CN108248887A - One kind emits equipment for small drone - Google Patents
One kind emits equipment for small drone Download PDFInfo
- Publication number
- CN108248887A CN108248887A CN201810060015.5A CN201810060015A CN108248887A CN 108248887 A CN108248887 A CN 108248887A CN 201810060015 A CN201810060015 A CN 201810060015A CN 108248887 A CN108248887 A CN 108248887A
- Authority
- CN
- China
- Prior art keywords
- lock body
- closing piece
- small drone
- pedestal
- rod
- 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.)
- Pending
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Launching or towing gear
- B64F1/06—Launching or towing gear using catapults
Abstract
Emit equipment the invention discloses one kind for small drone,Including pedestal,Transmitting station,Retaining mechanism and controller,The base top is provided with spring normal thereto,The top of spring is provided with transmitting station,Retaining mechanism includes the first lock body,Second lock body,Lifting power plant and electromagnetic control apparatus,The lifting power plant is fixedly mounted on pedestal,The driving axis connection of first lock body and lifting power plant,The bottom surface of transmitting station is equipped with square groove,Square groove side is provided with blind hole,Second lock body one end is hinged on transmitting station,Dynamic clamping head and quiet clamping head is placed in blind hole,One end of dynamic clamping head and quiet clamping head is connect with the second lock body,First lock body and the mutually close one end of the second lock body are respectively fixed with the first closing piece and the second closing piece,Electromagnetic Control mechanism is provided on first lock body,It is simple that the present invention improves mechanism,Use cost is low.
Description
Technical field
The present invention relates to unmanned plane lift-off technology fields more particularly to a kind of small drone that is used for emit equipment.
Background technology
At present, taking off for small drone mainly uses two ways：Hand is thrown and ejection.Winged mode is thrown for hand,
It is difficult to ensure that normal posture when unmanned plane takes off, easily fails.Ejection mode is all using vehicle-mounted or fixed, is not easy to
It carries and advances in complexity, it is difficult to reach best launch site, there is larger limit for the performance for giving full play to unmanned plane
System, in addition, unmanned plane vehicle transmitting electromagnetism unlocking mechanism has higher reliability, use cost is low, easy to operate, is recycled
It uses.Previous vehicle transmitting is unlocked using electric detonator mechanism, but the unlocking mechanism use cost is higher, and electric detonator is
Priming system, expensive, the purchase means of transportation of electric detonator has more strict requirements;Electric detonator is disposable products, transmitting
It need to once be re-replaced, it is impossible to be recycled.
Invention content
To solve the above-mentioned problems, the present invention proposes that a kind of small drone simple in structure, that use cost is low that is used for is sent out
Jet device.
Specifically, a kind of emit equipment for small drone, including pedestal, transmitting station, retaining mechanism and controller, institute
The base top stated is provided with spring normal thereto, and spring is in compressive state, and the top of the spring is provided with transmitting
Platform, the retaining mechanism include the first lock body, the second lock body, lifting power plant and electromagnetic control apparatus, and the lifting is dynamic
Power apparatus is fixedly mounted on pedestal, and first lock body and the second lock body are rod like parts, and the rod like parts section is square,
The driving axis connection of first lock body and lifting power plant, the bottom surface of transmitting station are equipped with square groove, and square groove side is provided with blind
Hole, the second described lock body one end are hinged on transmitting station, and the second lock body passes through the square groove, is placed in the blind hole
Dynamic clamping head and quiet clamping head, one end of dynamic clamping head and quiet clamping head are connect with the second lock body, first lock body and the second lock body it is mutually close one
End is respectively fixed with the first closing piece and the second closing piece, and first lock body and the second lock body are block, first closing piece,
The length of second closing piece be respectively greater than the first lock body, the second lock body section length, and the first closing piece right side and the first lock body
Right side be in same perpendicular, the left side of the second closing piece left side and the second lock body is in same vertical flat
In face, the upper left end face of first closing piece and the right lower end surface of the second closing piece are curved surface, during locking, the following table of the first closing piece
Face is in contact with the upper surface of the second closing piece, and Electromagnetic Control mechanism, the Electromagnetic Control are provided on first lock body
Device includes control-rod, and the transverse projection of the control-rod is in the upper right the vertical side face of the second closing piece；
Oil cylinder, servo motor and drill bit are further included, the oil cylinder is fitted vertically mounted on the bottom of pedestal, and servo motor is fixed
On the piston rod of oil cylinder, it is equipped on the output shaft of servo motor for the drill bit on drilling stratum.
The lifting power plant, electromagnetic control apparatus are all connect with controller.
The base end face is provided with leveling stent.
The length of the square groove is more than the cross-sectional width of the second lock body.
First lock body is provided with the mounting groove of electromagnetic control apparatus.
The control-rod collapsing length is more than the contact surface length of the first closing piece and the second closing piece.
The lifting power plant is hydraulic cylinder or pneumatic cylinder.
