CN106043666B - A kind of unmanned plane wing - Google Patents
A kind of unmanned plane wing Download PDFInfo
- Publication number
- CN106043666B CN106043666B CN201610709440.3A CN201610709440A CN106043666B CN 106043666 B CN106043666 B CN 106043666B CN 201610709440 A CN201610709440 A CN 201610709440A CN 106043666 B CN106043666 B CN 106043666B
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- CN
- China
- Prior art keywords
- coverboard
- wooden case
- reinforcement
- reinforcement wooden
- upper coverboard
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/187—Ribs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/32—Wings specially adapted for mounting power plant
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
The present invention discloses a kind of unmanned plane wing, including upper coverboard and lower coverboard, the upper coverboard and lower casing back are both provided with carbon cloth, the upper coverboard and lower coverboard are bonded with carbon cloth, it is formed with cavity between the upper coverboard and lower coverboard, rib and reinforcement wooden case are provided in the cavity, the reinforcement wooden case is hollow setting, and the rib and reinforcement wooden case are bonded with carbon cloth；The unmanned plane wing weight is slim and graceful.
Description
Technical field
The present invention relates to a kind of unmanned plane wings.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without cockpit on machine, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or
Machine tool remote control station personnel are by equipment such as radars, to it into line trace, positioning, remote control, telemetering and Digital Transmission.It can be in radio
It takes off as conventional airplane under remote control or is launched with booster rocket, can also take aerial launch to by machine tool and fly.Recycling
When, the mode automatic Landing as conventional airplane landing mission can be used, can also be recycled by remote control parachute or block.It can
Repetitiousness uses multiple.It is widely used in aerial reconnaissance, monitoring, communication, antisubmarine, electronic interferences and takes photo by plane.
But current unmanned plane wing is due to needing have higher intensity, so often having inside wing a large amount of
Rib causes wing overall weight larger, it is difficult to the needs of meeting in the market.
Invention content
The technical problem to be solved in the present invention is to provide a kind of unmanned plane wings that weight is slim and graceful.
To solve the above problems, the present invention adopts the following technical scheme that：
A kind of unmanned plane wing, including upper coverboard and lower coverboard, the upper coverboard and lower casing back are both provided with carbon fiber
Wei Bu, the upper coverboard and lower coverboard are bonded with carbon cloth, and cavity is formed between the upper coverboard and lower coverboard, described
It is provided with rib and reinforcement wooden case in cavity, the reinforcement wooden case is hollow setting, and the rib and reinforcement wooden case are and carbon fiber
Wei Bu is bonded.
Preferably, the upper casing back is provided with positioning strip and fixing piece, the positioning strip is arranged in a rectangular parallelepiped shape,
Mounting groove is formed between the positioning strip, the reinforcement wooden case is inserted in mounting groove, and bar planting is provided on the fixing piece,
The bar planting is arranged through upper coverboard and lower coverboard, and the bar planting end is in semicircle shape setting, can be with by being provided with mounting groove
Convenient for users to installation, the success rate of reinforcement wooden case installation is greatly improved, and by being provided with bar planting on fixing piece,
Stable structure is reliable, and bar planting can be used for connecting fuselage so that be dismounted between fuselage and wing more convenient.
Preferably, the positioning strip, fixing piece and lower coverboard are bonded with upper coverboard, stable structure is easy to process, even
It connects reliable.
Preferably, the rib and reinforcement wooden case are perpendicular, stable structure, rib can be promoted with the cooperation of reinforcement wooden case
The stress performance of wing entirety.
Preferably, the carbon cloth is arranged in crosswise, rib can be facilitated to be installed with reinforcement wooden case, it can be effective
Material is saved, reduces cost, and reinforcement can be played the role of again.
Preferably, the mounting groove mutually agrees with reinforcement wooden case, occur after reinforcement wooden case can be prevented to be inserted into mounting groove
The case where displacement and lead to decrease in yield.
Preferably, the upper coverboard and lower coverboard are made of fiberglass outer panels and wooden inner panel, the glass
Steel outer panels and the bonding of wooden inner panel, weight is slim and graceful, and intensity is high.
Preferably, being provided with installing pipe on the reinforcement wooden case, the installing pipe is arranged through upper coverboard and lower coverboard,
The side of the upper coverboard and lower coverboard is at a stalemate flat with installation pipe end, and installing pipe can be used for connecting with fuselage, and upper casing
The side of plate and lower coverboard with installation pipe end is at a stalemate flat wing and globality after fuselage installation can be made more preferable.
