CN206087269U - Electronic foot rest that rises and falls of quick detach - Google Patents
Electronic foot rest that rises and falls of quick detach Download PDFInfo
- Publication number
- CN206087269U CN206087269U CN201621078913.6U CN201621078913U CN206087269U CN 206087269 U CN206087269 U CN 206087269U CN 201621078913 U CN201621078913 U CN 201621078913U CN 206087269 U CN206087269 U CN 206087269U
- Authority
- CN
- China
- Prior art keywords
- foot rest
- steering wheel
- aircraft
- lid
- foot
- 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
Links
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims description 14
- 229910052799 carbon Inorganic materials 0.000 claims description 14
- 238000004806 packaging method and process Methods 0.000 abstract description 7
- 230000001174 ascending effect Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 2
- 238000010276 construction Methods 0.000 description 2
- 230000003028 elevating effect Effects 0.000 description 2
- 238000012856 packing Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000000630 rising effect Effects 0.000 description 1
- 238000004078 waterproofing Methods 0.000 description 1
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- Handcart (AREA)
Abstract
The utility model discloses an electronic foot rest that rises and falls of quick detach, serve lid, lower cover, aircraft including the foot rest and serve lid, hand screw, spring, round pin, steering wheel, support, pendulum rod, the arm of force and foot rest pole, control module, foot rest end is served to cover with the aircraft and all is provided with the draw -in groove, aircraft end cover connection aircraft end, and hand screw packs into in the lid is served to the aircraft, and the spring packs into on the hand screw, and the round pin sets up terminal and can block the upper cover draw -in groove that the aircraft was held and the foot rest is held, two upper covers of pin junction in hand screw, foot rest end pendulum rod and foot rest pole fixed connection. The utility model discloses can pull down the foot rest fast, can increase packaging strength again in order to reduce to pack the volume like this, we can load onto the foot rest fast when using, convenient and fast, and we have increased the power -off protection for the steering wheel simultaneously, adopt mechanical stop spacing simultaneously, have lengthened the life -span of steering wheel promptly, make mechanical motion more stable again, and are reliable, still have rain -proof function simultaneously.
Description
Technical field
The utility model is related to unmanned plane field, and in particular to a kind of Quick Release electric lifting device foot rest.
Background technology
The sale and transport of unmanned plane, because traditional foot rest is often fixed together with aircraft end, it is impossible to simply dismounted,
Also need to just be can be removably mounted by instrument simultaneously, speed is slow and very inconvenient, transport highly difficult, cause cost of transportation very high.
Existing automatic lifting type unmanned plane foot rest, is all single carbon pipe, and bearing capacity is less, and unstable, is not suitable for
For the industrial unmanned plane that carry ability is larger.
Traditional fixed foot rest, typically using old-fashioned bolt connection, disassembles very inconvenient, and packs very big, assembling speed
Degree is slow.
The content of the invention
Technical problem to be solved in the utility model is to provide a kind of solving and commonly use at present holding for electric up-down foot rest
The weak problem of loading capability, by two carbon pipes its bearing capacity is increased, and disclosure satisfy that the demand of the big carry of industrial unmanned plane；And
With quick releasing function, load and unload quick and convenient, quick despatch hardly possible, the unmanned plane transportation and packing volume for solving unmanned plane foot rest is excessive
Problem, means of transportation variation can be realized, reduce cost of transportation, and the Quick Release electric lifting device foot rest of good waterproof performance.
The utility model is achieved through the following technical solutions：A kind of Quick Release electric lifting device foot rest, including foot rest end
Upper lid, lower cover, lid, hand the turn of the screw, spring, pin, steering wheel, support, fork and foot frame rod, control module, foot rest on aircraft end
Draw-in groove is provided with end and aircraft end on lid, aircraft end top cap connects aircraft end, and hand the turn of the screw loads covers on aircraft end
Interior, spring loads in hand the turn of the screw, and pin is arranged at hand the turn of the screw end and can snap in the upper lid draw-in groove at aircraft end and foot rest end
In, the upper lid of pin connection two；
Foot rest end fork is fixedly connected with foot frame rod, lid and lid assembly connection on foot rest end on aircraft end, equipped with foot frame rod
Fork be connected with support, by control module drive steering wheel motion, steering wheel motion drive the arm of force motion with realize foot rest lift, when
Foot rest is elevated to and requires behind position, PCB control modules automatically to steering wheel power-off to protect steering wheel, while being stopped using machinery on the arm of force
Point carries out spacing.
