CN206954497U - A kind of unmanned plane foot stool quick-disassembly structure part - Google Patents

A kind of unmanned plane foot stool quick-disassembly structure part Download PDF

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Publication number
CN206954497U
CN206954497U CN201720639309.4U CN201720639309U CN206954497U CN 206954497 U CN206954497 U CN 206954497U CN 201720639309 U CN201720639309 U CN 201720639309U CN 206954497 U CN206954497 U CN 206954497U
Authority
CN
China
Prior art keywords
pad
foot stool
unmanned plane
structure part
disassembly structure
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
CN201720639309.4U
Other languages
Chinese (zh)
Inventor
刘伟
陈金颖
伍文
车嘉兴
党阳
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.)
Shenzhen Micromulticopter Aero Technology Co Ltd
Original Assignee
Shenzhen Micromulticopter Aero 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 Shenzhen Micromulticopter Aero Technology Co Ltd filed Critical Shenzhen Micromulticopter Aero Technology Co Ltd
Priority to CN201720639309.4U priority Critical patent/CN206954497U/en
Application granted granted Critical
Publication of CN206954497U publication Critical patent/CN206954497U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model discloses a kind of unmanned plane foot stool quick-disassembly structure part, fuselage including unmanned plane, the fuselage bottom of unmanned plane are provided with a foot stool quick-disassembly structure part, are connected with rivet with fuselage, foot stool quick-disassembly structure part includes a foot rest base, has a through hole among the foot rest base;Also include a switch, packing ring, the first pad, the second pad and nut, one end of the switch has a screw rod, the screw rod of switch is sequentially passed through into packing ring, the first pad, foot rest base and the second pad, screw rod passes through the outboard end of the second pad to the second pad, and passes through nut check.The utility model disassembly and installation is convenient and swift, great convenience assembling, installation and transport, plays a part of connecting foot stool and unmanned plane main body.

Description

A kind of unmanned plane foot stool quick-disassembly structure part
Technical field
It the utility model is related to unmanned plane field, and in particular to a kind of unmanned plane foot stool quick-disassembly structure part.
Background technology
With unmanned plane industry hair, the problem of portable transportation of unmanned plane and fast reserve operation are installed, shows;Foot stool Quick-disassembly structure part has played vital connection function, fast quick-detach, Fast Installation, is brought greatly just to transport and carrying Profit.But as the development of technology and the raising of requirement, current unmanned plane foot stool quick-disassembly structure part can not meet group The requirement of quick convenient transportation is filled, installation effectiveness reduces cost of transportation and motor-driven operation installation is considered to foot stool Quick Release knot to improve Component is improved.
Current unmanned plane uses foot stool and the fixed form of body one to connect substantially, although the simple transport of connection It is difficult, not portable, and foot stool and body are fixed to avoid the complicated Sexual behavior mode of assembling by most of unmanned plane company The complete machine means of transportation come, this mode cost of transportation is huge, consumes many manpower and materials.
Existing unmanned plane is to be connected using foot stool with the fixed form of body one mostly, although fuselage is connected jail with foot stool Gu structure is reliable, but stretching into fuselage and foot stool one tight space inconvenience instrument, it is cumbersome then to bring dismounting Problem, allow assembler worries endlessly.And existing fuselage is integrated with foot stool so that unmanned plane is whole in transportation Body transports, and packaging volume is big, and cost of transportation is high.
First, on mounting means, conventional unmanned plane foot stool uses the integration connection of foot stool fuselage substantially, and installation process is not It is convenient.Secondly, in means of transportation, because simple mounting means before, it has to make in transportation foot stool and fuselage I.e. complete machine transport is fitted together, because complete machine is transported, bulky can not take high ferro, and such cost of transportation is just very high It is expensive.
Utility model content
Technical problem to be solved in the utility model is to provide a kind of for unmanned plane foot stool Quick Release knot on current market The defects of means of structural connection and mounting means, is improved, and substantially reduces transportation and packing greatly and dismounting is inconvenient asks Topic.
The utility model is achieved through the following technical solutions:A kind of unmanned plane foot stool quick-disassembly structure part, including nothing Man-machine fuselage, the fuselage bottom of unmanned plane are provided with a foot stool quick-disassembly structure part, are connected with rivet with fuselage, foot stool Quick Release Structural member includes a foot rest base, has a through hole among the foot rest base;
Also include a switch, packing ring, the first pad, the second pad and nut, one end of the switch has a spiral shell Bar, the screw rod of switch is sequentially passed through into packing ring, the first pad, foot rest base and the second pad, screw rod is through the second pad to the The outboard end of two pads, and pass through nut check.
As preferable technical scheme, the bottom of the foot rest base is provided with a fixing hole, and the carbon pipe of foot stool is inserted in admittedly Determine in hole, and pass through switch locking.
As preferable technical scheme, the fixing hole outboard end of the foot rest base has the open slot of " one " font.
As preferable technical scheme, the packing ring is made of aluminium, and the first pad and the second pad use PP Material, the nut are made of aluminum alloy materials.
The beneficial effects of the utility model are:The utility model disassembly and installation is convenient and swift, great convenience assembling, Installation and transport, play a part of connecting foot stool and unmanned plane main body.
Brief description of the drawings
, below will be to embodiment in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art Or the required accompanying drawing used is briefly described in description of the prior art, it should be apparent that, drawings in the following description are only It is some embodiments of the utility model, for those of ordinary skill in the art, is not paying the premise of creative work Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is the structural representation after the completion of overall package of the present utility model;
Fig. 2 is the structural representation before installation of the present utility model;
Fig. 3 is the configuration schematic diagram of structural member of the present utility model.
Embodiment
All features disclosed in this specification, or disclosed all methods or during the step of, except mutually exclusive Feature and/or step beyond, can combine in any way.
Any feature disclosed in this specification (including any accessory claim, summary and accompanying drawing), except non-specifically chatting State, can alternative features equivalent by other or with similar purpose replaced.I.e., unless specifically stated otherwise, each feature It is an example in a series of equivalent or similar characteristics.
As shown in figure 1, the fuselage including unmanned plane, the fuselage bottom of unmanned plane is provided with a foot stool quick-disassembly structure part, It is connected with rivet with fuselage, foot stool quick-disassembly structure part includes a foot rest base 2, has a through hole among the foot rest base 2;
Also include a switch 3, packing ring 4, the first pad 7, the second pad 6 and nut 1, the one end for switching 3 has one Screw rod, the screw rod of switch is sequentially passed through into packing ring 4, the first pad 7, the pad 6 of foot rest base 2 and second, screw rod pads through second Piece and is locked to the outboard end of the second pad by nut 1.
As shown in Fig. 2 the bottom of foot rest base is provided with a fixing hole, the carbon pipe 5 of foot stool is inserted in fixing hole, and is passed through Switch locking, the fixing hole outboard end of foot rest base have the open slot of " one " font.Switch locking can be passed through so that peace It is tight loaded on the carbon pipe clamp in fixing hole.
Wherein, packing ring is made of aluminium, and the first pad and the second pad use PP materials, and the nut uses aluminium Alloy material is made.
Rotary switch is only needed when installing or removing foot stool quick-disassembly structure part as figure shows, it is very convenient.Part leads to It is high with property, it is reliable to assemble and disassemble easy connection.
Unmanned plane foot stool quick-disassembly structure part is to be required and designed according to the architectural feature and flight of unmanned plane, using bias The mode of wheel locking makes the carbon pipe of foot stool be connected by foot stool quick-disassembly structure with fuselage.When foot stool is installed, foot stool Quick Release Structural member is opened, and by foot stool carbon pipe clamp into foot stool quick-disassembly structure part, is pressed the switch of foot stool quick-disassembly structure part, is made foot stool Quick Release The snap lock Quick Release foot rest base of structural member, so as to lock the foot stool carbon pipe on Quick Release foot rest base, complete the quick peace of foot stool Dress process.When foot stool is dismantled, the switch of foot stool quick-disassembly structure part is lifted, the carbon of foot stool is taken out from foot stool quick-disassembly structure part Pipe, so that foot stool completes dismounting.
The beneficial effects of the utility model are:The utility model disassembly and installation is convenient and swift, great convenience assembling, Installation and transport, play a part of connecting foot stool and unmanned plane main body.
It is described above, only specific embodiment of the present utility model, but the scope of protection of the utility model is not limited to In this, any change or replacement expected without creative work, should all cover within the scope of protection of the utility model. Therefore, the scope of protection of the utility model should be determined by the scope of protection defined in the claims.

