CN211391718U - Can range upon range of aircraft - Google Patents
Can range upon range of aircraft Download PDFInfo
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- CN211391718U CN211391718U CN201922413375.1U CN201922413375U CN211391718U CN 211391718 U CN211391718 U CN 211391718U CN 201922413375 U CN201922413375 U CN 201922413375U CN 211391718 U CN211391718 U CN 211391718U
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- stackable
- rotor
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Abstract
The utility model discloses a can range upon range of aircraft, including fuselage, rotor, frame. The rotor is articulated with the rotating part of the fuselage. The outer frame is fixedly connected with the machine body. The utility model discloses the range upon range of aircraft size that technical scheme provided is little, easily stores the transportation, can conveniently realize the range upon range of storage between aircraft and the aircraft.
Description
Technical Field
The utility model relates to a rotor craft field, in particular to can range upon range of aircraft.
Background
Compared with aircrafts such as fixed wings and the like, the rotor craft is more stable in flying, can be rapidly switched among various flying states such as hovering, side flying, back flying and the like, has good take-off and landing and maneuvering performances, is suitable for fixed-point reconnaissance, aerial photography, surveying and mapping and other tasks, and has wide military and civil application.
The traditional rotor craft adopts a frameless structure, so that the craft can be stored only singly, and a great deal of inconvenience is brought to carrying and transporting processes. Novel can range upon range of aircraft adopts the frame structural style that can range upon range of, can make full use of effective space for range upon range of back rotor craft is more convenient for carry in batches and the transportation.
Disclosure of Invention
The utility model aims at overcoming above-mentioned problem, provide a range upon range of aircraft.
In order to achieve the purpose, the utility model discloses a method is: a stackable aircraft comprises a fuselage, a rotor wing and an outer frame. Wherein, the rotor is articulated with the rotary part of fuselage. The outer frame is fixedly connected with the machine body.
As the optimization of the utility model, the outer frame is round; the upper surface of the outer frame is concave, and the lower surface of the outer frame is convex. The stackable aircrafts and the stackable aircrafts can be stacked and stored, and the outer frame is a bearing part which is stacked and stored.
Has the advantages that:
the utility model discloses the range upon range of aircraft that technical scheme provided is simple reliable, can conveniently realize the range upon range of aircraft, does benefit to depositing and transporting of aircraft.
Drawings
FIG. 1 is a schematic illustration of a stackable aircraft;
FIG. 2 is a schematic front view of a stackable aircraft;
FIG. 3 is a cross-sectional schematic view of a stackable aircraft.
FIG. 4 is a layup schematic of a layup-capable aircraft.
Fig. 1, 2, 3 and 4 show the frame 1, fuselage, 2, rotor, 3, outer frame.
Detailed Description
The present invention will be further clarified by the following embodiments with reference to the attached drawings, which are implemented on the premise of the technical solution of the present invention, and it should be understood that these embodiments are only used for illustrating the present invention and are not used for limiting the scope of the present invention.
Example 1:
fig. 1 and fig. 2 are a schematic view and a front view of a stackable aircraft according to the present disclosure, respectively. The embodiment discloses a stackable aircraft, which comprises a fuselage 1, a rotor 2 and an outer frame 3. Wherein, rotor 2 is articulated with the rotary part of fuselage 1. The machine body 1 is fixedly connected with the outer frame 3.
Fig. 3 and 4 are a schematic cross-sectional view and a schematic laminated view of the stackable aircraft disclosed for the present embodiment, respectively. As the optimization of the utility model, the outer frame 3 is round; the upper surface of the outer frame 3 is concave, and the lower surface of the outer frame 3 is convex. The stackable aircrafts and the stackable aircrafts can be stacked and stored, and the outer frame 3 is a bearing part which is stacked and stored.
The technical means disclosed by the scheme of the utility model is not limited to the technical means disclosed by the technical means, but also comprises the technical scheme formed by the arbitrary combination of the technical characteristics. The foregoing is a detailed description of the present invention, and it should be noted that, for those skilled in the art, a plurality of modifications and decorations can be made without departing from the principle of the present invention, and these modifications and decorations are also considered as the protection scope of the present invention.
Claims (2)
1. A stackable aircraft, characterized by: comprises a fuselage (1), a rotor wing (2) and an outer frame (3); the rotor (2) is hinged with a rotating part of the fuselage (1); the machine body (1) is fixedly connected with the outer frame (3).
2. The stackable aircraft of claim 1, wherein: the outer frame (3) is circular; the upper surface of the outer frame (3) is concave inwards; the lower part of the outer frame (3) protrudes outwards; the outer frame (3) and the outer frame (3) can be stacked for storage, and the outer frame (3) is a bearing part for stacked storage.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922413375.1U CN211391718U (en) | 2019-12-29 | 2019-12-29 | Can range upon range of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922413375.1U CN211391718U (en) | 2019-12-29 | 2019-12-29 | Can range upon range of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211391718U true CN211391718U (en) | 2020-09-01 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922413375.1U Active CN211391718U (en) | 2019-12-29 | 2019-12-29 | Can range upon range of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211391718U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114132520A (en) * | 2021-12-24 | 2022-03-04 | 南京航空航天大学 | Stacking embedding device for unmanned aerial vehicle and stacking method thereof |
-
2019
- 2019-12-29 CN CN201922413375.1U patent/CN211391718U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114132520A (en) * | 2021-12-24 | 2022-03-04 | 南京航空航天大学 | Stacking embedding device for unmanned aerial vehicle and stacking method thereof |
| CN114132520B (en) * | 2021-12-24 | 2023-06-27 | 南京航空航天大学 | Stacking and jogging device for unmanned aerial vehicle and stacking method thereof |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20221202 Address after: Room 205, Building E, Science Park, Qinhuai Silicon Lane University, China Southern Airlines, No. 29, Yudao Street, Qinhuai District, Nanjing, Jiangsu, 210000 Patentee after: Nanjing Xunhang Technology Co.,Ltd. Address before: No.29, Jiangjun Avenue, economic and Technological Development Zone, Jiangning District, Nanjing, Jiangsu Province, 210000 Patentee before: Nanjing wing Aviation Technology Co.,Ltd. |