Used as preferred technical scheme, the foot frame rod is provided with two, and is made using carbon pipe.
Used as preferred technical scheme, the steering wheel drives steering wheel by control module, while by unmanned aerial vehicle (UAV) control device control
Drive module processed, steering wheel motion drives the arm of force to move to realize the ascending, descending of foot rest.
Used as preferred technical scheme, the steering wheel has automatic power-off protection circuit and rainproof function.
The beneficial effects of the utility model are：1st, using double carbon pipes, relatively current single carbon pipe on the market, load capacity is big
It is big to strengthen, at the same it is more steady and the utility model has water-proof function, even if using in rainy weather, also do not affect；
2nd, quick releasing function can well solve this problem, and when packaged we can quickly pull down foot rest, so i.e.
Packaging volume can be reduced, packaging intensity can be increased again, when in use we quickly can load onto foot rest, convenient and swift；
3rd, using symmetrical double carbon tubular constructions, its bearing capacity is greatly improved, while also more steady, and on the market automatic
Lifting foot rest does not possess quick releasing function, assembles and transport not convenient, and the utility model adopts Quick Release mode, assembly and disassembly facility, packaging
Volume is also less.
Description of the drawings
In order to be illustrated more clearly that the utility model embodiment or technical scheme of the prior art, below will be to embodiment
Or the accompanying drawing to be used needed for description of the prior art is briefly described, it should be apparent that, drawings in the following description are only
It is some embodiments of the present utility model, for those of ordinary skill in the art, in the premise for not paying creative work
Under, can be with according to these other accompanying drawings of accompanying drawings acquisition.
Fig. 1 is structural representation of the present utility model.
Specific 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 by any way.
Any feature disclosed in this specification (including any accessory claim, summary and accompanying drawing), except non-specifically is chatted
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, including lid 2, hand the turn of the screw 3, spring 4, pin 5, steering wheel 6, support on lid 1 on foot rest end, aircraft end
7th, the arm of force 8, fork 9 and foot frame rod 10, draw-in groove is provided with foot rest end on lid 1 and aircraft end on lid 2, and lid 1 connects on aircraft end
Aircraft end is connect, hand the turn of the screw 3 loads on aircraft end in lid 2, and spring 4 loads in hand the turn of the screw, and pin 5 is arranged at hand the turn of the screw
End simultaneously can be snapped on foot rest end and aircraft end in two draw-in grooves of lid, and pin 5 connects and covered on the two；
Lid 1 is connected with support 7 on foot rest end, while be also fixedly connected with foot frame rod 10, on aircraft end on lid 2 and foot rest end
The assembly connection of lid 1, steering wheel 6 is installed in support 7, and support 7 is connected with lid 1 on foot rest end, and the arm of force 8 is driven by steering wheel 6, is realized
Foot rest elevating movement, foot frame rod is fixed on fork 9, and fork is connected with support, realizes foot rest elevating movement.
In the present embodiment, foot frame rod 10 is provided with two, and is made using carbon pipe, using double carbon pipes, relatively current market
On single carbon pipe, load capacity greatly enhances, while more steady and the utility model has water-proof function, even if raining
Weather is used, and is not also affected.
Wherein, the steering wheel drives steering wheel by control module, while controlling drive module, steering wheel by unmanned aerial vehicle (UAV) control device
Motion drives the arm of force to move to realize the ascending, descending of foot rest.
Steering wheel has automatic power-off protection circuit, and when foot rest rising stem is to the position for arranging, our steering wheel is just from dynamic circuit breaker
Electricity, limits foot rest position angle by the way of mechanical stop, i.e., safe, and reliable.
During installation, hand the turn of the screw being pulled first, making pin move to the other end, at this moment spring is compressed, then by foot rest
Lid draw-in groove on the draw-in groove alignment aircraft end of end, cooperation is entered, and unclamps hand the turn of the screw, sells homing under spring force, will be upper
Lower cover connects, and completes to install.During dismounting, hand the turn of the screw, pin is pulled to move to the other end, foot rest end automatically disengages, and completes dismounting.
