CN204895861U - Unmanned cargo airplane - Google Patents
Unmanned cargo airplane Download PDFInfo
- Publication number
- CN204895861U CN204895861U CN201520402150.5U CN201520402150U CN204895861U CN 204895861 U CN204895861 U CN 204895861U CN 201520402150 U CN201520402150 U CN 201520402150U CN 204895861 U CN204895861 U CN 204895861U
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- China
- Prior art keywords
- ducted fan
- wing
- fan group
- unmanned
- transport plane
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Abstract
The utility model provides an unmanned cargo airplane, belong to unmanned airborne vehicle field, by the stationary vane, thick wing, with the dress at the inside unmanned cargo airplane who blows wing lift -rising mechanism group one -tenth who constitutes for the crescent fin by small -size ducted fan group and cross -section of thick wing, it is big to have lift, low latitude low -speed, the speed freely, but and short take off and landing, do not need the airport, its usage is the short -distance transport of agricultural, hang the agricultural implement and carry out the farm work, commercial goods transports, military usage is front transportation supply, the wounded etc. Transport, simple manufacture, and the cost is low, excellent performance's an unmanned cargo airplane, unmanned transport flight ship still can be made to this kind of cargo airplane, sea flight is plunderred in the low latitude.
Description
Technical field:
A kind of unmanned transport plane, belongs to unmanned field of aircraft, particularly relates to that a kind of fixed-wing is combined with thick wing and is provided with the unmanned transport plane that ducted fan group and cross section are the Chui Yi lift-rising mechanism that crescent shape vane cluster forms thick wing is inner.
Background technology:
The unmanned plane developed rapidly has been applied to the various aspects of national economy, people attempt to develop a kind of unmanned transport plane, this is that a kind of load capacity is larger, low-altitude low-speed, can short distance or VTOL function, does not need the unmanned plane being suitable for transporting of specific airport, there has been proposed various design plan, Chui Yi lift-rising mechanism is installed on fixed-wing unmanned plane by we can obtain good effect, its simple structure, economic and practical.
Summary of the invention:
Goal of the invention: a kind of unmanned transport plane is a kind of fixed-wing unmanned plane be made up of fixed-wing and thick wing, it is characterized in that the Chui Yi lift-rising mechanism that the vane cluster that the setting of thick wing inside is crescent shape by ducted fan group and cross section forms, its advantage is: lift is large, short take-off and landing (STOL), be best suited for farmland operation, field transport, commercial use be cargo transport, send express delivery, military use is rescue of battlefield, front supply, the machine simple structure, function admirable, cost are low, safety, environmental protection.
The present invention is achieved in that a kind of unmanned transport plane is by front fixed-wing, T-shaped tailplane, vertical tail, wing flap, body, traction electric propeller, drive motor, thick wing, ducted fan group, cross section is the vane cluster of crescent shape, ducted fan group control apparatus, steering wheel, alighting gear, power storehouse, equipment compartment, farm implements articulated device forms, and it is characterized in that: traction electric propeller, drive motor, front fixed-wing is arranged on front part of a body, vertical tail, T-shaped tailplane is arranged on After-Body, alighting gear, farm implements articulated device is arranged on underpart, power storehouse, equipment compartment is arranged on internal body, and thick wing is arranged on the middle and upper part of body, and thick wing is hollow structure, symmetrical on body, and leading edge lower portion has bar shaped induction opening, and trailing edge upper surface has L v notch v, and thick wing is inner symmetrical is provided with ducted fan, cross section is the vane cluster of crescent shape, and ducted fan group is corresponding with its crescent shape concave surface, and ducted fan group ducted fan quantity can be several, and the ducted fan rotation direction of left and right ducted fan group is contrary, quantity is identical, and the control apparatus of ducted fan group is connected with ducted fan group, steering wheel respectively with ducted fan group control apparatus, wing flap, vertical tail is connected, equipment compartment, power storehouse, steering wheel, ducted fan group, drive motor electrically connects, and equipment compartment comprises navigation parts, flight-control component, communication component, power storehouse is that inside is provided with secondary battery and has the power storehouse of charging unit, and alighting gear can be ski type, roller type, pontoon type, body surface is provided with LED display, audio alerting unit, this unmanned transport plane also can be by oil, electricity mixed power is powered can increase voyage and airborne period.
The advantage of this programme is that simple structure, high-mobility, multipurpose, wheeled vehicle, low-altitude low-speed, short take-off and landing (STOL), cost are low, the unmanned transport plane of function admirable.
accompanying drawing illustrates:
The machine of facing (schematic diagram) of Fig. 1, a kind of unmanned transport plane
The birds-eye view (schematic diagram) of Fig. 2, a kind of unmanned transport plane
The lateral plan (schematic diagram) of Fig. 3, a kind of unmanned transport plane
The front elevation (schematic diagram) of Fig. 4, thick wing
The birds-eye view (schematic diagram) of Fig. 5, thick wing
Fig. 6, be the A-A cross section view of Fig. 4
Fig. 7, be the B-B cross section view of Fig. 4
Fig. 8, be thick wing main duct fan produce lift principle schematic (ducted fan air extractor duct dips down, and can increase lift)
Fig. 9, be the schematic diagram that thick wing main duct fan air extractor duct dips down
In figure: 1 traction electric propeller, 2 drive motor, 3 thick wings, 4 farm implements articulated devices, 5 vertical tails, the flat wing of 6T shape water tail, fixed-wing before 7 wing flaps, 8,9 alighting gears, 10 bodies, 11 bar shaped induction openings, 12 equipment compartments, 13 power storehouses, 14 steering wheels, 15 cross sections are crescent shape vane cluster, 16 ducted fan groups, 17 ducted fan group control apparatuss, 18 ducted fans, 19 ducted fan group connection boxes, 20 bearing pins, 21 cross sections are crescent shape vane cluster concave surface, 22 cabins
detailed description of the invention:
Embodiment 1: install 1 traction electric screw slurry on 10 bodies, 2 drive motor, 5 vertical tails, 6T shape tailplane, fixed-wing before 8, 9 alighting gears, 4 farm implements articulated devices, 3, thick wing, at 10 internal bodies, 12 equipment compartments are installed, 13 power storehouses, 14 cabin machines, installing 15 cross sections in 3 thick wing inside is crescent shape vane cluster, 16 ducted fan groups, 17 ducted fan group control apparatuss, 7 wing flaps and 6T shape tailplane, before 8, fixed-wing is connected, 12 equipment compartments, 13 power storehouses, 14 steering wheels, 2 drive motor, 17 ducted fan group control apparatuss electrically connect, run by surface instruction.