Preferably, the bottom surface midpoint of the reinforcement wooden case and the peak of upper coverboard are located at same and lower casing back
On perpendicular straight line, outstanding support force can be played, the peak of coverboard can be prevented to be depressed into deformation, stress performance
It is good.
Preferably, being provided with motor mount on the upper coverboard, the motor mount is integral type with upper coverboard
Setting, the motor mount are detachably connected with lower coverboard, and overall structure is reliable and stable, between the upper coverboard and lower coverboard
It is formed fluted, is provided with aileron in the groove, the aileron is articulated and connected with upper coverboard, has certain turning power, makes
Good, the stable connection with effect.
Beneficial effects of the present invention are：It is formed with cavity between upper coverboard and lower coverboard, and is provided with one in cavity
A rib and reinforcement wooden case replace the structure of traditional multiple ribs, stringer and spar, greatly reduce whole weight, and the wing
Rib and reinforcement wooden case are bonded with carbon cloth so that carbon cloth, rib and reinforcement wooden case form force structure body, and structure is strong
Degree is high, and stress performance is good, in addition, upper casing back is provided with positioning strip and fixing piece, positioning strip is arranged in a rectangular parallelepiped shape, positioning
Mounting groove is formed between item, reinforcement wooden case is inserted in mounting groove, is provided with bar planting on fixing piece, bar planting through upper coverboard and
Lower coverboard setting, bar planting end is arranged in semicircle shape, by being provided with mounting groove, can greatly be carried convenient for users to installation
The high success rate of reinforcement wooden case installation, and by being provided with bar planting on fixing piece, stable structure is reliable, and bar planting can be used
In connection fuselage so that dismount more convenient between fuselage and wing, positioning strip, fixing piece and lower coverboard are viscous with upper coverboard
It closes, stable structure is easy to process, and connection is reliable, and rib and reinforcement wooden case are perpendicular, and stable structure, rib is matched with reinforcement wooden case
The stress performance of wing entirety can be promoted by closing, and carbon cloth is arranged in crosswise, and rib can be facilitated to be installed with reinforcement wooden case,
Material can be effectively saved, reduces cost, and reinforcement can be played the role of again, mounting groove mutually agrees with reinforcement wooden case, can
The case where displacement occur and lead to decrease in yield after preventing reinforcement wooden case to be inserted into mounting groove, upper coverboard and lower coverboard are by glass
Glass steel outer panels and wooden inner panel composition, fiberglass outer panels and the bonding of wooden inner panel, weight is slim and graceful, and intensity is high, reinforcement
Be provided with installing pipe on wooden case, installing pipe is arranged through upper coverboard and lower coverboard, the side of upper coverboard and lower coverboard with installation
Pipe end mutually maintains an equal level, and installing pipe can be used for connecting with fuselage, and the side of upper coverboard and lower coverboard with installation pipe end phase
Maintaining an equal level after wing can be made to be installed with fuselage, globality is more preferable, and the bottom surface midpoint of reinforcement wooden case and the peak of upper coverboard are located at
Same can play outstanding support force, can prevent the peak of coverboard on the perpendicular straight line of lower casing back
It is depressed into deformation, stress performance is good, and motor mount is provided on upper coverboard, and motor mount is set with upper coverboard for integral type
It sets, motor mount is detachably connected with lower coverboard, and overall structure is reliable and stable, is formed between upper coverboard and lower coverboard recessed
Slot is provided with aileron in groove, and aileron is articulated and connected with upper coverboard, has certain turning power, and using effect is good, and connection is steady
It is fixed.
Description of the drawings
To describe the technical solutions in the embodiments of the present invention more clearly, make required in being described below to embodiment
Attached drawing is briefly described, it should be apparent that, drawings in the following description are only some embodiments of the invention, for
For those of ordinary skill in the art, without creative efforts, other are can also be obtained according to these attached drawings
Attached drawing.
Fig. 1 is a kind of overall structure diagram of unmanned plane wing of the present invention；
Fig. 2 is a kind of partial sectional view of unmanned plane wing of the present invention.
Specific implementation mode
Embodiment 1
As shown in Figs. 1-2, a kind of unmanned plane wing, including upper coverboard 1 and lower coverboard 2, the upper coverboard 1 and lower coverboard 2
The back side is both provided with carbon cloth 3, and the upper coverboard 1 and lower coverboard 2 are bonded with carbon cloth 3, the upper coverboard 1 and lower casing
It is formed with cavity between plate 2（It is not shown）, rib 4 and reinforcement wooden case 5 are provided in the cavity, during the reinforcement wooden case 5 is
Sky setting, the rib 4 and reinforcement wooden case 5 are bonded with carbon cloth 3, are formed between upper coverboard 1 and lower coverboard 2 free
Chamber, and there are one the structures that rib 4 and reinforcement wooden case 5 replace traditional multiple ribs, stringer and spar for setting in cavity, greatly
Whole weight is reduced greatly, and rib 4 and reinforcement wooden case 5 are bonded with carbon cloth 3 so that carbon cloth 3, rib 4
Force structure body is formed with reinforcement wooden case 5, structural strength is high, and stress performance is good.
The present embodiment has the beneficial effect that：It is formed with cavity between upper coverboard and lower coverboard, and is provided in cavity
One rib and reinforcement wooden case replace the structure of traditional multiple ribs, stringer and spar, greatly reduce whole weight, and
Rib and reinforcement wooden case are bonded with carbon cloth so that carbon cloth, rib and reinforcement wooden case form force structure body, structure
Intensity is high, and stress performance is good.
Embodiment 2
As shown in Figs. 1-2, a kind of unmanned plane wing, including upper coverboard 1 and lower coverboard 2, the upper coverboard 1 and lower coverboard 2
The back side is both provided with carbon cloth 3, and the upper coverboard 1 and lower coverboard 2 are bonded with carbon cloth 3, the upper coverboard 1 and lower casing
It is formed with cavity between plate 2（It is not shown）, rib 4 and reinforcement wooden case 5 are provided in the cavity, during the reinforcement wooden case 5 is
Sky setting, the rib 4 and reinforcement wooden case 5 are bonded with carbon cloth 3, and 1 back side of upper coverboard is provided with positioning strip 6 and solid
Determine part（It is not shown）, the positioning strip 6 is arranged in a rectangular parallelepiped shape, and mounting groove is formed between the positioning strip 6（It is not shown）, institute
It states reinforcement wooden case 5 to be inserted in mounting groove, bar planting 7 is provided on the fixing piece, the bar planting 7 runs through upper coverboard 1 and lower casing
Plate 2 is arranged, and 7 end of the bar planting is arranged in semicircle shape, can be convenient for users to installation, greatly by being provided with mounting groove
The success rate of the installation of reinforcement wooden case 5 is improved, and by being provided with bar planting 7 on fixing piece, stable structure is reliable, bar planting 7
It can be used for connecting fuselage so that dismount more convenient between fuselage and wing, the positioning strip 6, fixing piece and lower coverboard 2 are equal
It being bonded with upper coverboard 1, stable structure is easy to process, and connection is reliable, and the rib 4 and reinforcement wooden case 5 are perpendicular, stable structure,
Rib 4 and reinforcement wooden case 5 coordinate the stress performance that can promote wing entirety, and the carbon cloth 3, can be in crosswise setting
Facilitate rib 4 to be installed with reinforcement wooden case 5, can effectively save material, reduce cost, and reinforcement can be played the role of again,
The mounting groove agrees with 5 phase of reinforcement wooden case, occurs the case where displacement after reinforcement wooden case 5 can be prevented to be inserted into mounting groove and causes
Decrease in yield, the upper coverboard 1 and lower coverboard 2 are by fiberglass outer panels（It is not shown）It is formed with wooden inner panel（Do not scheme
Show）, the fiberglass outer panels and the bonding of wooden inner panel, weight is slim and graceful, and intensity is high, and peace is provided on the reinforcement wooden case 5
Tubulature 8, the installing pipe 8 are arranged through upper coverboard 1 and lower coverboard 2, the side of the upper coverboard 1 and lower coverboard 2 with installation
8 end of pipe mutually maintains an equal level, and installing pipe 8 can be used for connecting with fuselage, and the side of upper coverboard 1 and lower coverboard 2 is last with installing pipe 8
End mutually maintain an equal level can make the installation of wing and fuselage after globality it is more preferable, the bottom surface midpoint of the reinforcement wooden case 5 and upper coverboard 1
Peak is located at same on the perpendicular straight line in lower 2 back side of coverboard, can play outstanding support force, can prevent upper casing
The peak of plate 1 is depressed into deformation, and stress performance is good, and motor mount is provided on the upper coverboard 1（It is not shown）, the electricity
Machine mounting base is arranged with upper coverboard 1 for integral type, and the motor mount is detachably connected with lower coverboard 2, and overall structure is stablized
Reliably, it is formed between the upper coverboard 1 and lower coverboard 2 fluted（It is not shown）, aileron 9, the pair are provided in the groove
The wing 9 is articulated and connected with upper coverboard 1, has certain turning power, using effect is good, stable connection, in upper coverboard 1 and lower coverboard 2
Between be formed with cavity, and in cavity setting there are one rib 4 and reinforcement wooden case 5 replace traditional multiple ribs, stringer and
The structure of spar greatly reduces whole weight, and rib 4 and reinforcement wooden case 5 are bonded with carbon cloth 3 so that carbon
Fiber cloth 3, rib 4 and reinforcement wooden case 5 form force structure body, and structural strength is high, and stress performance is good.
