CN206183986U - Ware is put in to light -duty fast -assembling model aeroplane and model ship - Google Patents
Ware is put in to light -duty fast -assembling model aeroplane and model ship Download PDFInfo
- Publication number
- CN206183986U CN206183986U CN201621163999.2U CN201621163999U CN206183986U CN 206183986 U CN206183986 U CN 206183986U CN 201621163999 U CN201621163999 U CN 201621163999U CN 206183986 U CN206183986 U CN 206183986U
- Authority
- CN
- China
- Prior art keywords
- outer end
- sub
- model
- connecting rod
- latch
- 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
Landscapes
- Toys (AREA)
Abstract
The utility model provides a ware is put in to light -duty fast -assembling model aeroplane and model ship, includes main brace pole and sub -strut pole, and sub -strut pole slidable mounting installs top pressure spring between main brace pole and the sub -strut pole in the main brace pole, and the jack catch is installed respectively to the outer end of main brace pole and sub -strut pole, being fixed with the mounting panel on the main brace pole, installing the steering wheel on the mounting panel, the rocking arm is installed to drive shaft on the steering wheel, and the outer end of rocking arm is rotated and is connected with the connecting rod, and the outer end of connecting rod is connected with the bolt, is equipped with the installation piece that the interval set up about a pair of on the mounting panel, and the installation piece is gone up to open has the perforation that supplies the bolt to pass.
Description
Technical field
The utility model is related to, more particularly to a kind of Light-duty Quick-installation model plane dispenser.
Background technology
At present, in recent years, remote controlled model plane Development of UAV is swift and violent, although head is little, but flying speed is fast, and mobility is good,
Energy VTOL, is suitable for various terrain environments, and in addition to as worldwide toy, unmanned plane is also widely used in business
Industry field, wherein air-drop function is widely applied, for example, drops lifebuoy rescue drowning people, air-drop courier packages, air-drop
Exploitation, air-drop novelties etc., the case of all existing a large amount of practical applications.
Unmanned plane will realize the function of air-drop, it is necessary to install dispenser this sleeve piece additional.Dispenser currently on the market is most
It is metal structure, and is coupled with unmanned plane underlying holder by screw, major defect is larger weight, installs complicated, it is impossible to
Fast assembling-disassembling is realized, as one threshold that amateur's contact is used.
Utility model content
The utility model will solve the problems, such as above-mentioned prior art, there is provided a kind of Light-duty Quick-installation model plane dispenser, lead to
Cross spring and strut strut, the claw of dispenser is compressed the mounting bracket of unmanned plane and is realized fixing, without any work during installation
Tool, can complete installation and debugging in one minute.
The utility model solves the technical scheme of its technical problem use:This Light-duty Quick-installation model plane dispenser, including master
Strut and sub-strut bar, sub-strut bar are slidably mounted in main supporting rod, and top pressure spring, main supporting rod are provided between main supporting rod and sub-strut bar
Outer end with sub-strut bar is separately installed with claw;Installing plate is fixed with main supporting rod, steering wheel is installed, on steering wheel on installing plate
Drive shaft is provided with rocking arm, and the outer end of rocking arm is rotatably connected to connecting rod, and the outer end of connecting rod is connected with latch, and installing plate is provided with one
To the spaced mounting blocks in left and right, the perforation passed through for latch is provided with mounting blocks.
In order to further perfect, the mounting groove loaded for steering wheel is provided with installing plate, the left and right sides of steering wheel outer end is provided with
Fixed edge, fixed edge with corresponding fixing hole is separately installed with installing plate.
It is further perfect, abutment sleeve is installed on the left of perforation.
Further perfect, by short pin connection between rocking arm and connecting rod, the inner of latch is provided with groove, and connecting rod outer end is placed in
Latch is connected in groove and by having strong market potential inner.
The utility model has the advantages that:The utility model (1) delivery device compact conformation, easy to use, Neng Gouan
Entirely, stabilization carry article and realize safe air-drop;(2) dispenser is realized fast with unmanned plane using spring spacer bar compression claw
Speed is fixed, simplifies installation process, improves installation effectiveness;(3) it is lightweight, reduce unmanned plane and bear a heavy burden, be conducive to improving unmanned plane
Effective heavy burden, mobility and voyage.
Brief description of the drawings
Fig. 1 be the utility model in latch insert in perforation in structural representation;
Fig. 2 be the utility model in latch leave perforation in structural representation;
Fig. 3 is explosive view of the present utility model;
Fig. 4 is scheme of installation of the present utility model.
Description of reference numerals:Main supporting rod 1, sub-strut bar 2, top pressure spring 3, claw 4, installing plate 5, mounting groove 5-1, steering wheel 6,
Fixed edge 6-1, rocking arm 7, connecting rod 8, latch 9, groove 9-1, mounting blocks 10, perforate 10-1, and fixing hole 11, abutment sleeve 12 is short
Pin 13, has strong market potential 14.
Specific embodiment
The utility model is described in further detail below in conjunction with the accompanying drawings:
Referring to the drawings:Light-duty Quick-installation model plane dispenser in the present embodiment, including main supporting rod 1 and sub-strut bar 2, sub-strut bar 2 are slided
It is dynamic to be installed in main supporting rod 1, the outer end of top pressure spring 3, main supporting rod 1 and sub-strut bar 2 is installed between main supporting rod 1 and sub-strut bar 2
It is separately installed with claw 4;Installing plate 5 is fixed with main supporting rod 1, steering wheel 6 is installed on installing plate 5, the drive shaft peace on steering wheel 6
Equipped with rocking arm 7, the outer end of rocking arm 7 is rotatably connected to connecting rod 8, and the outer end of connecting rod 8 is connected with latch 9, and installing plate 5 is provided with a pair
The spaced mounting blocks 10 in left and right, are provided with the perforation 10-1 passed through for latch 9 on mounting blocks 10.
The mounting groove 5-1 loaded for steering wheel 6 is wherein provided with installing plate 5, the left and right sides of the outer end of steering wheel 6 is provided with fixed edge
Corresponding fixing hole 11 is separately installed with 6-1, fixed edge 6-1 and installing plate 5-1.Positioning is installed on the left of perforation 10-1
Sleeve 12.Connected by short pin 13 between rocking arm 7 and connecting rod 8, the inner of latch 9 is provided with groove 9-1, and the outer end of connecting rod 8 is placed in recessed
To be connected to latch 9 inner in groove 9-1 and by having strong market potential 14.
The dispenser overall structure is as shown in Figure 1:The left end of spring 3 and sub-strut bar 2 can be accommodated in the cylinder of main supporting rod 1,
Axially pressing major and minor strut with hand can shorten strut overall length, recover former long after letting go;Latch 9 inserts wearing for the upper right side of installing plate 5
In the 10-1 of hole, the article of UAV flight is to hang on latch 9 herein.Perforation 10-1 left sides are provided with abutment sleeve 12, and extension is worn
Hole 10-1 length, play the guiding role, it is ensured that keep coaxial with perforation 10-1 when latch 9 is moved;The rotational band motion rocker arm 7 of steering wheel 6 is put
Dynamic, the outer end of rocking arm 7 pulls connecting rod 8, traction latch 9 to be axially moveable.
The operating principle of the dispenser releasing is as shown in Figure 2:Operator's control steering wheel 6 is rotated counterclockwise, and band shakes
The counter-clockwise swing of arm 7, to Zola's connecting rod 8, so that latch 9 is moved to left, the perforation 10-1 from mounting blocks 10 is extracted, and hangs over latch
Article on 9 falls because of gravity immediately.
Dispenser is shown in Fig. 4 with the installation of unmanned plane.The installation of the dispenser is very easy:Make the claw 4 of the left end of main supporting rod 1
The horizontal stand of unmanned plane lower left is blocked, sub-strut bar is held and is applied pressure and shorten strut overall length, make sub-strut bar right-hand member
Claw 4 is directed at the horizontal stand of unmanned plane lower right, and after letting go, spring 3 releases sub-strut bar 2, claw 4 is blocked the water on right side
Flat support is to complete to install.Delivery device simple structure, with low cost, realization for the air-drop of model plane carry of the present utility model
Fast and reliable installation, part is few, lightweight, is conducive to improving the payload and mobility of unmanned plane.
Although the utility model is shown and described by reference to preferred embodiment, this specialty is common
Technical staff is it is to be appreciated that in the range of claims, can make the various change in form and details.
Claims (4)
1. a kind of Light-duty Quick-installation model plane dispenser, including main supporting rod (1) and sub-strut bar (2), it is characterized in that:The sub-strut bar (2)
It is slidably mounted in main supporting rod (1), top pressure spring (3), main supporting rod (1) and pair is installed between main supporting rod (1) and sub-strut bar (2)
The outer end of strut (2) is separately installed with claw (4);Installing plate (5) is fixed with the main supporting rod (1), is installed on installing plate (5)
There is steering wheel (6), the drive shaft on steering wheel (6) is provided with rocking arm (7), and the outer end of rocking arm (7) is rotatably connected to connecting rod (8), connecting rod
(8) outer end is connected with latch (9), and the installing plate (5) is provided with a pair or so spaced mounting blocks (10), mounting blocks
(10) perforation (10-1) passed through for latch (9) is provided with.
2. Light-duty Quick-installation model plane dispenser according to claim 1, it is characterized in that:It is provided with the installing plate (5) and supplies rudder
The mounting groove (5-1) that machine (6) loads, the left and right sides of steering wheel (6) outer end is provided with fixed edge (6-1), fixed edge (6-1) and installation
Corresponding fixing hole (11) is separately installed with plate (5).
3. Light-duty Quick-installation model plane dispenser according to claim 1, it is characterized in that:Install in the left side of the perforation (10-1)
There is abutment sleeve (12).
4. Light-duty Quick-installation model plane dispenser according to claim 1, it is characterized in that:Between the rocking arm (7) and connecting rod (8)
Connected by short pin (13), the inner of the latch (9) is provided with groove (9-1), and connecting rod (8) outer end is placed in groove (9-1)
In and by having strong market potential, (14) to be connected to latch (9) inner.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621163999.2U CN206183986U (en) | 2016-11-01 | 2016-11-01 | Ware is put in to light -duty fast -assembling model aeroplane and model ship |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201621163999.2U CN206183986U (en) | 2016-11-01 | 2016-11-01 | Ware is put in to light -duty fast -assembling model aeroplane and model ship |
Publications (1)
Publication Number | Publication Date |
---|---|
CN206183986U true CN206183986U (en) | 2017-05-24 |
Family
ID=58733371
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201621163999.2U Expired - Fee Related CN206183986U (en) | 2016-11-01 | 2016-11-01 | Ware is put in to light -duty fast -assembling model aeroplane and model ship |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN206183986U (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108328353A (en) * | 2018-02-28 | 2018-07-27 | 上海拓攻机器人有限公司 | A kind of movable type logistics conveyer system |
CN113022879A (en) * | 2021-05-17 | 2021-06-25 | 南京航天国器智能装备有限公司 | Follow car and tie unmanned aerial vehicle and keep away barrier system |
-
2016
- 2016-11-01 CN CN201621163999.2U patent/CN206183986U/en not_active Expired - Fee Related
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN108328353A (en) * | 2018-02-28 | 2018-07-27 | 上海拓攻机器人有限公司 | A kind of movable type logistics conveyer system |
CN113022879A (en) * | 2021-05-17 | 2021-06-25 | 南京航天国器智能装备有限公司 | Follow car and tie unmanned aerial vehicle and keep away barrier system |
CN113022879B (en) * | 2021-05-17 | 2021-09-14 | 南京航天国器智能装备有限公司 | Follow car and tie unmanned aerial vehicle and keep away barrier system |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN206183986U (en) | Ware is put in to light -duty fast -assembling model aeroplane and model ship | |
CN102556336A (en) | Wing fast unfolding device for folding-wing unmanned plane | |
CN207191432U (en) | Rescue four rotor wing unmanned aerial vehicles in a kind of public security waters | |
CN205059994U (en) | A horn folding device for aircraft | |
CN205906203U (en) | H type structure can two -way deformation unmanned aerial vehicle | |
CN203698652U (en) | Undercarriage of unmanned aerial vehicle | |
CN110393390B (en) | Earthquake self-rescue bed | |
CN205022845U (en) | A horn folding device for aircraft | |
CN208233352U (en) | One kind using buffer unit based on unmanned plane landing | |
CN201012291Y (en) | Kite | |
CN205022841U (en) | A horn folding device for aircraft | |
CN107117291B (en) | Helping hand transportation foot rest and have unmanned aerial vehicle of this foot rest | |
CN107031874A (en) | A kind of space non-cooperative target instantaneously triggered grabs adsorption device | |
CN207274965U (en) | A kind of detachable walker of unmanned helicopter | |
CN210391546U (en) | Unmanned aerial vehicle descending device | |
CN207737514U (en) | A kind of main wing splicing assembly jig | |
CN208746229U (en) | A kind of Novel model airplane aircraft | |
CN102674175A (en) | Self-adaptive crane auto-locked by gravity | |
CN207840786U (en) | A kind of quick release tooling | |
CN206163564U (en) | Battery quick assembly disassembly positioning locking device | |
CN211391671U (en) | Unmanned aerial vehicle descending mechanism | |
CN212448161U (en) | Unmanned aerial vehicle control parameter debugging frame | |
CN209380639U (en) | A kind of specific purpose tool of assist removal rivet | |
CN107719674B (en) | Intelligent unmanned aerial vehicle for student who possesses vertical take-off and landing function | |
CN208855858U (en) | Quick disassembled formula horizontal tail attachment device |
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: 20170524 Termination date: 20191101 |
|
CF01 | Termination of patent right due to non-payment of annual fee |