The beneficial effects of the present invention are：Using the radiation pattern of ejection, ensure correct posture when unmanned plane takes off, send out
Before penetrating, the first lock body moves up, and before closing piece under the action of end curved surface and dynamic clamping head and quiet clamping head, retaining mechanism is made to rapidly enter lock
Tight mechanism, and lifting power plant drives transmitting station to move down, and spring is made to be in compressive state, during transmitting, control-rod pushes away
Dynamic second closing piece is to left movement, and so as to fulfill unlock, structure is simpler compared with prior art and can be dropped with repeat its transmission
Low use cost.
Description of the drawings
Fig. 1 is for the structure diagram of small drone transmitting equipment；
Fig. 2 is for the enlarged drawing of small drone transmitting device A；
1- pedestals in figure, 2- transmitting stations, the first lock bodies of 3-, the second lock bodies of 4-, 5- lifting power plants, 6- electromagnetic control apparatus,
7- dynamic clamping head and quiet clamping heads, 8- curved surfaces, 9- control-rods, 10- oil cylinders.
Specific embodiment
For a clearer understanding of the technical characteristics, objects and effects of the present invention, now control illustrates this hair
Bright specific embodiment.
As shown in Figure 1, a kind of emit equipment for small drone, including pedestal 1, transmitting station 2, retaining mechanism and control
Device, 1 top of pedestal is provided with spring normal thereto, and spring is in compressive state, the top setting of the spring
There is transmitting station 2, the retaining mechanism includes the first lock body 3, the second lock body 4, lifting power plant 5 and electromagnetic control apparatus 6,
The lifting power plant 5 is fixedly mounted on pedestal 1, and first lock body 3 and the second lock body 4 are rod like parts, the bar
Shape part section is square, and the driving axis connection of the first lock body 3 and lifting power plant 5, the bottom surface of transmitting station 2 is equipped with square groove,
Square groove side is provided with blind hole, and described 4 one end of the second lock body is hinged on transmitting station 2, and the second lock body 4 passes through the side
Shape slot is placed with dynamic clamping head and quiet clamping head 7 in the blind hole, and one end of dynamic clamping head and quiet clamping head 7 is connect with the second lock body 4.
As shown in Fig. 2, first lock body 3 one end mutually close with the second lock body 4 be respectively fixed with the first closing piece and
Second closing piece, first lock body 3 and the second lock body 4 are block, and first closing piece, the length difference of the second closing piece are big
Length in the first lock body 3,4 section of the second lock body, and the first closing piece right side and the right side of the first lock body 3 be in it is same
In perpendicular, the second closing piece left side and the left side of the second lock body 4 are in same perpendicular, first closing piece
Upper left end face and the right lower end surface of the second closing piece be curved surface 8, during locking, the lower surface of the first closing piece is upper with the second closing piece
Surface is in contact, and Electromagnetic Control mechanism is provided on first lock body 3, and the electromagnetic control apparatus 6 includes control-rod
9, the transverse projection of the control-rod 9 is in the upper right the vertical side face of the second closing piece.
As shown in Figure 1, the lifting power plant 5, electromagnetic control apparatus 6 are all connect with controller.The pedestal 1
Bottom surface is provided with leveling stent.The length of the square groove is more than the cross-sectional width of the second lock body 4.First lock body 3
It is provided with the mounting groove of electromagnetic control apparatus 6.9 collapsing length of control-rod is more than the contact with the second closing piece of the first closing piece
Face length.The lifting power plant 5 is hydraulic cylinder or pneumatic cylinder.As shown in Figure 1, a kind of set for small drone transmitting
It is standby, oil cylinder 10, servo motor and drill bit are further included, the oil cylinder 10 is fitted vertically mounted on the bottom of pedestal 1, servo motor
It is fixed on the piston rod of oil cylinder 10, is equipped on the output shaft of servo motor for the drill bit on drilling stratum, make transmitting equipment
More stablize.
The course of work of the present invention is as follows：Before unmanned plane transmitting, lifting power plant 5 pushes the first lock body to move up,
When the first closing piece and the second closing piece close to when, the second lock body 4 rotates around hinge joint, and the first closing piece and the second closing piece edge
Curved face contact slides, when two closing pieces are staggered, under the action of dynamic clamping head and quiet clamping head 7, and the lower surface of the first closing piece and the second lock
The upper surface of block is in contact, and so as to fulfill locking, then lifting power plant 5 pulls transmitting station to move downwardly together, makes spring
In compressive state, the piston rod of 1 bottom of pedestal moves down, and servo motor is started to work, and drill bit is made to pierce ground；Unmanned plane
During transmitting, controller sends out instruction, and control-rod 9 is made to push the second lock body 4 to the left, realizes unlock transmitting.