The utility model solves the problems, such as that the bearing capacity for commonly using electric up-down foot rest at present is weak, is increased by two carbon pipes
Plus its bearing capacity, disclosure satisfy that the demand of the big carry of industrial unmanned plane；And with quick releasing function, load and unload quick and convenient, solution
Determine the problem that quick despatch is difficult, unmanned plane transportation and packing volume is excessive of unmanned plane foot rest, can realize that means of transportation is various
Change, reduce cost of transportation.Waterproofing design is considered in design, with water-proof function, disclosure satisfy that unmanned plane in special operation condition
Under job requirements.
The beneficial effects of the utility model are：1st, using double carbon pipes, relatively current single carbon pipe on the market, load capacity is big
It is big to strengthen, at the same it is more steady and the utility model has water-proof function, even if using in rainy weather, also do not affect；
2nd, quick releasing function can well solve this problem, and when packaged we can quickly pull down foot rest, so i.e.
Packaging volume can be reduced, packaging intensity can be increased again, when in use we quickly can load onto foot rest, convenient and swift；
3rd, using symmetrical double carbon tubular constructions, its bearing capacity is greatly improved, while also more steady, and on the market automatic
Lifting foot rest does not possess quick releasing function, assembles and transport not convenient, and the utility model adopts Quick Release mode, assembly and disassembly facility, packaging
Volume is also less.
The above, specific embodiment only of the present utility model, but protection domain of the present utility model do not limit to
In this, any change or replacement expected without creative work all should be covered within protection domain of the present utility model.
Therefore, the protection domain that protection domain of the present utility model should be limited by claims is defined.
Claims (4)
1. a kind of Quick Release electric lifting device foot rest, it is characterised in that：Including lid, hand on lid on the foot rest end of foot rest end, lower cover, aircraft end
On the turn of the screw, spring, pin, steering wheel, support, fork, the arm of force and foot frame rod, control module, foot rest end and aircraft end on lid all
It is provided with draw-in groove；
Aircraft end top cap connects aircraft end, and hand the turn of the screw loads covers interior on aircraft end, and spring loads in hand the turn of the screw, and pin sets
It is placed in hand the turn of the screw end and can snaps in the upper lid draw-in groove at aircraft end and foot rest end, the upper lid of pin connection two；
Foot rest end fork is fixedly connected with foot frame rod, lid and lid assembly connection on foot rest end, the pendulum equipped with foot frame rod on aircraft end
Bar is connected with support, drives steering wheel motion, steering wheel motion to drive arm of force motion to lift to realize foot rest, work as foot rest by control module
It is elevated to and requires behind position, PCB control modules are automatically to steering wheel power-off to protect steering wheel, while is entered using mechanical stop on the arm of force
Row is spacing.
2. Quick Release electric lifting device foot rest as claimed in claim 1, it is characterised in that：The foot frame rod is provided with two, and adopts
Made with carbon pipe.
3. Quick Release electric lifting device foot rest as claimed in claim 1, it is characterised in that：The steering wheel drives rudder by control module
Machine, while controlling drive module by unmanned aerial vehicle (UAV) control device, steering wheel motion drives the arm of force to move to realize the lifting of foot rest.
4. the Quick Release electric lifting device foot rest as described in claim 1 or 3, it is characterised in that：The steering wheel have automatically power off guarantor
Protection circuit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621078913.6U CN206087269U (en) | 2016-09-26 | 2016-09-26 | Electronic foot rest that rises and falls of quick detach |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621078913.6U CN206087269U (en) | 2016-09-26 | 2016-09-26 | Electronic foot rest that rises and falls of quick detach |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206087269U true CN206087269U (en) | 2017-04-12 |
Family
ID=58479589
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621078913.6U Expired - Fee Related CN206087269U (en) | 2016-09-26 | 2016-09-26 | Electronic foot rest that rises and falls of quick detach |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206087269U (en) |
-
2016
- 2016-09-26 CN CN201621078913.6U patent/CN206087269U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170412 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |