CN211711079U - Task load carrying/throwing wing - Google Patents
Task load carrying/throwing wing Download PDFInfo
- Publication number
- CN211711079U CN211711079U CN201922351609.4U CN201922351609U CN211711079U CN 211711079 U CN211711079 U CN 211711079U CN 201922351609 U CN201922351609 U CN 201922351609U CN 211711079 U CN211711079 U CN 211711079U
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- wing
- cabin
- task load
- slide rail
- task
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Abstract
The utility model discloses a task load delivery/input wing, wing wingtip be provided with task load cabin, task load cabin in be provided with the slide rail, the slide rail on be provided with a plurality of detachable sliders, the slider be connected with the driving motor who sets up in task load cabin, the slide rail end be provided with and put in spacing lock, put in spacing lock and launch the input device with the setting in task load cabin and be connected, the utility model discloses carry/input the cabin with the wing outer segment as task load, can be used to be difficult to arrange the aircraft of burying the input cabin in the fuselage, bury the cabin in as one kind, can avoid external influence to aircraft aerodynamic characteristic. The launching is carried out towards the wing tip, so that the collision between the launched mission load and the airplane can be greatly avoided.
Description
Technical Field
The utility model belongs to aircraft design field especially relates to a task load delivery/input wing.
Background
Aircraft carrying drop-on mission loads are typically carried/dropped via externally hung or fuselage embedded cabins. The external hanging mode can affect the aerodynamic characteristics of the aircraft platform. Although the aerodynamic characteristics of the aircraft platform are not affected by the embedded cabin of the aircraft body, the embedded cabin of the aircraft body occupies the space of the aircraft body, breaks the continuous structure of the aircraft body, and is difficult to safely separate the task load.
SUMMERY OF THE UTILITY MODEL
The utility model aims at: the load carrying/releasing wing can avoid the influence of the external hanging on an airplane platform and realize the carrying and reliable releasing of task loads under the condition of not changing the continuous structure of an airplane body.
The technical scheme of the utility model:
the utility model provides a task load delivery/puts in wing, includes the wing, the wing wingtip be provided with task load cabin, task load cabin in be provided with the slide rail, the slide rail on be provided with carry slider, carry position locking mechanical system, transport mechanism 8, put in position locking mechanical system, put in the mechanism, transport mechanism and conveying motor be connected, put in the mechanism and put in the motor and be connected, the slide rail outer end be provided with put in spacing and slider recovery unit.
The upper end of the outer side of the task load cabin is hinged with an openable wingtip cabin door.
When the wingtip cabin door rotates along the upper end of the outer side of the mission load cabin, the opening angle is not less than 135 degrees.
The task load cabin is of a rectangular structure and is integrally designed with a force bearing structure of the wing.
The slide rail is arranged at the top in the task load cabin along the wingspan direction.
The slider is provided with a hook.
The utility model has the advantages that: the utility model provides a pair of wing is put in task load delivery, regard the wing outer segment as task load delivery/put in the cabin, can be used to arrange the aircraft of formula of burying in the fuselage and put in the cabin with being difficult to. As an embedded cabin, the influence of external hanging on the aerodynamic characteristics of the airplane can be avoided. The launching is carried out towards the wing tip, so that the collision between the launched mission load and the airplane can be greatly avoided.
Drawings
Figure 1 is a schematic structural view of the present invention,
FIG. 2 is a schematic view of a slide rail structure;
in the figure, the device comprises a wing 1, a wing 2, a wingtip cabin door 3, a mission load cabin 4, a slide rail 5, a conveying motor 6, a mounting slide block 7, a mounting position locking mechanism 8, a conveying mechanism 9, a throwing position locking mechanism 10, a throwing mechanism 11, a throwing motor 12, a throwing limit and slide block recovery device.
Detailed Description
The utility model discloses set up the delivery/input cabin of putting in task load in 1 outer segment of wing inside, task load accessible wingtip hatch door 2 launches the input. The mission load can be carried and launched outwards through the slide rails 4 arranged inside the wings 1. The delivery cabin is arranged in the outer section of the wing 1, the appearance of the wing 1 is not changed, and the aerodynamic characteristics of the whole aircraft are not affected. Due to the fact that the launching is carried out from the wingtips, the probability of collision between the launched mission load and the airplane is small, and safety is high. The wing carrying/launching cabin is suitable for airplanes which are difficult to arrange an embedded launching cabin on the airplane body, and is suitable for small launching type task loads (such as subminiature unmanned planes).
The present invention is described in further detail below with reference to the attached drawings.