Claims (7)
1. one kind emits equipment for small drone, which is characterized in that including pedestal（1）, transmitting station（2）, retaining mechanism and
Controller, the pedestal（1）Top is provided with spring normal thereto, and spring is in compressive state, the top of the spring
End is provided with transmitting station（2）, the retaining mechanism includes the first lock body（3）, the second lock body（4）, lifting power plant（5）With
Electromagnetic control apparatus（6）, the lifting power plant（5）It is fixedly mounted on pedestal（1）On, first lock body（3）With
Two lock bodies（4）For rod like parts, the rod like parts section is square, the first lock body（3）With lifting power plant（5）Drive shaft connect
It connects, transmitting station（2）Bottom surface be equipped with square groove, square groove side is provided with blind hole, second lock body（4）One end is hinged on
Transmitting station（2）On, and the second lock body（4）Across the square groove, dynamic clamping head and quiet clamping head is placed in the blind hole（7）, elasticity is again
Position part（7）One end and the second lock body（4）Connection, first lock body（3）With the second lock body（4）Mutually close one end difference
It is fixed with the first closing piece and the second closing piece, first lock body（3）With the second lock body（4）For block, first closing piece,
The length of second closing piece is respectively greater than the first lock body（3）, the second lock body（4）The length in section, and the first closing piece right side and the
One lock body（3）Right side be in same perpendicular, the second closing piece left side and the second lock body（4）Left side be in
In same perpendicular, the upper left end face of first closing piece and the right lower end surface of the second closing piece are curved surface（8）, locking
When, the lower surface of the first closing piece is in contact with the upper surface of the second closing piece, first lock body（3）On be provided with Electromagnetic Control
Mechanism, the electromagnetic control apparatus（6）Including control-rod（9）, the control-rod（9）Transverse projection on the right side of the second closing piece
In upper the vertical side face；
Further include oil cylinder（10）, servo motor and drill bit, the oil cylinder（10）It is fitted vertically mounted on pedestal（1）Bottom,
Servo motor is fixed on oil cylinder（10）Piston rod on, be equipped on the output shaft of servo motor for the drill bit on drilling stratum.
It is 2. according to claim 1 a kind of for small drone transmitting equipment, which is characterized in that the lifting drive
Device（5）, electromagnetic control apparatus（6）All it is connect with controller.
It is 3. according to claim 1 a kind of for small drone transmitting equipment, which is characterized in that the pedestal（1）
Bottom surface is provided with leveling stent.
It is 4. according to claim 1 a kind of for small drone transmitting equipment, which is characterized in that the square groove
Length is more than the second lock body（4）Cross-sectional width.
It is 5. according to claim 1 a kind of for small drone transmitting equipment, which is characterized in that first lock body
（3）It is provided with electromagnetic control apparatus（6）Mounting groove.
It is 6. according to claim 1 a kind of for small drone transmitting equipment, which is characterized in that the control-rod
（9）Collapsing length is more than the contact surface length of the first closing piece and the second closing piece.
It is 7. according to claim 1 a kind of for small drone transmitting equipment, which is characterized in that the lifting drive
Device（5）For hydraulic cylinder or pneumatic cylinder.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810060015.5A CN108248887A (en) | 2018-01-22 | 2018-01-22 | One kind emits equipment for small drone |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810060015.5A CN108248887A (en) | 2018-01-22 | 2018-01-22 | One kind emits equipment for small drone |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108248887A true CN108248887A (en) | 2018-07-06 |
Family
ID=62741669
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810060015.5A Pending CN108248887A (en) | 2018-01-22 | 2018-01-22 | One kind emits equipment for small drone |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108248887A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109911235A (en) * | 2019-04-17 | 2019-06-21 | 成都航空职业技术学院 | A kind of unmanned aerial vehicle ejecting buffer protection device |
| CN110924897A (en) * | 2019-12-24 | 2020-03-27 | 黑龙江北方双佳钻采机具有限责任公司 | Drilling tool stabilizer strutting arrangement |
| CN112660407A (en) * | 2021-01-13 | 2021-04-16 | 陆颖怡 | High-pressure pneumatic boosting take-off device of light unmanned aerial vehicle |
-
2018
- 2018-01-22 CN CN201810060015.5A patent/CN108248887A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109911235A (en) * | 2019-04-17 | 2019-06-21 | 成都航空职业技术学院 | A kind of unmanned aerial vehicle ejecting buffer protection device |
| CN109911235B (en) * | 2019-04-17 | 2020-11-17 | 成都航空职业技术学院 | Buffering protection device for unmanned aerial vehicle ejection |
| CN110924897A (en) * | 2019-12-24 | 2020-03-27 | 黑龙江北方双佳钻采机具有限责任公司 | Drilling tool stabilizer strutting arrangement |
| CN112660407A (en) * | 2021-01-13 | 2021-04-16 | 陆颖怡 | High-pressure pneumatic boosting take-off device of light unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180706 |
|
| WD01 | Invention patent application deemed withdrawn after publication |