CN207450285U - For the fixed-wing unmanned aerial vehicle ejecting system of flight controlled training - Google Patents
For the fixed-wing unmanned aerial vehicle ejecting system of flight controlled training Download PDFInfo
- Publication number
- CN207450285U CN207450285U CN201721416492.8U CN201721416492U CN207450285U CN 207450285 U CN207450285 U CN 207450285U CN 201721416492 U CN201721416492 U CN 201721416492U CN 207450285 U CN207450285 U CN 207450285U
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- China
- Prior art keywords
- base member
- slide
- air pump
- shaft
- aerial vehicle
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Abstract
The utility model provides a kind of fixed-wing unmanned aerial vehicle ejecting system for flight controlled training, including base member and the slide that takes off being arranged on above base member；The slide that takes off is equipped with strip through-hole；Base member one end is rotatablely connected by one end of main shaft and the slide that takes off, height is provided at the top of the base member other end and adjusts telescope motor, it highly adjusts the output terminal at the top of telescope motor to be connected with the height regulating rod being vertically arranged, the other end of height regulating rod is connected with the slide bottom of taking off；Base member includes bar shaped fixed plate and the air pump component for being arranged on the bar shaped fixed plate both sides, air pump component is connected by side shaft with the bar shaped fixed plate, the output terminal of two air pump components is connected with M type supporting racks, the middle of the M types supporting rack is rotatablely connected by the second shaft and metal tube, metal tube is internally provided with main spring, and main spring end is connected to the telescopic rod through strip through-hole；The telescopic rod other end is connected by first rotating shaft with unmanned plane connecting rod.
Description
Technical field
The utility model is related to technical field of flight control, and in particular to a kind of fixed-wing for flight controlled training without
Man-machine ejection system.
Background technology
With the development of domestic General Aviation, the quantity of all purpose aircraft is growing, but fly training cost with
American-European countries compares, selling at exorbitant prices.Therefore certain foundation training is carried out to pilot using flight simulator, can not only carried
The efficiency of height training, and training cost can be saved.
With fast development of the unmanned plane in civilian technology field, the flight operation of unmanned plane is controlled to fly simulation training
In play increasing effect.At present, unmanned aerial plane launching system is mainly using hydraulic pressure, pneumatic, rocket assist these types hair
Penetrate mode；These types of radiation pattern, there is the problem of complicated, manufacture use cost is high, and maintenance is difficult.
Utility model content
The purpose of this utility model is that in view of the deficiencies of the prior art, provide a kind of fixation for flight controlled training
Wing unmanned aerial vehicle ejecting system, the fixed-wing unmanned aerial vehicle ejecting system for being used for flight controlled training can well solve above-mentioned ask
Topic.
To reach above-mentioned requirements, the technical scheme adopted by the utility model is that：It provides a kind of for flight controlled training
Fixed-wing unmanned aerial vehicle ejecting system, the fixed-wing unmanned aerial vehicle ejecting system for being used for flight controlled training include base member and set
Put the slide that takes off above the base member；The slide that takes off is equipped with strip through-hole；Base member one end passes through main shaft
It is rotatablely connected with one end of the slide that takes off, height is provided at the top of the base member other end and adjusts telescope motor, institute
State height adjust telescope motor at the top of output terminal be connected with the height regulating rod being vertically arranged, the height regulating rod it is another
End is connected with the slide bottom of taking off；Base member includes bar shaped fixed plate and the gas for being arranged on the bar shaped fixed plate both sides
Pump part, the air pump component are connected by side shaft with the bar shaped fixed plate, the output terminal of described two air pump components
It is connected with M type supporting racks, the middle of the M types supporting rack is rotatablely connected by the second shaft and metal tube, the metal
Pipe is internally provided with main spring, and the main spring end is connected to the telescopic rod through the strip through-hole；The telescopic rod other end
It is connected by first rotating shaft with unmanned plane connecting rod.
This has the advantage that as follows for the fixed-wing unmanned aerial vehicle ejecting system of flight controlled training：
(1) by setting air pump component, M types supporting rack, the second shaft, side shaft, main spring, metal on base member
Pipe and telescopic rod, the ejection that can be stored power mode by two kinds of air pump component and main spring and realize unmanned plane.
