CN108791884A - Unmanned plane delivery device and unmanned plane with the unmanned plane device delivery device - Google Patents
Unmanned plane delivery device and unmanned plane with the unmanned plane device delivery device Download PDFInfo
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- CN108791884A CN108791884A CN201810696596.1A CN201810696596A CN108791884A CN 108791884 A CN108791884 A CN 108791884A CN 201810696596 A CN201810696596 A CN 201810696596A CN 108791884 A CN108791884 A CN 108791884A
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- unmanned plane
- delivery device
- pilot hole
- pedestal
- lever
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 36
- 230000002265 prevention Effects 0.000 claims abstract description 9
- 230000002035 prolonged effect Effects 0.000 claims 1
- 238000000034 method Methods 0.000 abstract description 2
- 230000033001 locomotion Effects 0.000 description 6
- 238000010586 diagram Methods 0.000 description 4
- 230000007246 mechanism Effects 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 2
- 238000004891 communication Methods 0.000 description 1
- 230000034994 death Effects 0.000 description 1
- 231100000517 death Toxicity 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 238000013507 mapping Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012544 monitoring process Methods 0.000 description 1
- 230000002093 peripheral effect Effects 0.000 description 1
- 238000011160 research Methods 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 230000004584 weight gain Effects 0.000 description 1
- 235000019786 weight gain Nutrition 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D1/00—Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight
- B64D1/02—Dropping, ejecting, or releasing articles
- B64D1/08—Dropping, ejecting, or releasing articles the articles being load-carrying devices
- B64D1/12—Releasing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transmission Devices (AREA)
Abstract
The invention discloses unmanned plane delivery device and the unmanned plane with the unmanned plane device delivery device, belong to air vehicle technique field.Including actuator, actuator seat, pedestal, driving lever and release lever；The central axes of pilot hole are overlapped with the central axes of drive shaft, and the inner wall of pilot hole is equipped with the rotation prevention portion extended along pilot hole length direction, and dispensing port opening down is simultaneously connected to pilot hole；Unlocking lever tube is connected on driving lever, and is screwed togather with driving lever, and release lever is slidably inserted in the pilot hole of pedestal, the outer wall of release lever is equipped with limiting section, one of limiting section and rotation prevention portion are raised line, and another is limiting slot, and raised line is slidably contained in limiting slot.The goal of the invention of the present invention is to provide a kind of unmanned plane delivery device, and the equipment safety is high, is clamped and stablizes to heavy load, can solve the problems, such as that vibration or actuator during unmanned plane during flying damage due to missile caused to fall.
Description
Technical field
Dress is launched the invention belongs to air vehicle technique field, especially unmanned plane delivery device and with the unmanned plane device
The unmanned plane set.
Background technology
As China deepens continuously to the research of unmanned aircraft, the scope of application of unmanned aircraft is also increasingly expanded
Exhibition, the function that unmanned aircraft has is also stronger and stronger, military attack, monitoring, communication, mapping, disaster relief etc..It is right
In at present, existing unmanned plane delivery device, principle are born using four-bar mechanism, delivery device load heavy type on the market
When load, the frictional force of release lever and pedestal is very big, and the actuator of low-power can not be dragged, and missile can not be released, and
The defects of serious power consumption, weight gain can be carried when changing high-power actuator into.And work as unmanned plane in flight course, it can
It can cause falling for missile because vibration or actuator damage make release lever detach pedestal, cause unnecessary loss, very
To injures and deaths.
Invention content
The goal of the invention of the present invention is to provide unmanned plane delivery device and nobody with the unmanned plane device delivery device
Machine, the delivery device is safe, is clamped and stablizes to heavy load, vibration during capable of solving because of unmanned plane during flying or
The problem of actuator damages and missile is caused to fall.
In order to achieve the above objectives, the technical solution adopted in the present invention is：
A kind of unmanned plane delivery device, which is characterized in that including
Actuator seat；
Actuator, including driving ontology and with the drive shaft that connect of driving ontology, the driving ontology is installed in institute
It states on actuator seat；
Pedestal, the pedestal are connect with the actuator seat, and pilot hole and dispensing port are offered on the pedestal, described to lead
It is overlapped to the central axes in hole with the central axes of the drive shaft, the inner wall of the pilot hole is equipped with along the guiding hole length side
To the rotation prevention portion of extension, the opening down and described dispensing port of the dispensing port is connected to the pilot hole；
Driving lever, one end of the driving lever and the driving axis connection, and the central axes of the driving lever and the drive
The central axes of moving axis overlap, and the outer wall of the driving lever is equipped with screw thread；And
Release lever, the unlocking lever tube are connected on the driving lever, and are screwed togather with the driving lever, the release lever sliding
Ground is inserted in the pilot hole of the pedestal, and the outer wall of the release lever is equipped with limiting section, the limiting section and the rotation stop
One of portion is raised line, and another is limiting slot, and the raised line is slidably contained in the limiting slot.
Based on features described above：When driving lever is rotated, since driving lever and release lever screw togather, the rotation stop in pilot hole
Portion defines the rotation of release lever, and release lever can only be axial for linear motion along it at this time, by changing actuator driven axis
Direction of rotation can convert the direction of motion of release lever.When release lever is moved towards dispensing port direction, release lever end and throwing
A mouthful inner wall is put to be clamped missile；When release lever to far from dispensing port direction move when, release lever end to missile into
Row is launched.The present invention is used slides transmission mechanism in spiral, can be axially moved with smaller torque rotation generation and larger
Axial force can be clamped heavier missile thereby using the actuator of lower-wattage and be easy to take out release lever from pedestal
From ensureing the release of weight.Also, when generating vibration in flight course or when actuator damages, due to working as release lever conduct
When driving link moves in a straight line, driving lever can form self-locking to release lever, to limit the movement of release lever.Therefore this hair
Bright safety higher, weight are light, at low cost.
Further, the actuator seat includes a link and two connecting plates that are oppositely arranged, two pieces of connecting plates
One end is connect with the both sides of link respectively, and the link is connect with the actuator, and the drive shaft is located at described in two pieces
Between connecting plate；The pedestal is connect with two pieces of connecting plates.
Further, the actuator and link are detachably connected by screw bolt and nut.
Further, the pedestal and connecting plate are detachably connected by bolt.
Further, the pedestal is equipped with hollow portion.
Further, the dispensing port inner wall opposite with pilot hole is equipped with consistent logical of internal diameter and pilot hole internal diameter
Hole, and the through-hole is located along the same line with the pilot hole.
Further, the release lever is fixed with block in a ring on the periphery wall of driving lever one end, described
The central axes of block are overlapped with the central axes of driving lever, and the outer diameter of the block is more than the aperture of the pilot hole.
Further, the screw thread of the driving lever uses trapezoidal thread or saw-tooth thread.
Further, the pedestal upper surface is equipped with the threaded hole that several are used to be detachably connected with unmanned plane.
The present invention also provides a kind of unmanned plane, which has above-mentioned unmanned plane delivery device.
Due to the adoption of the above technical scheme, the invention has the advantages that：
1. the present invention is safe, heavy load is clamped and is stablized, the vibration during capable of solving because of unmanned plane during flying
Or actuator damage and the problem of cause missile to fall.
2. the present invention is at low cost, weight is light, can effectively mitigate the load of unmanned plane, reduce the loss of energy.
3. structure of the invention is stablized, it is easy to be dismounted with unmanned plane.
Description of the drawings
Fig. 1 is the structural schematic diagram of a better embodiment unmanned plane delivery device of the invention；
Fig. 2 is the exploded view of unmanned plane delivery device shown in Fig. 1
Fig. 3 is the structural schematic diagram of actuator seat in unmanned plane delivery device shown in Fig. 1；
Fig. 4 is the structural schematic diagram of release lever in unmanned plane delivery device shown in Fig. 1；
Fig. 5 is the structural schematic diagram of pedestal in unmanned plane delivery device shown in Fig. 1；
Fig. 6 is the view of pedestal other direction in unmanned plane delivery device shown in Fig. 1；
Main element symbol description is as follows in figure：
In attached drawing, 1- actuators, 1.1- drivings ontology, 1.2- drive shafts, 2- driving levers, 3- actuators seat, 3.1- connections
Plate, 3.2- links, 3.3- mounting holes, 4- release levers, 4.1- limiting sections, 4.2- blocks, 5- pedestals, 5.1- pilot holes, 5.2-
Hollow portion, 5.3- dispensing ports, 5.4- rotation prevention portions, 5.5- threaded holes, 5.6- through-holes.
Specific implementation mode
The specific implementation of invention is further illustrated below in conjunction with attached drawing.
As depicted in figs. 1 and 2, a kind of unmanned plane delivery device, including actuator seat 3, actuator 1, pedestal 5, driving lever 2
With release lever 4.
As shown in figure 3, in the present embodiment, actuator seat 3 specifically includes the company that a link 3.2 and two is oppositely arranged
Fishplate bar 3.1, on link 3.2 perforation offer mounting hole 3.3, two pieces of 3.1 one end of connecting plate both sides with link 3.2 respectively
Connection, and extend in the same direction.Actuator 1 includes the drive shaft 1.2 for driving ontology 1.1 and being connect with driving ontology 1.1,
Wherein, driving ontology 1.1 is installed on link 3.2, and wears mounting hole, in the present embodiment, is driven ontology 1.1 and is connected
Frame 3.2 is connect to connect by bolt and nut；Drive shaft 1.2 is located between two pieces of connecting plates 3.1, and drive shaft 1.2 can drive this
Body 1.1 is rotated by.In the present embodiment, actuator 1 uses steering engine, it will be understood that in other embodiments, holds
Row device 1 can also use other driving mechanisms, such as motor etc..
As shown in Figure 5 and Figure 6, pedestal 5 is connect with the two pieces of one end of connecting plate 3.1 far from link 3.2, in this embodiment party
In formula, pedestal 5 is substantially in bulk, and one side is located between two pieces of connecting plates 3.1, and is connected by bolt with two pieces of connecting plates 3.1
It connects.Pilot hole 5.1 and dispensing port 5.3 are offered on pedestal 5.Wherein, 1 drive shaft 1.2 of the central axes of pilot hole 5.1 and actuator
Central axes overlap, the inner wall of pilot hole 5.1 is equipped with the rotation prevention portion 5.4 extended along 5.1 length direction of pilot hole.Dispensing port
5.3 is opening down, and dispensing port 5.3 is connected to pilot hole 5.1.In the present embodiment, dispensing port 5.3 is substantially u-shaped, excellent
Choosing is opened in the bottom position of pedestal 5, and outside the space that two pieces of connecting plates 3.1 are formed, dispensing port 5.3 also penetrates through pedestal 5
Side towards two pieces of connecting plates 3.1.Further, it is additionally provided with hollow portion 5.2 on pedestal 5, to mitigate delivery device entirety
Weight effectively mitigates the load of unmanned plane, reduces energy loss.In the present embodiment, hollow portion 5.2 penetrates through pedestal 5
Side towards two pieces of connecting plates 3.1.5 top surface of pedestal is equipped with several threaded holes for being used to be detachably connected with unmanned plane
5.5, to enable delivery device to be more stably installed on unmanned plane, keep the delivery device more steady in flight course
It is fixed.Preferably, the material of pedestal 5 and actuator seat 3 is stainless steel, to increase the service life of the delivery device.
2 one end of driving lever is connect with the drive shaft 1.2 of actuator 1, and 2 periphery wall of driving lever is equipped with screw thread, in driving lever 2
Axis is overlapped with 1 drive shaft of actuator, 1.2 central axes.4 one end of release lever is equipped with and the matched internal thread of 2 external screw thread of driving lever
Hole, release lever 4 are socketed on driving lever 2, and the external screw thread of the internal thread and driving lever 2 of release lever is made to be screwed, and release lever 4 slides
Ground is inserted in the pilot hole 5.1 of pedestal 5.The outer wall of release lever 4 is equipped with limiting section 4.1, limiting section 4.1 and rotation prevention portion 5.4
One of them is raised line, and another is limiting slot, which is slidably contained in the limiting slot, in the present embodiment, rotation stop
Portion 5.4 is raised line, and limiting section 4.1 is limiting slot.The screw thread of driving lever 2 preferably uses trapezoidal thread or saw-tooth thread.
In the present embodiment, internal diameter and pilot hole 5.1 are additionally provided on the inner wall opposite with pilot hole 5.1 of dispensing port 5.3
The consistent through-hole 5.6 of internal diameter, through-hole 5.6 are located along the same line with pilot hole 5.1.Release lever 4 is close to the outer of 1 one end of actuator
Block 4.2 in a ring is also fixed on peripheral wall, the central axes of block 4.2 are overlapped with the central axes of driving lever 2, and block
4.2 outer diameter is more than the aperture of pilot hole 5.1.In the present embodiment, when without using the delivery device, by 4 court of release lever
5.3 direction of dispensing port is moved to maximum distance, and the end of release lever 4 is located exactly in the through-hole 5.6 of 5.3 inner wall of dispensing port, gear
Block 4.2 is abutted with 5 outer wall of pedestal, is conducive to protect 4 end of release lever in this way.
Operation principle：Actuator 1 can drive driving lever 2 to rotate.Under the cooperation of limiting section 4.1 and rotation prevention portion 5.4, release
Putting bar 4 can not rotate with driving lever 2, at this time release lever 4 only can along driving lever 2 axial direction it is for linear motion, by change hold
The direction of rotation of 1 drive shaft 1.2 of row device can make release lever 4 along towards 5.3 direction of dispensing port or far from 5.3 direction of dispensing port
Movement.When release lever 4 is moved towards 5.3 direction of dispensing port, 4 end of release lever coordinates with 5.3 inner wall of dispensing port to missile
It is clamped；When release lever 4 far from 5.3 direction of dispensing port to when moving, missile is launched in 4 end of release lever.This hair
Bright embodiment is used can use smaller torque rotation generation to be axially moved and larger axial direction in spiral sliding transmission mechanism
Power can be clamped heavier missile thereby using the actuator of lower-wattage and be easy to take out release lever 4 from pedestal 5
From ensureing the release of weight.Also, when generating vibration in flight course or when actuator damages, due to working as 4 conduct of release lever
When driving link moves in a straight line, driving lever 2 can form self-locking to release lever 4, to limit the movement of release lever 4.Therefore
Safety higher, the weight of the present invention is light, at low cost.
Embodiment of the present invention also provides a kind of unmanned plane with above-mentioned unmanned plane delivery device.
Above description is the detailed description for the present invention preferably possible embodiments, but embodiment is not limited to this hair
Bright patent claim, it is all the present invention suggested by technical spirit under completed same changes or modifications change, should all belong to
In the covered the scope of the claims of the present invention.
Claims (10)
1. a kind of unmanned plane delivery device, which is characterized in that including
Actuator seat；
Actuator, including driving ontology and with the drive shaft that connect of driving ontology, the driving ontology be installed in described in hold
On row device seat；
Pedestal, the pedestal are connect with the actuator seat, and pilot hole and dispensing port, the pilot hole are offered on the pedestal
Central axes overlapped with the central axes of the drive shaft, the inner wall of the pilot hole is equipped with to be prolonged along the pilot hole length direction
The opening down and described dispensing port of the rotation prevention portion stretched, the dispensing port is connected to the pilot hole；
Driving lever, one end of the driving lever and the driving axis connection, and the central axes of the driving lever and the drive shaft
Central axes overlap, the outer wall of the driving lever is equipped with screw thread；And
Release lever, the unlocking lever tube are connected on the driving lever, and are screwed togather with the driving lever, and the release lever is slidably inserted
In the pilot hole of the pedestal, the outer wall of the release lever is equipped with limiting section, the limiting section and the rotation prevention portion its
One of be raised line, another is limiting slot, and the raised line is slidably contained in the limiting slot.
2. a kind of unmanned plane delivery device as described in claim 1, which is characterized in that the actuator seat includes a connection
Frame and two connecting plates that are oppositely arranged, two pieces of described connecting plate one end are connect with the both sides of link respectively, the link with
The actuator connection, the drive shaft is across the link and positioned at two pieces of connecting plates；The pedestal and two
Connecting plate described in block connects.