A mission load carrying/launch wing comprising: the device comprises a wing 1, a wing tip cabin door 2, a task load cabin 3, a slide rail 4, a conveying motor 5, a hanging slide block 6, a hanging position locking mechanism 7, a conveying mechanism 8, a throwing position locking mechanism 9, a throwing mechanism 10, a throwing motor 11 and a throwing limiting and slide block recycling device 12.
The wingtip of the wing 1 is provided with a task load cabin 3, the wingtip cabin door 2 is arranged outside the wingtip of the wing 1, a slide rail 4 is arranged in the task load cabin 3, a hanging slide block 6, a hanging position locking mechanism 7, a conveying mechanism 8, a throwing position locking mechanism 9 and a throwing mechanism 10 are arranged on the slide rail 4, the conveying mechanism 8 is connected with a conveying motor 5, the throwing mechanism 10 is connected with a throwing motor 11, and the outer end of the slide rail 4 is provided with a throwing limiting and slide block recycling device 12.
The task load is mounted on the slide rail 4 through the mounting slide block 6 and is fixed through the mounting position locking mechanism 7, so that the position fixation in the carrying process is realized.
When the aircraft is thrown, the wingtip cabin door 2 is opened, the conveying mechanism 8 is controlled by the conveying motor 5 to move to the mounting position locking mechanism 7 on the outermost side, the locking mechanism 7 is unlocked by the conveying mechanism 8 and is connected with the mounting slide block 6 on the outermost side, then the mounting slide block 6 and the task load on the outermost side are conveyed to the throwing position locking mechanism 9, the throwing position locking mechanism 9 locks the mounting slide block 6 at a throwing position, and the conveying mechanism 8 is separated from the mounting slide block 6.
After the releasing position locking mechanism 9 is locked, the releasing motor 11 controls the releasing mechanism 10 to move to the releasing position locking mechanism 9, the releasing mechanism 10 unlocks the releasing position locking mechanism 9, and the releasing mechanism is connected with the mounting slide block 6.
After the preparation of throwing is completed, the throwing mechanism 10 is controlled by the throwing motor 11, the hanging slide block 6 and the task load accelerate towards the wing tip along the slide rail, when the throwing mechanism 10 and the hanging slide block 6 accelerate to the position of the throwing limit and slide block recovery device 12, the outward movement is stopped, the task load and the hanging slide block 6 are automatically separated under the acceleration, and after the task load is thrown towards the wing tip, the throwing limit and slide block recovery device 12 moves the hanging slide block 6 out of the throwing limit position.
And repeating the steps to realize the continuous wing tip throwing of the multiple task loads.
Claims (6)
1. A mission load carrying/launch wing, characterized by: including wing (1), wing (1) wingtip be provided with task load cabin (3), task load cabin (3) in be provided with slide rail (4), slide rail (4) on be provided with carry slider (6), carry position locking mechanical system (7), transport mechanism (8), put in position locking mechanical system (9), put in mechanism (10), transport mechanism (8) be connected with conveying motor (5), put in mechanism (10) and put in motor (11) and be connected, slide rail (4) outer end be provided with put in spacing and slider recovery unit (12).
2. A mission load carrying/delivering wing as claimed in claim 1, wherein: the upper end of the outer side of the mission load cabin (3) is hinged with an openable wingtip cabin door (2).
3. A mission load carrying/delivering wing as claimed in claim 2, wherein: when the wingtip cabin door (2) rotates along the upper end of the outer side of the mission load cabin (3), the opening angle is not less than 135 degrees.
4. A mission load carrying/delivering wing as claimed in claim 1, wherein: the task load cabin (3) is of a rectangular structure and is integrally designed with a force bearing structure of the wing (1).
5. A mission load carrying/delivering wing as claimed in claim 1, wherein: the slide rail (4) is arranged at the top in the task load cabin (3) along the wingspan direction.
6. A mission load carrying/delivering wing as claimed in claim 1, wherein: the hanging slide block (6) is provided with a hook.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922351609.4U CN211711079U (en) | 2019-12-24 | 2019-12-24 | Task load carrying/throwing wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201922351609.4U CN211711079U (en) | 2019-12-24 | 2019-12-24 | Task load carrying/throwing wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN211711079U true CN211711079U (en) | 2020-10-20 |
Family
ID=72819840
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201922351609.4U Active CN211711079U (en) | 2019-12-24 | 2019-12-24 | Task load carrying/throwing wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN211711079U (en) |
-
2019
- 2019-12-24 CN CN201922351609.4U patent/CN211711079U/en active Active
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