(2) by setting base member, and base member and the slide that takes off are rotatablely connected using main shaft, while risen
Fly slide middle part set for telescopic rod by strip through-hole, the components such as main spring, metal tube and telescopic rod can be put
In the lower section for the slide that takes off, prevent these components from being collided in unmanned aerial vehicle ejecting with unmanned plane.
(3) by the way that main spring is arranged on inside metal tube, and it main spring with telescopic rod is connected can prevent main spring
It gets rusty for a long time exposed to outside.
Description of the drawings
Attached drawing described herein is used for providing further understanding of the present application, the part of the application is formed, at this
The same or similar part, the schematic description and description of the application are represented using identical reference number in a little attached drawings
For explaining the application, the improper restriction to the application is not formed.In the accompanying drawings：
Fig. 1 schematically shows the fixed-wing unmanned plane for flight controlled training according to the application one embodiment
The structure diagram of ejection system.
Fig. 2 schematically shows the fixed-wing unmanned plane for flight controlled training according to the application one embodiment
The structure diagram of the base member of ejection system.
Fig. 3 schematically shows the fixed-wing unmanned plane for flight controlled training according to the application one embodiment
The structure diagram of the slide that takes off of ejection system.
Wherein：1st, main shaft；2nd, take off slide；3rd, unmanned plane connecting rod；4th, first rotating shaft；5th, base member；6th, air pump
Component；7th, M types supporting rack；8th, the second shaft；9th, height regulating rod；10th, height adjusts telescope motor；11st, bar shaped fixed plate；
12nd, side shaft；13rd, main spring；14th, metal tube；15th, telescopic rod；16th, strip through-hole.
Specific embodiment
To make the purpose, technical scheme and advantage of the application clearer, below in conjunction with drawings and the specific embodiments, to this
Application is described in further detail.
In the following description, the reference of " one embodiment ", " embodiment ", " example ", " example " etc. is shown
The embodiment or example so described can include special characteristic, structure, characteristic, property, element or limit, but not each real
Applying example or example all necessarily includes special characteristic, structure, characteristic, property, element or limit.In addition, reuse phrase " according to
One embodiment of the application " is not necessarily referring to identical embodiment although it is possible to refer to identical embodiment.
For the sake of simplicity, some technical features known to those skilled in the art are omitted in being described below.
According to one embodiment of the application, a kind of fixed-wing unmanned aerial vehicle ejecting system for flight controlled training is provided
System, as shown in Figs. 1-3, including base member 5 and the slide 2 that takes off being arranged on above the base member 5；It takes off on slide 2
Equipped with strip through-hole 16；5 one end of base member is rotatablely connected by one end of main shaft 1 and the slide 2 that takes off, the pedestal
Height is provided at the top of 5 other end of component and adjusts telescope motor 10, the height adjust the output terminal at 10 top of telescope motor with
The height regulating rod 9 being vertically arranged connects, and the other end of the height regulating rod 9 is connected with 2 bottom of slide of taking off.
According to one embodiment of the application, this is used for the pedestal of the fixed-wing unmanned aerial vehicle ejecting system of flight controlled training
Component 5 includes bar shaped fixed plate 11 and the air pump component 6 for being arranged on 11 both sides of bar shaped fixed plate, and the air pump component 6 is equal
It is connected by side shaft 12 with the bar shaped fixed plate 11, the output terminal of described two air pump components 6 connects with M types supporting rack 7
It connects, the middle of the M types supporting rack 7 is rotatablely connected by the second shaft 8 with metal tube 14, and the metal tube 14 is internally provided with
Main spring 13,13 end of main spring are connected to the telescopic rod 15 through the strip through-hole 16；15 other end of telescopic rod
It is connected by first rotating shaft 4 with unmanned plane connecting rod 3.
According to one embodiment of the application, this is used for the main bullet of the fixed-wing unmanned aerial vehicle ejecting system of flight controlled training
13 both ends of spring are connected respectively with the second shaft 8 and telescopic rod 15.
According to one embodiment of the application, this is used for the M types of the fixed-wing unmanned aerial vehicle ejecting system of flight controlled training
Supporting rack 7 is used to connect two vertical bars including two for the vertical bar being connected with 6 output terminal of air pump component and one
Horizon bar.