3. a kind of unmanned plane delivery device as claimed in claim 2, which is characterized in that the actuator and link pass through spiral shell
Screw bolt and nut is detachably connected.
4. a kind of unmanned plane delivery device as claimed in claim 2, which is characterized in that the pedestal and connecting plate pass through bolt
It is detachably connected.
5. a kind of unmanned plane delivery device as described in claim 1, which is characterized in that the pedestal is equipped with hollow portion.
6. a kind of unmanned plane delivery device as described in claim 1, which is characterized in that the dispensing port is opposite with pilot hole
Inner wall is equipped with the internal diameter through-hole consistent with pilot hole internal diameter, and the through-hole is located along the same line with the pilot hole.
7. a kind of unmanned plane delivery device as described in claim 1, which is characterized in that the release lever is close to driving lever one end
Periphery wall on be fixed with block in a ring, the central axes of the block are overlapped with the central axes of driving lever, the block
Outer diameter be more than the pilot hole aperture.
8. a kind of unmanned plane delivery device as described in claim 1, which is characterized in that the screw thread of the driving lever is using trapezoidal
Screw thread or saw-tooth thread.
9. a kind of unmanned plane delivery device as described in claim 1, which is characterized in that the pedestal upper surface is equipped with several
Threaded hole for being detachably connected with unmanned plane.
10. a kind of unmanned plane, including unmanned plane delivery device, it is characterised in that：The unmanned plane delivery device is according to right
It is required that the unmanned plane delivery device described in any one of 1-9.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810696596.1A CN108791884A (en) | 2018-06-29 | 2018-06-29 | Unmanned plane delivery device and unmanned plane with the unmanned plane device delivery device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810696596.1A CN108791884A (en) | 2018-06-29 | 2018-06-29 | Unmanned plane delivery device and unmanned plane with the unmanned plane device delivery device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108791884A true CN108791884A (en) | 2018-11-13 |
Family
ID=64072649
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810696596.1A Pending CN108791884A (en) | 2018-06-29 | 2018-06-29 | Unmanned plane delivery device and unmanned plane with the unmanned plane device delivery device |
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| CN (1) | CN108791884A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109808887A (en) * | 2019-01-29 | 2019-05-28 | 西北工业大学 | A kind of throwing laying mechanism for small drone |
| CN110466769A (en) * | 2019-08-02 | 2019-11-19 | 辽宁力德航空科技有限公司 | A kind of unmanned plane delivery device |
| CN114633885A (en) * | 2022-05-12 | 2022-06-17 | 长安大学 | Split type geological disaster monitoring instrument deployed by unmanned aerial vehicle and deployment method thereof |
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| CN106043699A (en) * | 2016-07-13 | 2016-10-26 | 绵阳空天科技有限公司 | Dropping device of unmanned aerial vehicle |
| CN206885354U (en) * | 2017-05-11 | 2018-01-16 | 昊翔电能运动科技(昆山)有限公司 | A kind of unmanned plane throwing device and unmanned plane |
| CN108033014A (en) * | 2017-12-19 | 2018-05-15 | 佛山市神风航空科技有限公司 | Can remote control throw parcel small drone |
| CN208429236U (en) * | 2018-06-29 | 2019-01-25 | 广西壹蕴科技股份有限公司 | Unmanned plane delivery device and unmanned plane with the unmanned plane device delivery device |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109808887A (en) * | 2019-01-29 | 2019-05-28 | 西北工业大学 | A kind of throwing laying mechanism for small drone |
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| CN110466769A (en) * | 2019-08-02 | 2019-11-19 | 辽宁力德航空科技有限公司 | A kind of unmanned plane delivery device |
| CN114633885A (en) * | 2022-05-12 | 2022-06-17 | 长安大学 | Split type geological disaster monitoring instrument deployed by unmanned aerial vehicle and deployment method thereof |
| CN114633885B (en) * | 2022-05-12 | 2022-08-02 | 长安大学 | Split type geological disaster monitoring instrument deployed by unmanned aerial vehicle and deployment method thereof |
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