CN109808870A - A kind of fast assembling disassembling structure of the vertical horizontal tail connection of unmanned plane - Google Patents
A kind of fast assembling disassembling structure of the vertical horizontal tail connection of unmanned plane Download PDFInfo
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- CN109808870A CN109808870A CN201910256455.2A CN201910256455A CN109808870A CN 109808870 A CN109808870 A CN 109808870A CN 201910256455 A CN201910256455 A CN 201910256455A CN 109808870 A CN109808870 A CN 109808870A
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- attachment base
- vertical fin
- horizontal
- horizontal tail
- stabilizer assemblies
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Abstract
The invention discloses a kind of fast assembling disassembling structures of the vertical horizontal tail connection of unmanned plane；By preceding connection Quick-release pin, afterwards connect Quick-release pin, attachment base forms after attachment base and horizontal tail before attachment base, horizontal tail after attachment base, vertical fin before vertical fin；The forward and backward attachment base of vertical fin is connected with vertical fin component respectively, and both ends vertical fin component respectively has the forward and backward attachment base of vertical fin.Attachment base is connected with horizontal stabilizer assemblies respectively before and after horizontal tail.There are two attachment bases after preceding attachment base and two to be located at horizontal stabilizer assemblies both ends for horizontal stabilizer assemblies.When unmanned plane expansion, horizontal stabilizer assemblies are placed between the vertical fin of both ends, mobile horizontal stabilizer assemblies cooperate the pin hole of the pin hole of the forward and backward attachment base of the horizontal tail of both ends of the surface and the forward and backward attachment base of vertical fin of vertical fin component, and insert front and back and connect Quick-release pin, realize the installation of horizontal stabilizer assemblies.When unmanned plane is removed the time receiving, the front and back for pulling up both ends respectively connects Quick-release pin, realizes the separation of horizontal stabilizer assemblies and vertical fin component.Fast assembling disassembling structure maintenance is simple, operation is convenient.
Description
Technical field
The present invention relates to air vehicle technique fields, specifically, being related to a kind of fast assembling-disassembling of vertical horizontal tail connection of unmanned plane
Structure.
Background technique
Unmanned plane has many advantages, such as that strong small in size, low cost, environmental suitability, using flexible, operating efficiency are high.Especially exist
When executing uninteresting, long-time task, unmanned plane has man-machine incomparable advantage.Unmanned plane has been widely used for battlefield
It scouts, in pinpoint target monitoring, Strike and emergency disaster relief.Tactics type small and medium size unmanned aerial vehicles mostly use rocket assist to emit
Mode has maneuverability, does not depend on airfield runway while can implement prominent preceding deployment according to wartime situation.Therefore it is required that its nothing
Man-machine system needs to have stronger state transfer capability, and each main separation unit can be in wartime quick assembly and disassembly.
Existing unmanned plane horizontal tail is connect with vertical fin mostly uses bolt fastening, and disassembly process must rely on tool, and dismount
Process needs to tighten by horizontal tail with vertical fin attachment lug mounting hole to it and using fastening bolt, complex installation process and used time compared with
It is long.Moreover, when using bolt fastening, it is necessary to the screw threads such as split pin or screw thread fastening glue be used to loosen measure to prevent fastening bolt
It loosens.In order to improve UAV system expansion or remove the rate of producing effects, flight servicing time is saved, needs to design a kind of dismounting letter
The fast assembling-disassembling unmanned plane single, disassembly and assembly time is short hangs down, horizontal tail connection structure.
Summary of the invention
In order to avoid the shortcomings of the prior art, the present invention proposes a kind of fast assembling-disassembling knot of vertical horizontal tail connection of unmanned plane
Structure；The fast assembling disassembling structure, which has, adapts to that UAV system rapid deployment, quickly to remove receipts, maintenance simple, easy to use
Feature.
The technical solution adopted by the present invention to solve the technical problems is: including horizontal stabilizer assemblies and vertical fin component, feature
It is before connecting Quick-release pin before further including, connecting Quick-release pin, vertical fin afterwards after attachment base, vertical fin attachment base before attachment base, horizontal tail, puts down
Attachment base after tail；The horizontal stabilizer assemblies are located between two vertical fin components, and horizontal stabilizer assemblies both ends are connected with before two groups of horizontal tails respectively
Attachment base is connected after seat, horizontal tail, and vertical fin component is connected with attachment base after attachment base, vertical fin before two groups of vertical fins respectively, horizontal stabilizer assemblies
Before the horizontal tail of both ends of the surface after attachment base and horizontal tail before the installation pin hole of attachment base and the vertical fin of vertical fin component after attachment base and vertical fin
The installation pin hole cooperation of attachment base is opposite, and connection Quick-release pin and rear connection Quick-release pin before inserting respectively, realize horizontal stabilizer assemblies with
The installation of two vertical fin components；When unmanned plane is removed the time receiving, the preceding connection Quick-release pin for pulling up two vertical fin components respectively is connected with rear
Quick-release pin removes horizontal stabilizer assemblies, realizes the separation of horizontal stabilizer assemblies and two vertical fin components.
The installation pin hole of attachment base and the vertical fin group after attachment base and horizontal tail before the horizontal tail of the horizontal stabilizer assemblies both ends of the surface
Before the vertical fin of part after attachment base and vertical fin attachment base the installation of installation pin hole confronting coaxial.
Beneficial effect
A kind of fast assembling disassembling structure of the vertical horizontal tail connection of unmanned plane proposed by the present invention；By preceding connection Quick-release pin, rear connection
Attachment base forms after attachment base and horizontal tail before attachment base, horizontal tail after attachment base, vertical fin before Quick-release pin, vertical fin；The forward and backward connection of vertical fin
Seat is connected with vertical fin component respectively, and left and right vertical fin respectively has the forward and backward attachment base of vertical fin.Before and after horizontal tail attachment base respectively with horizontal stabilizer assemblies
It is connected.Horizontal stabilizer assemblies are located at horizontal stabilizer assemblies both ends of the surface there are two attachment base after preceding attachment base and two.When unmanned plane is unfolded
When, horizontal stabilizer assemblies are placed between the vertical fin of left and right, and mobile horizontal stabilizer assemblies make to connect after attachment base and horizontal tail before the horizontal tails of both ends of the surface
The pin hole of seat is aligned with the pin hole of attachment base after attachment base before the vertical fin of vertical fin component and vertical fin, and is inserted front and back and connected quick-release
Pin, realizes the installation of horizontal stabilizer assemblies.When unmanned plane is removed the time receiving, the front and back for pulling up both sides respectively connects Quick-release pin, realizes horizontal tail group
The separation of part and vertical fin component.Fast assembling disassembling structure adapt to UAV system rapid deployment, quickly remove receipts, maintenance it is simple,
It is easy to use.
The fast assembling disassembling structure of the vertical horizontal tail connection of unmanned plane of the present invention, is a kind of using abutting joint seat, quick-release pin connection
Unmanned plane is flat, vertical fin fast assembling disassembling structure.The structure is simple, light-weight；Constitutional detail is less, easy to use, removes receipts or exhibition
ETAD expected time of arrival and departure is short；The dismounting of entire horizontal stabilizer assemblies and vertical fin component can be realized by plugging Quick-release pin, greatly reduce unmanned plane system
It system flight preparation and removes between the time receiving.
Detailed description of the invention
With reference to the accompanying drawing with embodiment to a kind of unmanned plane of the present invention hang down the fast assembling disassembling structure that horizontal tail connects make into
One step is described in detail.
Fig. 1 is horizontal tail vertical fin fast assembling-disassembling schematic diagram of the invention.
Fig. 2 is that horizontal tail vertical fin of the invention dismantles schematic diagram.
Fig. 3 is the fast assembling disassembling structure schematic diagram of the vertical horizontal tail connection of unmanned plane of the present invention.
In figure:
It is connected before 1. before connecting 3. vertical fin of Quick-release pin after Quick-release pin 2. after 4. vertical fin of attachment base before 5. horizontal tail of attachment base
Attachment base after 6. horizontal tail of attachment base
Specific embodiment
The present embodiment is a kind of fast assembling disassembling structure of vertical horizontal tail connection of unmanned plane.
Refering to fig. 1~Fig. 3, the present embodiment are related to a kind of unmanned plane tailplane and vertical tail fast assembling disassembling structure, adopt
With abutting joint seat, the unmanned plane horizontal tail of quick-release pin connection, vertical fin fast assembling-disassembling.The fast assembling-disassembling knot of the vertical horizontal tail connection of unmanned plane
Structure is by attachment base after attachment base 3, vertical fin before horizontal stabilizer assemblies, vertical fin component and preceding connection Quick-release pin 1, rear connection Quick-release pin 2, vertical fin
4, attachment base 6 forms after attachment base 5, horizontal tail before horizontal tail.Horizontal stabilizer assemblies are located between two vertical fin components；Horizontal stabilizer assemblies both ends point
Be not fixedly connected with attachment base 6 after attachment base 5, horizontal tail before two groups of horizontal tails, vertical fin component respectively with attachment base 3 before two groups of vertical fins,
Attachment base 4 is connected after vertical fin；It the installation pin hole of attachment base 6 and hangs down after attachment base 5 and horizontal tail before the horizontal tail of horizontal stabilizer assemblies both ends of the surface
Before the vertical fin of tail component after attachment base 3 and vertical fin attachment base 4 the cooperation of installation pin hole, and 1 He of Quick-release pin is connected before inserting respectively
Quick-release pin 2 is connected afterwards, realizes the installation of horizontal stabilizer assemblies and vertical fin component.When unmanned plane is removed the time receiving, vertical fin component two is pulled up respectively
The preceding connection Quick-release pin 1 on side and rear connection Quick-release pin 2, remove horizontal stabilizer assemblies, realize the separation of horizontal stabilizer assemblies and vertical fin component.
In the present embodiment, the installation pin hole of attachment base 6 and hang down after attachment base 5 and horizontal tail before the horizontal tail of horizontal stabilizer assemblies both ends of the surface
The installation pin hole of attachment base 4 is corresponding after attachment base 3 and vertical fin before the vertical fin of tail component, and is co-axially mounted.
When installation operation, when unmanned plane expansion, horizontal stabilizer assemblies are placed between two vertical fin components；Mobile horizontal tail group
Part makes the installation pin hole and two vertical fin components of attachment base 6 after attachment base 5 and horizontal tail before the horizontal tail of two end faces of horizontal stabilizer assemblies
Vertical fin before attachment base 3 it is opposite with the installation pin hole of attachment base 4 after vertical fin, then respectively inserting before connection Quick-release pin 1 and after connect
Quick-release pin 2 is connect, realizes the installation of horizontal stabilizer assemblies.When unmanned plane is removed the time receiving, the preceding connection Quick-release pin 1 for pulling up both sides respectively connects with after
Quick-release pin 2 is connect, horizontal stabilizer assemblies are removed, realizes the separation of horizontal stabilizer assemblies and vertical fin component.Fast assembling disassembling structure adapts to unmanned plane system
System rapid deployment, quickly to remove receipts, maintenance simple, easy to use.
Claims (2)
- The fast assembling disassembling structure of horizontal tail connection 1. a kind of unmanned plane hangs down, including horizontal stabilizer assemblies and vertical fin component, it is characterised in that: also Including preceding connection Quick-release pin, afterwards connects Quick-release pin, connects after attachment base, horizontal tail before attachment base, horizontal tail before vertical fin after attachment base, vertical fin Joint chair；The horizontal stabilizer assemblies are located between two vertical fin components, horizontal stabilizer assemblies both ends respectively with attachment base, horizontal tail before two groups of horizontal tails Attachment base is connected afterwards, and vertical fin component is connected with attachment base after attachment base, vertical fin before two groups of vertical fins respectively, horizontal stabilizer assemblies both ends of the surface Attachment base after attachment base and vertical fin before the installation pin hole of attachment base and the vertical fin of vertical fin component after attachment base and horizontal tail before horizontal tail It is opposite that pin hole cooperation is installed, and connection Quick-release pin and rear connection Quick-release pin before inserting respectively, realizes horizontal stabilizer assemblies and two vertical fins The installation of component；When unmanned plane is removed the time receiving, the preceding connection Quick-release pin for pulling up two vertical fin components respectively connects Quick-release pin with rear, takes Lower horizontal stabilizer assemblies realize the separation of horizontal stabilizer assemblies and two vertical fin components.
- The fast assembling disassembling structure of horizontal tail connection 2. unmanned plane according to claim 1 hangs down, it is characterised in that: the horizontal tail group Before the horizontal tail of part both ends of the surface after attachment base and horizontal tail before the installation pin hole of attachment base and the vertical fin of the vertical fin component attachment base and The installation pin hole confronting coaxial installation of attachment base after vertical fin.
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910256455.2A CN109808870A (en) | 2019-04-01 | 2019-04-01 | A kind of fast assembling disassembling structure of the vertical horizontal tail connection of unmanned plane |
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| Application Number | Priority Date | Filing Date | Title |
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| CN201910256455.2A CN109808870A (en) | 2019-04-01 | 2019-04-01 | A kind of fast assembling disassembling structure of the vertical horizontal tail connection of unmanned plane |
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| CN109808870A true CN109808870A (en) | 2019-05-28 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
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| CN112880640A (en) * | 2021-01-18 | 2021-06-01 | 西北工业大学 | Double-tail-support layout unmanned aerial vehicle horizontal measuring device and using method |
| US20220234717A1 (en) * | 2019-09-05 | 2022-07-28 | Autel Robotics Co., Ltd. | Wing detachment assembly and aerial vehicle |
| CN115009508A (en) * | 2022-08-08 | 2022-09-06 | 成都飞机工业（集团）有限责任公司 | Zero-length launching unmanned aerial vehicle jettisonable vertical fin structure |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| US20220234717A1 (en) * | 2019-09-05 | 2022-07-28 | Autel Robotics Co., Ltd. | Wing detachment assembly and aerial vehicle |
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| CN115009508A (en) * | 2022-08-08 | 2022-09-06 | 成都飞机工业（集团）有限责任公司 | Zero-length launching unmanned aerial vehicle jettisonable vertical fin structure |
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Application publication date: 20190528 |