CN207791155U - Unmanned propeller-parachuting - Google Patents
Unmanned propeller-parachuting Download PDFInfo
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- CN207791155U CN207791155U CN201820149990.9U CN201820149990U CN207791155U CN 207791155 U CN207791155 U CN 207791155U CN 201820149990 U CN201820149990 U CN 201820149990U CN 207791155 U CN207791155 U CN 207791155U
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- parachuting
- rotor
- idler wheel
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- unmanned propeller
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Abstract
This disclosure relates to which a kind of unmanned propeller-parachuting, including body (10), the body (10) are equipped with umbrella cabin；Paraglider (20) can be ejectedly accommodated in the umbrella cabin；And rotor (30), it is mounted on the body (10), to provide lift for the body (10).Through the above technical solutions, rotor is arranged on the body of unmanned propeller-parachuting, rotor can generate lift when rotated so that body can take off vertically, to avoid being restricted by factors such as the job area of take-off venue and wind conditions.When taking off, paraglider can be accommodated in umbrella cabin, and after unmanned propeller-parachuting, which rises, flies to certain altitude, rotor stops rotating, and paraglider is popped up from umbrella cabin provides lift to continue as unmanned propeller-parachuting.
Description
Technical field
This disclosure relates to unmanned vehicle technical field, and in particular, to a kind of unmanned propeller-parachuting.
Background technology
Unmanned propeller-parachuting is a kind of unmanned vehicle using paragliding, is applied to the fields such as plant protection.In related skill
In art, the form of ski-jump take-off is usually taken in unmanned propeller-parachuting, generates initial velocity by thrust, lift is generated by paraglider.
This mode of taking off is influenced more apparent by the job area of take-off venue and wind condition etc., often occurs umbrella in take-off process
The case where head collapses, and umbrella car deviation etc. cannot normally take off.
Utility model content
Purpose of this disclosure is to provide a kind of unmanned propeller-parachutings, are constrained by takeoff condition with solving existing unmanned propeller-parachuting
Larger problem.
To achieve the goals above, the disclosure provides a kind of unmanned propeller-parachuting, including：
Body, the body are equipped with umbrella cabin；
Paraglider can be ejectedly accommodated in the umbrella cabin；And
Rotor is mounted on the body, to provide lift for the body.
Optionally, the unmanned propeller-parachuting further includes the support arm extended laterally outward from the body, the rotor
Mounted on the end of the support arm, the rotor includes multiple, is symmetrically disposed in the both sides of the body.
Optionally, the rotor of the body both sides when rotated oppositely oriented.
Optionally, the support arm is removably mounted on the body.
Optionally, the rear end of the body is provided with vertical rotor.
Optionally, the rear end of the body is provided with guard circle, and the guard circle is looped around the periphery of the vertical rotor.
Optionally, the bottom of the body is provided with idler wheel.
Optionally, the idler wheel includes the first idler wheel being arranged immediately below the front end of the body, and is arranged in institute
State the second idler wheel and third idler wheel below the rear end side of body.
Optionally, first idler wheel is mounted on by the first strut for extending straight down on the body, and described the
Second wheel is mounted on by the second strut extended obliquely downward on the body, and the third idler wheel is by extending obliquely downward
Third strut be mounted on the body, second strut and the third strut are symmetrical with the longitudinal center of the body
Line.
Through the above technical solutions, rotor is arranged on the body of unmanned propeller-parachuting, rotor when rotated can
Enough generate lift so that body can take off vertically, to avoid by the job area of take-off venue and wind condition etc.
Factor restricts.When taking off, paraglider can be accommodated in umbrella cabin, after unmanned propeller-parachuting, which rises, flies to certain altitude, level rotation
The wing stops rotating, and paraglider is popped up from umbrella cabin provides lift to continue as unmanned propeller-parachuting.
Other feature and advantage of the disclosure will be described in detail in subsequent specific embodiment part.
Description of the drawings
Attached drawing is for providing further understanding of the disclosure, and a part for constitution instruction, with following tool
Body embodiment is used to explain the disclosure together, but does not constitute the limitation to the disclosure.In the accompanying drawings：
Fig. 1 is the side view of unmanned propeller-parachuting in accordance with one embodiment of the present disclosure；
Fig. 2 is the vertical view of unmanned propeller-parachuting in accordance with one embodiment of the present disclosure, wherein paraglider is not shown；
Fig. 3 is the front view of unmanned propeller-parachuting in accordance with one embodiment of the present disclosure, wherein paraglider is not shown.
Reference sign
10 body, 20 paraglider
30 rotor, 40 support arm
50 vertical rotor, 60 guard circle
71 first idler wheel, 72 second idler wheel
73 third idler wheel, 81 first strut
82 second strut, 83 third strut
Specific implementation mode
The specific implementation mode of the disclosure is described in detail below in conjunction with attached drawing.It should be understood that this place is retouched
The specific implementation mode stated is only used for describing and explaining the disclosure, is not limited to the disclosure.
