is equipped with fixation hole.
Preferably, the fixing end is threadedly coupled with connecting pin, and the fixing end is external thread piece, and the connecting pin is interior Screw element, and internal screw thread is equipped with band ratchet device.
Preferably, the position that the connecting pin is in contact with the end face of fixing end jack is equipped with annular groove, the annular Sealing ring is equipped in groove.
Compared with prior art, the utility model has the beneficial effect that this connection cables mechanism realizes multi-thread cable Combined integratedization, plug side are evenly distributed with positioning protrusion, and the position of jack side relative positioning protrusion is equipped with positioning groove, Cooperation between positioning protrusion and positioning groove, plays the role of fool proof, and pin is enable quickly to be inserted into pin orifice, It avoids because of error pin orifice, and leads to the damage to the connection cables mechanism, fixing end is threadedly coupled with connecting pin, fixing end For external thread piece, connecting pin is inner thread piece, and internal screw thread is equipped with band ratchet device, simplifies operation step when cable connection Suddenly, photoelectricity cable, while the ratchet-type structure of connecting pin setting can be quickly connected, fixing end and connecting pin can be made to cooperate More fasten, so that the mechanism is born high-altitude strong wind and involve, avoid vibration scarifying phenomenon generation, further, connecting pin with The position that the end face of fixing end jack is in contact is equipped with annular groove, is equipped with sealing ring in annular groove, sealing ring can play The effect of waterproof avoids extraneous water from being flowed into inside connecting pin, influences whole using effect.
Detailed description of the invention
The present invention will be further described with reference to the accompanying drawings and examples.
Fig. 1 is a kind of structural representation applied in the connection cables mechanism being tethered on unmanned plane described in the utility model Figure;
Fig. 2 is a kind of fixation end structure applied in the connection cables mechanism being tethered on unmanned plane described in the utility model Schematic diagram;
Fig. 3 is a kind of connection end structure applied in the connection cables mechanism being tethered on unmanned plane described in the utility model Schematic diagram;
Fig. 4 is a kind of connecting pin section applied in the connection cables mechanism being tethered on unmanned plane described in the utility model Schematic diagram.
Specific embodiment
The utility model is described in further detail presently in connection with attached drawing.These attached drawings are simplified schematic diagram, Only illustrate the basic structure of the utility model in a schematic way, therefore it only shows composition related with the utility model.
It is as shown in Figs 1-4 it is a kind of apply in the connection cables mechanism being tethered on unmanned plane, including unmanned plane main body, nobody Owner's body is equipped with connection cables mechanism, and connection cables mechanism both ends are welded with fibre-optical splice, and connection cables mechanism includes removable The fixing end 1 and the connecting pin 2 connect with the detachable side of fixing end 1 that the formula of unloading is connected in unmanned plane main body are set in fixing end 1 There is fixed block 3, fixed block 3 is equipped with fixation hole 4, is electrically connected with metal connecting piece inside fixing end 1 and connecting pin 2, even It connects end 2 and is equipped with the plug 6 with pin orifice 5, fixing end 1 is equipped with the jack 7 to match with 6 size of plug and infuses with pin The pin 8 that hole 5 matches, 6 side of plug are evenly distributed with positioning protrusion 9, and the position of 7 side relative positioning protrusion 9 of jack is set There is positioning groove 10, the position that connecting pin 2 is in contact with the end face of 1 jack 7 of fixing end is equipped with annular groove 11, annular groove 11 It is interior to be equipped with sealing ring 12.
The utility model is as follows in specific implementation: this connection cables mechanism includes unmanned plane main body, is set in unmanned plane main body There is connection cables mechanism, realize multi-thread cable combined integratedization, connection cables mechanism both ends are welded with fibre-optical splice, connection cables Mechanism includes fixing end 1 of the detachable connection in unmanned plane main body and the connecting pin that connects with the detachable side of fixing end 1 2, fixing end 1 is equipped with fixed block 3, and fixed block 3 is equipped with fixation hole 4, will be fixed by the fixation hole 4 being arranged on fixed block 3 End 1 is detachably secured to uav bottom center, be electrically connected with metal inside fixing end 1 and connecting pin 2 and connect Part, metal connecting piece make positive and negative anodes, and fixing end 1 connects the power supply in unmanned plane main body, and the fibre-optical splice of fixing end connects nobody Optical fiber connector on owner's body is transmitted for data, and connecting pin 2 is connected to ground by the composite cable long more than 100 meters Power supply, the optical fiber connector on the fibre-optical splice connection ground of connecting pin 2, is transmitted, fixing end 1 is adopted with connecting pin 2 for data With single mode optical fiber, fixing end 1 is threadedly coupled with connecting pin 2, and fixing end 1 is external thread piece, and connecting pin 2 is inner thread piece, and interior Screw thread is equipped with band ratchet device, while the ratchet-type structure that connecting pin 2 is arranged, and fixing end 1 can be made to cooperate with connecting pin 2 tighter Gu alloing the mechanism to bear high-altitude strong wind to involve, the generation of vibration scarifying phenomenon is avoided, fixing end 1 and 2 spiral shell of connecting pin are passed through Connecting pin 2 need to be only inserted into fixing end 1 when connection by the mode of line connection, and is screwed into manually until fastening, work terminate, The screw thread for being tethered at cable connecting pin 2 need to be reversely only backed out, i.e., disengagable connection facilitates the operation of user, simplifies cable mechanism Operating procedure when connection can quickly connect photoelectricity cable, and connecting pin 2 is equipped with the plug 6 with pin orifice 5, fixed End 1 is equipped with the jack 7 to match with 6 size of plug and the pin 8 to match with pin orifice 5, and 6 side of plug is uniformly distributed There is positioning protrusion 9, the position of 7 side relative positioning protrusion 9 of jack is equipped with positioning groove 10, positioning protrusion 9 and positioning groove 10 Between cooperation play the role of fool proof, so that pin 8 is quickly inserted into pin orifice 5, avoid drawing because of 8 error of pin Footnote hole 5, and lead to the damage to the connection cables mechanism, the position that connecting pin 2 is in contact with the end face of 1 jack 7 of fixing end Equipped with annular groove 11, it is equipped with sealing ring 12 in annular groove 11, sealing ring 12 can play the effect of waterproof, avoid the external world Water is flowed into inside connecting pin 2, influences whole using effect.
It is enlightenment, through the above description, related work people with the above-mentioned desirable embodiment according to the utility model Member can carry out various changes and amendments in the range of without departing from this item utility model technical idea completely.This item is real It is not limited to the contents of the specification with novel technical scope, it is necessary to its technology is determined according to scope of the claims Property range.