Claims (5)
1. a unmanned transport plane, by front fixed-wing, T-shaped tailplane, vertical tail, wing flap, body, traction electric propeller, drive motor, thick wing, ducted fan group, cross section is the vane cluster of crescent shape, ducted fan group control apparatus, steering wheel, alighting gear, power storehouse, equipment compartment, farm implements articulated device forms, and it is characterized in that: traction electric propeller, front fixed-wing is arranged on the front portion of body, T-shaped tailplane, vertical tail is arranged on the rear portion of body, alighting gear, farm implements articulated device is arranged on the bottom of body, power storehouse, equipment compartment is arranged on internal body, and thick wing is arranged on the middle and upper part of body, and thick wing is hollow structure, symmetrical on body, leading edge lower portion has bar shaped induction opening, and trailing edge upper surface has L v notch v, and thick wing is inner symmetrical is provided with ducted fan group, cross section is the vane cluster of crescent shape, ducted fan group is corresponding with the concave surface of crescent shape, ducted fan group ducted fan quantity can be several, the contrary quantity of ducted fan rotation direction of left and right ducted fan group is identical, the control apparatus of ducted fan group is connected with ducted fan group, steering wheel respectively with ducted fan group control apparatus, wing flap, vertical tail is connected, equipment compartment, power storehouse, steering wheel, ducted fan group, drive motor electrically connects.
2. the unmanned transport plane of one according to claim 1 is further characterized in that: described equipment compartment comprises navigation parts, flight-control component and communication component.
3. the unmanned transport plane of one according to claim 1 is further characterized in that: described power storehouse is the power storehouse that inside is provided with secondary battery and charging unit.
4. the unmanned transport plane of one according to claim 1 is further characterized in that: described alighting gear is ski type or roller type or pontoon type.
5. the unmanned transport plane of one according to claim 1 is further characterized in that its body surface is provided with LED display and has audio alerting unit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520402150.5U CN204895861U (en) | 2015-06-04 | 2015-06-04 | Unmanned cargo airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520402150.5U CN204895861U (en) | 2015-06-04 | 2015-06-04 | Unmanned cargo airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204895861U true CN204895861U (en) | 2015-12-23 |
Family
ID=54918059
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520402150.5U Withdrawn - After Issue CN204895861U (en) | 2015-06-04 | 2015-06-04 | Unmanned cargo airplane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204895861U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105667783A (en) * | 2016-02-29 | 2016-06-15 | 南京信息工程大学 | Tiliting fixed-wing water unmanned plane with power structure |
| CN106275421A (en) * | 2015-06-04 | 2017-01-04 | 陈志石 | A kind of unmanned transporter |
| CN106741979A (en) * | 2017-03-09 | 2017-05-31 | 杭州米为科技有限公司 | A kind of drive mechanism for aircraft |
| CN108263607A (en) * | 2016-12-30 | 2018-07-10 | 珠海天空速递有限公司 | Unmanned aircraft with combined type lift member |
| CN109808530A (en) * | 2019-02-20 | 2019-05-28 | 武汉理工大学 | A kind of vehicle-mounted multi-rotor unmanned aerial vehicle charging unit |
-
2015
- 2015-06-04 CN CN201520402150.5U patent/CN204895861U/en not_active Withdrawn - After Issue
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106275421A (en) * | 2015-06-04 | 2017-01-04 | 陈志石 | A kind of unmanned transporter |
| CN106275421B (en) * | 2015-06-04 | 2018-06-01 | 陈志石 | A kind of unmanned transporter |
| CN105667783A (en) * | 2016-02-29 | 2016-06-15 | 南京信息工程大学 | Tiliting fixed-wing water unmanned plane with power structure |
| CN108263607A (en) * | 2016-12-30 | 2018-07-10 | 珠海天空速递有限公司 | Unmanned aircraft with combined type lift member |
| CN108263607B (en) * | 2016-12-30 | 2024-04-12 | 珠海天空速递有限公司 | Unmanned aerial vehicle with composite lift elements |
| CN106741979A (en) * | 2017-03-09 | 2017-05-31 | 杭州米为科技有限公司 | A kind of drive mechanism for aircraft |
| CN106741979B (en) * | 2017-03-09 | 2023-08-15 | 杭州米为科技有限公司 | Transmission structure for aircraft |
| CN109808530A (en) * | 2019-02-20 | 2019-05-28 | 武汉理工大学 | A kind of vehicle-mounted multi-rotor unmanned aerial vehicle charging unit |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20151223 Effective date of abandoning: 20180601 |
|
| AV01 | Patent right actively abandoned |