Claims (4)

  1. A kind of 1. unmanned plane foot stool quick-disassembly structure part, it is characterised in that:Fuselage including unmanned plane, the fuselage bottom peace of unmanned plane Equipped with a foot stool quick-disassembly structure part, it is connected with rivet with fuselage, foot stool quick-disassembly structure part includes a foot rest base, the foot rest base Centre has a through hole;
    Also include a switch, packing ring, the first pad, the second pad and nut, one end of the switch has a screw rod, will The screw rod of switch sequentially passes through packing ring, the first pad, foot rest base and the second pad, and screw rod passes through the second pad to the second pad Outboard end, and pass through nut check.
  2. 2. unmanned plane foot stool quick-disassembly structure part as claimed in claim 1, it is characterised in that:The bottom of the foot rest base is provided with One fixing hole, the carbon pipe of foot stool is inserted in fixing hole, and passes through switch locking.
  3. 3. unmanned plane foot stool quick-disassembly structure part as claimed in claim 2, it is characterised in that:On the outside of the fixing hole of the foot rest base Open slot of the end with " one " font.
  4. 4. unmanned plane foot stool quick-disassembly structure part as claimed in claim 1, it is characterised in that:The packing ring is made of aluminium, First pad and the second pad use PP materials, and the nut is made of aluminum alloy materials.
CN201720639309.4U 2017-06-05 2017-06-05 A kind of unmanned plane foot stool quick-disassembly structure part Expired - Fee Related CN206954497U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720639309.4U CN206954497U (en) 2017-06-05 2017-06-05 A kind of unmanned plane foot stool quick-disassembly structure part

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720639309.4U CN206954497U (en) 2017-06-05 2017-06-05 A kind of unmanned plane foot stool quick-disassembly structure part

Publications (1)

Publication Number Publication Date
CN206954497U true CN206954497U (en) 2018-02-02

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720639309.4U Expired - Fee Related CN206954497U (en) 2017-06-05 2017-06-05 A kind of unmanned plane foot stool quick-disassembly structure part

Country Status (1)

Country Link
CN (1) CN206954497U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108423179A (en) * 2018-05-07 2018-08-21 昆山龙智翔智能科技有限公司 A kind of electronic plant protection drone
CN109795677A (en) * 2019-03-22 2019-05-24 西北工业大学 A kind of unmanned plane fast assembling-disassembling landing gear structure

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108423179A (en) * 2018-05-07 2018-08-21 昆山龙智翔智能科技有限公司 A kind of electronic plant protection drone
CN109795677A (en) * 2019-03-22 2019-05-24 西北工业大学 A kind of unmanned plane fast assembling-disassembling landing gear structure

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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: 20180202