Claims (5)

1. a kind of apply in the connection cables mechanism being tethered on unmanned plane, including unmanned plane main body, it is characterised in that: it is described nobody Owner's body is equipped with connection cables mechanism, and connection cables mechanism both ends are welded with fibre-optical splice, the connection cables mechanism It is described solid including fixing end of the detachable connection in unmanned plane main body and the connecting pin connect with the detachable side of fixing end Metal connecting piece is electrically connected with inside fixed end and connecting pin, the connecting pin is equipped with the plug with pin orifice, described Fixing end is equipped with the jack to match with plug size and the pin to match with pin orifice.
It a kind of is applied in the connection cables mechanism being tethered on unmanned plane 2. according to claim 1, it is characterised in that: described Plug side is evenly distributed with positioning protrusion, and the position of jack side relative positioning protrusion is equipped with positioning groove.
It a kind of is applied in the connection cables mechanism being tethered on unmanned plane 3. according to claim 1, it is characterised in that: described Fixing end is equipped with fixed block, and the fixed block is equipped with fixation hole.
It a kind of is applied in the connection cables mechanism being tethered on unmanned plane 4. according to claim 1, it is characterised in that: described Fixing end is threadedly coupled with connecting pin, and the fixing end is external thread piece, and the connecting pin is inner thread piece, and internal screw thread is equipped with Band ratchet device.
It a kind of is applied in the connection cables mechanism being tethered on unmanned plane 5. according to claim 1, it is characterised in that: described The position that connecting pin is in contact with the end face of fixing end jack is equipped with annular groove, is equipped with sealing ring in the annular groove.
CN201821593815.5U 2018-09-28 2018-09-28 Connecting cable mechanism applied to mooring unmanned aerial vehicle Expired - Fee Related CN209016345U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201821593815.5U CN209016345U (en) 2018-09-28 2018-09-28 Connecting cable mechanism applied to mooring unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201821593815.5U CN209016345U (en) 2018-09-28 2018-09-28 Connecting cable mechanism applied to mooring unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN209016345U true CN209016345U (en) 2019-06-21

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Application Number Title Priority Date Filing Date
CN201821593815.5U Expired - Fee Related CN209016345U (en) 2018-09-28 2018-09-28 Connecting cable mechanism applied to mooring unmanned aerial vehicle

Country Status (1)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113036522A (en) * 2021-02-24 2021-06-25 中国科学院高能物理研究所 Photoelectric composite connector

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113036522A (en) * 2021-02-24 2021-06-25 中国科学院高能物理研究所 Photoelectric composite connector

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CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20190621

Termination date: 20200928