In the disclosure, in the absence of explanation to the contrary, the noun of locality used such as "upper", "lower" refer to that unmanned plane exists
Normal operating condition it is upper and lower, specifically can refer to the page of Fig. 1, "inner", "outside" be for corresponding parts itself
For profile, the longitudinal direction of unmanned propeller-parachuting refers to its front-rear direction, laterally refers to left and right sides when its front and back flight.
In addition, the term " first " used in the disclosure, " second " etc. are to distinguish an element and another element, do not have suitable
Sequence and importance.In the following description when referring to the accompanying drawings, unless otherwise indicated, the same numbers in different attached drawings indicate it is identical or
Similar element.
The unmanned propeller-parachuting that the disclosure provides includes body and provides the first power plant of lift for body.Such as Fig. 1
Shown in Fig. 3, the first power plant includes paraglider 20 and rotor 30, and body 10 is equipped with umbrella cabin, and paraglider 20 can bullet
It is accommodated in going out in umbrella cabin, rotor 30 is mounted on body 10.In this way, rotor 30 can generate liter when rotated
Power so that body 10 can take off vertically, to avoid by factors systems such as the job area of take-off venue and wind conditions
About.When taking off, paraglider 20 can be accommodated in umbrella cabin, after unmanned propeller-parachuting, which rises, flies to certain altitude, rotor 30
It stops rotating, paraglider 20 is popped up from umbrella cabin provides lift to continue as unmanned propeller-parachuting.The pop-up mode of paraglider 20 can
To use conventional setting in the art, such as it is referred to the ejection mode of parachute.
The second power plant for providing forward force for body is additionally provided on body 10, specifically, such as Fig. 1 to Fig. 3
Shown, the second power plant may include vertical rotor 50, and vertical rotor 50 is arranged in the rear end of body 10.Vertical rotor 50 is revolved
Driving force can be generated when turning, and to push body 10 to advance forward, when vertical rotor 50 reversely rotates, can also provide body
Brake force or the power of retrogressing when 10 traveling.
Further, the rear end of body 10 is also provided with guard circle 60, and with reference to Fig. 3, guard circle 60 is looped around vertically
The periphery of rotor 50, there are certain intervals with the periphery of vertical rotor 50, to not influence the case where vertical rotor 50 rotates
Under, prevent vertical rotor 50 from being wounded by the barrier of surrounding.Guard circle 60 may be used as frame structure, to mitigate weight, and
And the air-flow that can be generated to avoid influence vertical rotor 50.
Rotor 30 is referred to the setting form of helicopter or multi-rotor unmanned aerial vehicle.As shown in Fig. 2, in this embodiment party
In formula, unmanned propeller-parachuting further includes the support arm 40 extended laterally outward from body 10, and rotor 30 is mounted on the end of support arm 40
Portion.Rotor 30 includes multiple, that is, lift is provided in the form of more rotors.As shown in Fig. 2, multiple rotors 30 are right
Ground is claimed to be arranged in the both sides of body 10, to ensure the balance of body 10.
Further, the rotor 30 of 10 both sides of body when rotated oppositely oriented, such as shown in Fig. 2, drawing side
The rotation direction of two rotors 30 to the left and two rotors 30 on right side it is oppositely oriented, to prevent body 10 from
Body twists, deviation.
In addition, support arm 40 can be to be removably mounted on body 10, that is, rotor 30 can be installed selectively
On body 10.When installing rotor 30 on body 10, the lift that rotor 30 can be utilized to generate makes body 10 hang down
Directly take off.When not installing rotor 30 on body 10, paraglider 20 can be popped up first from umbrella cabin, and then utilize cunning
The lift driving body 10 that Xiang umbrella 20 generates takes off.When not installing rotor 30, the lighter in weight of unmanned propeller-parachuting can be with
Improve its cruising ability.
As shown in Figure 1 to Figure 3, the bottom of body 10 is also provided with idler wheel, that is, unmanned propeller-parachuting can also be used and be slided
It jumps up winged form.In this case, paraglider 20 is popped up from umbrella cabin first, can condition take-off venue appropriate into
Row takes off.In this way, the disclosure provide unmanned propeller-parachuting can either take off vertically, also can ski-jump take-off, enrich user choosing
Selecting property.
Further, referring to figs. 1 to Fig. 3, idler wheel may include the first idler wheel being arranged immediately below the front end of body 10
71, and the second idler wheel 72 and third idler wheel 73 that are arranged below the rear end side of body 10, wherein the second idler wheel 72 and third
Idler wheel 73 can be symmetrical with the longitudinal centre line of body 10.The stationarity of body 10 is ensured in the form of supported at three point, simultaneously
Idler wheel is avoided excessively to increase the weight of unmanned propeller-parachuting.
Further, as shown in figure 3, the first idler wheel 71 is mounted on body 10 by the first strut 81 extended straight down
On, the second idler wheel 72 is mounted on by the second strut 82 extended obliquely downward on body 10, and third idler wheel 73 is by being tilted towards
The third strut 83 of lower extension is mounted on body 10, and the second strut 82 and third strut 83 are symmetrical with the longitudinal center of body 10
Line.Second strut 82 and third strut 83 are obliquely installed, and can enhance the stability of the two support body 10.