According to one embodiment of the application, this be used for the fixed-wing unmanned aerial vehicle ejecting system of flight controlled training by
Air pump component 6, M types supporting rack 7, the second shaft 8, side shaft 12, main spring 13, metal tube 14 on base member 5 are set and stretched
Contracting bar 15, the ejection that can be stored power mode by 13 two kinds of air pump component 6 and main spring and realize unmanned plane；By setting base portion
Part 5, and be rotatablely connected base member 5 and the slide 2 that takes off using main shaft 1, while set and be used in 2 middle part of slide of taking off
Telescopic rod 15 by strip through-hole 16, the components such as main spring 13, metal tube 14 and telescopic rod 15 can be placed in the slide 2 that takes off
Lower section, prevent these components in unmanned aerial vehicle ejecting with unmanned plane collide；By the way that main spring 13 is arranged in metal tube 14
Portion, and main spring 13 is connected with telescopic rod 15 can prevent 13 long-time of main spring from getting rusty exposed to outside.
According to one embodiment of the application, which is using
When uav bottom can be fixed in unmanned plane connecting rod 3, the top of unmanned plane connecting rod 3 can be provided with hook, will hang
Hook hook can be provided with air pump inside the bottom of unmanned plane, air pump component 6, its output terminal can be compressed in air realizes storage
It can and can discharge and promote M types supporting rack 7, telescopic rod 15 can be to pass through strip through-hole 16 and the unmanned plane for 2 top of slide of taking off
Connection.
Embodiment described above only represents the several embodiments of the utility model, and description is more specific and detailed, but
It can not be interpreted as the limitation to the scope of the utility model.It should be pointed out that for those of ordinary skill in the art,
Without departing from the concept of the premise utility, various modifications and improvements can be made, these belong to the utility model
Protection domain.Therefore the scope of protection of the utility model should be subject to the claim.
Claims (3)
1. for the fixed-wing unmanned aerial vehicle ejecting system of flight controlled training, it is characterised in that：Including base member and it is arranged on
The slide that takes off above the base member；
The slide that takes off is equipped with strip through-hole；
Described base member one end is rotatablely connected by one end of main shaft and the slide that takes off, the base member other end
Top is provided with height and adjusts telescope motor, and the height adjusts the output terminal at the top of telescope motor and the height tune being vertically arranged
Pole connects, and the other end of the height regulating rod is connected with the slide bottom of taking off；
The base member includes bar shaped fixed plate and the air pump component for being arranged on the bar shaped fixed plate both sides, the air pump portion
Part is connected by side shaft with the bar shaped fixed plate, and the output terminal of described two air pump components is connected with M type supporting racks,
The middle of the M types supporting rack is rotatablely connected by the second shaft and metal tube, and the metal tube is internally provided with main spring, institute
It states main spring end and is connected to the telescopic rod through the strip through-hole；The telescopic rod other end passes through first rotating shaft and unmanned plane
Connecting rod connects.
2. the fixed-wing unmanned aerial vehicle ejecting system according to claim 1 for flight controlled training, it is characterised in that：Institute
Main spring both ends are stated to be connected with the second shaft and telescopic rod respectively.
3. the fixed-wing unmanned aerial vehicle ejecting system according to claim 1 for flight controlled training, it is characterised in that：Institute
It is vertical for connecting two for the vertical bar being connected with the air pump element outputs and one including two to state M types supporting rack
The horizon bar of bar.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721416492.8U CN207450285U (en) | 2017-10-30 | 2017-10-30 | For the fixed-wing unmanned aerial vehicle ejecting system of flight controlled training |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721416492.8U CN207450285U (en) | 2017-10-30 | 2017-10-30 | For the fixed-wing unmanned aerial vehicle ejecting system of flight controlled training |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207450285U true CN207450285U (en) | 2018-06-05 |
Family
ID=62282512
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721416492.8U Expired - Fee Related CN207450285U (en) | 2017-10-30 | 2017-10-30 | For the fixed-wing unmanned aerial vehicle ejecting system of flight controlled training |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207450285U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109398737A (en) * | 2018-09-28 | 2019-03-01 | 洪炜林 | A kind of unmanned plane casting device using generation information technology |
-
2017
- 2017-10-30 CN CN201721416492.8U patent/CN207450285U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109398737A (en) * | 2018-09-28 | 2019-03-01 | 洪炜林 | A kind of unmanned plane casting device using generation information technology |
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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: 20180605 Termination date: 20181030 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |