CN205819543U - A kind of composite wing unmanned plane wing of fast demountable - Google Patents
A kind of composite wing unmanned plane wing of fast demountable Download PDFInfo
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- CN205819543U CN205819543U CN201620803195.8U CN201620803195U CN205819543U CN 205819543 U CN205819543 U CN 205819543U CN 201620803195 U CN201620803195 U CN 201620803195U CN 205819543 U CN205819543 U CN 205819543U
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- wing
- outer section
- stage casing
- power rail
- unmanned plane
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Abstract
The utility model discloses the composite wing unmanned plane wing of a kind of fast demountable, described composite wing unmanned plane wing includes that stage casing wing, power rail and outer section of wing, described stage casing wing are connected to the not homonymy of power rail respectively with outer section of wing by attachment structure；Described attachment structure includes connecting rod and connecting hole；Also include the locking mechanism for realizing stage casing wing, outer section of both wing locks relative to position.The wing of this version not only can realize fast assembling-disassembling, each other positive lock, simultaneously, the power rail being used for fixed vertical power spin oar is set as single parts, can be by the length of power rail being set greater than stage casing wing and the width of outer section of wing, i.e. constant at wing-body width, length by motivation of adjustment bar so that what the generation of Vertical Dynamic propeller was suitable bows, faces upward moment.
Description
Technical field
This utility model relates to Flight Vehicle Structure technical field, and the composite wing particularly relating to a kind of fast demountable is unmanned
Machine wing.
Background technology
It is few that Mini-Unmanned Aerial Vehicles disposes operator rapid, required, is suitably executed emergent monitoring, open air search and rescue on foot etc.
Accidental quick response task.
In order to easy to carry, prior art is designed SUAV that use dismantled and assembled structure, meanwhile, dismantled and assembled
The design overall thinking of structure is simple for needs disassembly and assembly structure, it is reliable to connect, complete dismounting is independent of instrument.Knot to unmanned plane
Structure is made to optimize further, launches and storage efficiency with raising UAS further, reduces workload and the behaviour of operator
Make difficulty, be those skilled in the art's technical problems urgently to be resolved hurrily.
Utility model content
This utility model provides the composite wing unmanned plane wing of a kind of fast demountable, is used for solving to improve further nothing
Man-machine system launches and storage efficiency, reduces workload and the technical problem of operation easier of operator.
The composite wing unmanned plane wing of a kind of fast demountable that this utility model provides is solved by techniques below main points
Certainly problem: the composite wing unmanned plane wing of a kind of fast demountable, described composite wing unmanned plane wing includes stage casing wing, power
Bar and outer section of wing, described stage casing wing is connected to the not homonymy of power rail respectively with outer section of wing by attachment structure；
Described attachment structure includes connecting rod and connecting hole, in two parts connected by attachment structure, and connecting rod
Being fixed on the connecting end surface of one of them parts, connecting hole is arranged on the connecting end surface of another parts, and two parts lead to
Cross in connecting rod insertion connecting hole and complete to connect；
Also include the locking mechanism for realizing stage casing wing, outer section of both wing locks relative to position.
Concrete, the stage casing wing provided in this structure is connected for the fuselage with unmanned plane, and can be used for arranging automatically
The equipment such as pilot, electrical source of power, device power supply (DPS)；Outer section of wing is used for installing aileron, servosystem etc.；Before and after power rail two
End installs the propeller for producing lift.The connecting rod that connects through of three above parts inserts connecting hole, and by locking
Mechanism carries out position locking and realizes the connection of three.So, the wing of this version not only can realize fast assembling-disassembling, mutually it
Between positive lock, meanwhile, the power rail being used for fixed vertical power spin oar is set as single parts, can by will
The length of power rail is set greater than stage casing wing and the width of outer section of wing, i.e. constant at wing-body width, by adjusting
The length of power rail so that what the generation of Vertical Dynamic propeller was suitable bows, faces upward moment.
As those skilled in the art, when unmanned plane during flying, two parts of attachment structure both sides can not occur relatively
Rotating, therefore connecting rod can be arranged to square bar, triangular pelvis, spline shaft-like etc., the cross sectional shape of connecting hole mates with connecting rod,
Such as connecting rod rectangular shaft, connecting hole is rectangular opening；Simultaneously, it is possible to by using two or more attachment structures to retrain a pair
Need the form of the parts connected.
Further technical scheme is:
As the form that implements of locking mechanism, described locking mechanism includes being fixed on stage casing wing, outer section of wing two
Bar on the connecting end surface of one of which in person, described power rail is provided through the through hole of power rail both sides, stage casing
Being provided with rod aperture on the connecting end surface of another one in wing, outer section of both wing, described bar inserts rod aperture after through hole
In, described stage casing wing, outer section of both wing are additionally provided with positioner in another one, described positioner is for running through
Bar applies the resistance hindering bar to depart from rod aperture.In this locking mechanism, the obstruction bar applied by positioner is departed from
The resistance of rod aperture, realizes avoiding connecting rod by the purpose skidded off in connecting hole.
As the form that implements of above positioner, described positioner for be threadedly connected to stage casing wing, outer section
Screw in another one in both wings, the screw hole installed for screw passes through mutually with described rod aperture.In this programme, spiral shell can be passed through
Follow closely and bar applying compressive stress is achieved the goal, it is possible to a hole is set on bar, gos deep into the mistake of screw hole at screw
Cheng Zhong, screw gos deep into one end of screw hole and is inserted through in the hole of bar, plays and avoid connecting rod by the purpose skidded off in connecting hole.
As the another kind of way of realization of positioner, described positioner is for being installed on stage casing wing, outer section of wing two
Spring lock catch in another one in person.Above Spring lock catch can use the structure of spring ball pen to design, and uses at a sleeve
A piece spring and an expansion link are inside set, with the pen container of upper bush equivalent spring ball pen, expansion link equivalent pen core, and will overlap
Cylinder is fixed in stage casing wing, the outer section of middle another one of both wings, arranges a hole, in pressing Spring lock catch on bar
Pressing part, can make the end of expansion link stretch into, project through in the hole of bar.
As the another kind of way of realization of positioner, described positioner is for being installed on stage casing wing, outer section of wing two
The first permanent magnet in another one in person, the material of described bar free end is can be by the metal of described first permanent magnet absorption
Second permanent magnet attracting with described first permanent magnet is installed on the free end of material or bar.By attracting in this programme
Power, it is achieved hinder connecting rod to be skidded off by connecting hole.
The compactedness of wing each several part combination after for the benefit of wing connects, simultaneously as reducing single connecting rod stress
Technical scheme, is connected with power rail, for realizing the attachment structure that outer section wing is connected with power rail for realizing stage casing wing
Quantity be multiple；
It is made up of stage casing wing and power rail and is formed on two joint faces, in each connection by outer section of wing and power rail
On face, multiple attachment structures are distributed along the length direction of joint face.
For ease of the transmission between different wing difference parts of the circuits such as electrical source of power, device power supply (DPS) and control signal,
It is provided with electrical connector on two joint faces being made up of stage casing wing and power rail and be made up of outer section of wing and power rail,
Described electrical connector includes male corresponding to installation site and female, and described male is fixed on connected two parts wherein
On one, described female be fixed on connected two parts another on.
Owing to power rail is mainly as the fixed component of Vertical Dynamic propeller, compared to stage casing wing and outer section of wing,
Can power rail be arranged narrower, so, for ease of stage casing wing, power rail, outer section of wing are received, described connecting rod
It is both secured on power rail.
This utility model has the advantages that
The wing of this version not only can realize fast assembling-disassembling, each other positive lock, meanwhile, will be used for fixing hanging down
The power rail of direct acting wrench of a force system oar is set as single parts, can be by the length of power rail is set greater than stage casing machine
The wing and the width of outer section of wing are i.e. constant at wing-body width, by the length of motivation of adjustment bar so that Vertical Dynamic spiral
What oar generation was suitable bows, faces upward moment.
Accompanying drawing explanation
Fig. 1 is one specific embodiment of composite wing unmanned plane wing of a kind of fast demountable described in the utility model
Partial schematic diagram.
Numbering in figure is followed successively by: 1, stage casing wing, and 2, power rail, 3, outer section of wing, 411, connecting rod, 412, connect
Hole, 421, male, 422, female, 511, positioner, 512, bar.
Detailed description of the invention
Below in conjunction with embodiment, the utility model is described in further detail, but structure of the present utility model is not only
It is limited to following example.
Embodiment 1:
As it is shown in figure 1, the composite wing unmanned plane wing of a kind of fast demountable, during described composite wing unmanned plane wing includes
Section wing 1, power rail 2 and outer section of wing 3, described stage casing wing 1 and outer section of wing 3 are connected to power by attachment structure respectively
The not homonymy of bar 2；
Described attachment structure includes connecting rod 411 and connecting hole 412, in two parts connected by attachment structure,
Connecting rod 411 is fixed on the connecting end surface of one of them parts, and connecting hole 412 is arranged at the connecting end surface of another parts
On, two parts are inserted by connecting rod 411 and complete in connecting hole 412 to connect；
Also include the locking mechanism for realizing stage casing wing 1, both outer section of wings 3 lock relative to position.
Concrete, the stage casing wing 1 provided in this structure is connected for the fuselage with unmanned plane, and can be used for arranging automatically
The equipment such as pilot, electrical source of power, device power supply (DPS)；Outer section of wing 3 is used for installing aileron, servosystem etc.；Before and after power rail 2
The propeller for producing lift is installed at two ends.The connecting rod 411 that connects through of three above parts inserts connecting hole 412, and
Carry out position locking by locking mechanism and realize the connection of three.So, the wing of this version not only can realize quickly tearing open
Dress, each other positive lock, meanwhile, be set as a single portion by the power rail 2 being used for fixed vertical power spin oar
Part, can be by being set greater than stage casing wing 1 and the width of outer section of wing 3 by the length of power rail 2, i.e. at wing-body width
Constant, by the length of motivation of adjustment bar 2 so that what the generation of Vertical Dynamic propeller was suitable bows, faces upward moment.
As those skilled in the art, when unmanned plane during flying, two parts of attachment structure both sides can not occur relatively
Rotate, therefore connecting rod 411 can be arranged to square bar, triangular pelvis, spline shaft-like etc., the cross sectional shape of connecting hole 412 be connected
Bar 411 mates, and such as connecting rod 411 rectangular shaft, connecting hole 412 is rectangular opening；Simultaneously, it is possible to by using two or more
Attachment structure retrains the form of the parts of a pair needs connection.
Embodiment 2:
As it is shown in figure 1, the present embodiment is further qualified on the basis of embodiment 1: as the concrete reality of locking mechanism
Existing form, described locking mechanism includes being fixed on the connecting end surface of stage casing wing 1, the middle one of which of both outer section of wings 3
Bar 512, described power rail 2 is provided through the through hole of power rail 2 both sides, in stage casing wing 1, both outer section of wings 3
Being provided with rod aperture on the connecting end surface of another one, described bar 512 inserts in rod aperture after through hole, described stage casing wing 1,
Being additionally provided with positioner 511 in both outer section of wings 3 in another one, described positioner 511 is for applying to bar 512
Bar 512 is hindered to depart from the resistance of rod aperture.In this locking mechanism, the obstruction bar 512 applied by positioner 511 is taken off
From the resistance of rod aperture, realize avoiding connecting rod 411 by the purpose skidded off in connecting hole 412.
As the form that implements of above positioner 511, described positioner 511 is for being threadedly connected to stage casing wing
1, the screw in another one in both outer section of wings 3, the screw hole installed for screw passes through mutually with described rod aperture.In this programme,
By screw, bar 512 can be applied compressive stress to achieve the goal, it is possible on bar 512, arrange a hole, at screw
During going deep into screw hole, screw gos deep into one end of screw hole and is inserted through in the hole of bar 512, plays and avoids connecting rod 411
By the purpose skidded off in connecting hole 412.
As the another kind of way of realization of positioner 511, described positioner 511 for be installed on stage casing wing 1, outer section
Spring lock catch in another one in both wings 3.Above Spring lock catch can use the structure of spring ball pen to design, and uses one
Arranging a spring and an expansion link in individual sleeve, with the pen container of upper bush equivalent spring ball pen, expansion link is equal to pen core,
And sleeve is fixed in stage casing wing 1, the middle another one of both outer section of wings 3, bar 512 arranges a hole, pressing
Pressing part in Spring lock catch, in can making the end of expansion link stretch into, projecting through the hole of bar 512.
As the another kind of way of realization of positioner 511, described positioner 511 for be installed on stage casing wing 1, outer section
The first permanent magnet in another one in both wings 3, the material of described bar 512 free end is can be by described first permanent magnet
On the metal material of absorption or the free end of bar 512, second permanent magnet attracting with described first permanent magnet is installed.This
Scheme is passed through captivation, it is achieved hinder connecting rod 411 to be skidded off by connecting hole 412.
Embodiment 3:
As it is shown in figure 1, the present embodiment is further qualified on the basis of embodiment 1: wing after for the benefit of wing connects
The compactedness of each several part combination, simultaneously as reducing the technical scheme of single connecting rod 411 stress, is used for realizing stage casing wing
1 it is connected with power rail 2, is multiple for realizing the quantity of the attachment structure that outer section wing 3 is connected with power rail 2；
It is made up of stage casing wing 1 and power rail 2 and is formed on two joint faces, each by outer section of wing 3 and power rail 2
On joint face, multiple attachment structures are distributed along the length direction of joint face.
For ease of the transmission between different wing difference parts of the circuits such as electrical source of power, device power supply (DPS) and control signal,
It is provided with on two joint faces being made up of stage casing wing 1 and power rail 2 and be made up of outer section of wing 3 and power rail 2 electrically
Joint, described electrical connector includes male 421 corresponding to installation site and female 422, and described male 421 is fixed on connected
In one of them of two parts, described female 422 be fixed on connected two parts another on.
Owing to power rail 2 is mainly as the fixed component of Vertical Dynamic propeller, compared to stage casing wing 1 and outer section of wing
3, can power rail 2 be arranged narrower, so, for ease of stage casing wing 1, power rail 2, outer section of wing 3 are received, described
Connecting rod 411 is both secured on power rail 2.
Above content is to combine the further description that this utility model is made by concrete preferred implementation, it is impossible to recognize
Fixed detailed description of the invention of the present utility model is confined to these explanations.Common skill for this utility model art
For art personnel, other embodiments drawn under without departing from the technical solution of the utility model, should be included in this practicality
In novel protection domain.
Claims (8)
1. the composite wing unmanned plane wing of a fast demountable, it is characterised in that during described composite wing unmanned plane wing includes
Section wing (1), power rail (2) and outer section of wing (3), described stage casing wing (1) and outer section of wing (3) pass through attachment structure respectively
It is connected to the not homonymy of power rail (2)；
Described attachment structure includes connecting rod (411) and connecting hole (412), in two parts connected by attachment structure,
Connecting rod (411) is fixed on the connecting end surface of one of them parts, and connecting hole (412) is arranged at the connection end of another parts
On face, two parts are inserted by connecting rod (411) and complete in connecting hole (412) to connect；
Also include for realizing stage casing wing (1), the locking mechanism of outer section of both relative position locking of wing (3).
The composite wing unmanned plane wing of a kind of fast demountable the most according to claim 1, it is characterised in that described locking
Mechanism includes the bar (512) being fixed on the connecting end surface of stage casing wing (1), outer section of both middle one of which of wing (3),
The through hole of power rail (2) both sides it is provided through on described power rail (2), another in stage casing wing (1), both outer section of wings (3)
Being provided with rod aperture on the connecting end surface of one, described bar (512) inserts in rod aperture after through hole, described stage casing wing
(1), outer section of wing (3) both are additionally provided with positioner (511) in another one, described positioner (511) is for passing through
Bar (512) applies the resistance hindering bar (512) to depart from rod aperture.
The composite wing unmanned plane wing of a kind of fast demountable the most according to claim 2, it is characterised in that described location
Device (511) is the screw being threadedly connected in stage casing wing (1), outer section of both middle another one of wing (3), installs for screw
Screw hole pass through mutually with described rod aperture.
The composite wing unmanned plane wing of a kind of fast demountable the most according to claim 2, it is characterised in that described location
Device (511) is the Spring lock catch being installed in stage casing wing (1), outer section of both middle another one of wing (3).
The composite wing unmanned plane wing of a kind of fast demountable the most according to claim 2, it is characterised in that described location
Device (511) is the first permanent magnet being installed in stage casing wing (1), outer section of both middle another one of wing (3), described bar
(512) material of free end is to pacify on the described metal material of the first permanent magnet absorption or the free end of bar (512)
Equipped with second permanent magnet attracting with described first permanent magnet.
The composite wing unmanned plane wing of a kind of fast demountable the most according to claim 1, it is characterised in that be used for realizing
Stage casing wing (1) is connected with power rail (2), for realizing the quantity of the attachment structure that outer section wing (3) is connected with power rail (2)
It is multiple；
It is made up of stage casing wing (1) and power rail (2) and is formed on two joint faces by outer section of wing (3) and power rail (2),
On each joint face, multiple attachment structures are distributed along the length direction of joint face.
The composite wing unmanned plane wing of a kind of fast demountable the most according to claim 1, it is characterised in that by stage casing machine
It is provided with electrically on two joint faces that the wing (1) and power rail (2) form and be made up of outer section of wing (3) and power rail (2)
Joint, described electrical connector includes male (421) corresponding to installation site and female (422), described male (421) be fixed on by
Connect two parts one of them on, described female be fixed on connected two parts another on.
The composite wing unmanned plane wing of a kind of fast demountable the most according to claim 1, it is characterised in that described connection
Bar (411) is both secured on power rail (2).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620803195.8U CN205819543U (en) | 2016-07-28 | 2016-07-28 | A kind of composite wing unmanned plane wing of fast demountable |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620803195.8U CN205819543U (en) | 2016-07-28 | 2016-07-28 | A kind of composite wing unmanned plane wing of fast demountable |
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| CN205819543U true CN205819543U (en) | 2016-12-21 |
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| CN201620803195.8U Active CN205819543U (en) | 2016-07-28 | 2016-07-28 | A kind of composite wing unmanned plane wing of fast demountable |
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Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107215451A (en) * | 2017-06-16 | 2017-09-29 | 中电科芜湖通用航空产业技术研究院有限公司 | A kind of wing attachment structure of general-purpose aircraft |
| CN107651162A (en) * | 2017-09-27 | 2018-02-02 | 西安冰果智能航空科技有限公司 | A kind of unmanned plane wing quick assembling mechanism |
| CN109665101A (en) * | 2019-01-07 | 2019-04-23 | 浙江自贸区协同科技有限公司 | A kind of modularization head |
| CN111434579A (en) * | 2019-01-11 | 2020-07-21 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle tail boom quick assembly disassembly structure |
-
2016
- 2016-07-28 CN CN201620803195.8U patent/CN205819543U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107215451A (en) * | 2017-06-16 | 2017-09-29 | 中电科芜湖通用航空产业技术研究院有限公司 | A kind of wing attachment structure of general-purpose aircraft |
| CN107651162A (en) * | 2017-09-27 | 2018-02-02 | 西安冰果智能航空科技有限公司 | A kind of unmanned plane wing quick assembling mechanism |
| CN109665101A (en) * | 2019-01-07 | 2019-04-23 | 浙江自贸区协同科技有限公司 | A kind of modularization head |
| CN111434579A (en) * | 2019-01-11 | 2020-07-21 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle tail boom quick assembly disassembly structure |
| CN111434579B (en) * | 2019-01-11 | 2022-09-09 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle tail-stay quick assembly disassembly structure |
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