The preferred embodiment of the disclosure is described in detail above in association with attached drawing, still, the disclosure is not limited to above-mentioned reality
The detail in mode is applied, in the range of the technology design of the disclosure, a variety of letters can be carried out to the technical solution of the disclosure
Monotropic type, these simple variants belong to the protection domain of the disclosure.
It is further to note that specific technical features described in the above specific embodiments, in not lance
In the case of shield, can be combined by any suitable means, in order to avoid unnecessary repetition, the disclosure to it is various can
The combination of energy no longer separately illustrates.
In addition, arbitrary combination can also be carried out between a variety of different embodiments of the disclosure, as long as it is without prejudice to originally
Disclosed thought equally should be considered as disclosure disclosure of that.
Claims (9)
1. a kind of unmanned propeller-parachuting, which is characterized in that including：
Body (10), the body (10) are equipped with umbrella cabin；
Paraglider (20) can be ejectedly accommodated in the umbrella cabin；And
Rotor (30) is mounted on the body (10), to provide lift for the body (10).
2. unmanned propeller-parachuting according to claim 1, which is characterized in that further include laterally outward prolonging from the body (10)
The support arm (40) stretched, the rotor (30) are mounted on the end of the support arm (40), and the rotor (30) includes more
It is a, it is symmetrically disposed in the both sides of the body (10).
3. unmanned propeller-parachuting according to claim 2, which is characterized in that the rotor of body (10) both sides
(30) when rotated oppositely oriented.
4. unmanned propeller-parachuting according to claim 2, which is characterized in that the support arm (40) is removably mounted on described
On body (10).
5. unmanned propeller-parachuting according to claim 1, which is characterized in that the rear end of the body (10) is provided with vertical rotation
The wing (50).
6. unmanned propeller-parachuting according to claim 5, which is characterized in that the rear end of the body (10) is provided with guard circle
(60), the guard circle (60) is looped around the periphery of the vertical rotor (50).
7. the unmanned propeller-parachuting according to any one of claim 1-6, which is characterized in that the bottom of the body (10) is set
It is equipped with idler wheel.
8. unmanned propeller-parachuting according to claim 7, which is characterized in that the idler wheel includes being arranged in the body (10)
Front end immediately below the first idler wheel (71), and be arranged the second idler wheel (72) below the rear end side of the body (10) and
Third idler wheel (73).
9. unmanned propeller-parachuting according to claim 8, which is characterized in that first idler wheel (71) by prolonging straight down
The first strut (81) stretched is mounted on the body (10), and second idler wheel (72) is by extend obliquely downward second
Bar (82) is mounted on the body (10), and the third idler wheel (73) is installed by the third strut (83) extended obliquely downward
On the body (10), second strut (82) and the third strut (83) are symmetrical in the longitudinal direction of the body (10)
Heart line.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820149990.9U CN207791155U (en) | 2018-01-29 | 2018-01-29 | Unmanned propeller-parachuting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820149990.9U CN207791155U (en) | 2018-01-29 | 2018-01-29 | Unmanned propeller-parachuting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207791155U true CN207791155U (en) | 2018-08-31 |
Family
ID=63267043
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820149990.9U Active CN207791155U (en) | 2018-01-29 | 2018-01-29 | Unmanned propeller-parachuting |
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109455296A (en) * | 2018-06-20 | 2019-03-12 | 周欢东 | A kind of unmanned transporter of parafoil that air security adaptability height has big load |
| CN109625262A (en) * | 2018-10-12 | 2019-04-16 | 周欢东 | Has the unmanned transporter of the high parafoil of steady air security that lands that takes off that flies |
| CN111392044A (en) * | 2020-03-02 | 2020-07-10 | 周欢东 | Unmanned aerial vehicle express delivery for delivery |
| TWI790860B (en) * | 2021-12-15 | 2023-01-21 | 溫文賢 | Oil-cooled four-stroke engine for powered paragliding |
| CN109625262B (en) * | 2018-10-12 | 2024-05-10 | 周欢东 | Unmanned parachute conveyor with stable flying, taking-off and landing and high air safety |
-
2018
- 2018-01-29 CN CN201820149990.9U patent/CN207791155U/en active Active
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109455296A (en) * | 2018-06-20 | 2019-03-12 | 周欢东 | A kind of unmanned transporter of parafoil that air security adaptability height has big load |
| CN109625262A (en) * | 2018-10-12 | 2019-04-16 | 周欢东 | Has the unmanned transporter of the high parafoil of steady air security that lands that takes off that flies |
| CN109625262B (en) * | 2018-10-12 | 2024-05-10 | 周欢东 | Unmanned parachute conveyor with stable flying, taking-off and landing and high air safety |
| CN111392044A (en) * | 2020-03-02 | 2020-07-10 | 周欢东 | Unmanned aerial vehicle express delivery for delivery |
| CN111392044B (en) * | 2020-03-02 | 2024-05-10 | 周欢东 | Unmanned aerial vehicle express delivery for delivery |
| TWI790860B (en) * | 2021-12-15 | 2023-01-21 | 溫文賢 | Oil-cooled four-stroke engine for powered paragliding |
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