The present embodiment has the beneficial effect that：It is formed with cavity between upper coverboard and lower coverboard, and is provided in cavity
One rib and reinforcement wooden case replace the structure of traditional multiple ribs, stringer and spar, greatly reduce whole weight, and
Rib and reinforcement wooden case are bonded with carbon cloth so that carbon cloth, rib and reinforcement wooden case form force structure body, structure
Intensity is high, and stress performance is good, and upper casing back is provided with positioning strip and fixing piece, and positioning strip is arranged in a rectangular parallelepiped shape, positioning strip
Between be formed with mounting groove, reinforcement wooden case is inserted in mounting groove, is provided with bar planting on fixing piece, bar planting through upper coverboard and under
Coverboard is arranged, and bar planting end is arranged in semicircle shape, by being provided with mounting groove, can greatly be improved convenient for users to installation
The success rate of reinforcement wooden case installation, and by being provided with bar planting on fixing piece, stable structure is reliable, and bar planting can be used for
Connect fuselage so that dismounted between fuselage and wing it is more convenient, positioning strip, fixing piece and lower coverboard with upper coverboard bond,
Stable structure, easy to process, connection is reliable, and rib and reinforcement wooden case are perpendicular, stable structure, and rib can with the cooperation of reinforcement wooden case
To promote the stress performance of wing entirety, carbon cloth is arranged in crosswise, and rib can be facilitated to be installed with reinforcement wooden case, can be with
Material is effectively saved, reduces cost, and reinforcement can be played the role of again, mounting groove mutually agrees with reinforcement wooden case, can be to prevent
Only there is the case where displacement and leads to decrease in yield after being inserted into mounting groove in reinforcement wooden case, and upper coverboard and lower coverboard are by fiberglass
Outer panels and wooden inner panel composition, fiberglass outer panels and the bonding of wooden inner panel, weight is slim and graceful, and intensity is high, reinforcement wooden case
On be provided with installing pipe, installing pipe is arranged through upper coverboard and lower coverboard, the side of upper coverboard and lower coverboard with installing pipe end
End mutually maintains an equal level, and installing pipe can be used for connecting with fuselage, and the side of upper coverboard and lower coverboard is at a stalemate flat with installation pipe end
Globality is more preferable after wing can be made to be installed with fuselage, and the bottom surface midpoint of reinforcement wooden case and the peak of upper coverboard are positioned at same
Item can play outstanding support force, can prevent the peak of coverboard from being pressed on the perpendicular straight line of lower casing back
To deformation, stress performance is good, and motor mount is provided on upper coverboard, and motor mount is arranged with upper coverboard for integral type, electricity
Machine mounting base is detachably connected with lower coverboard, and overall structure is reliable and stable, and fluted, groove is formed between upper coverboard and lower coverboard
It is inside provided with aileron, aileron is articulated and connected with upper coverboard, has certain turning power, using effect is good, stable connection.
The above description is merely a specific embodiment, but scope of protection of the present invention is not limited thereto, any
The change or replacement expected without creative work, should be covered by the protection scope of the present invention.
Claims (1)
1. a kind of unmanned plane wing, it is characterised in that：Including upper coverboard and lower coverboard, the upper coverboard and lower casing back are all provided with
It is equipped with carbon cloth, the upper coverboard and lower coverboard are bonded with carbon cloth, be formed between the upper coverboard and lower coverboard
Cavity, rib and reinforcement wooden case are provided in the cavity, and the reinforcement wooden case is hollow setting, the rib and reinforcement wooden case
Being bonded with carbon cloth, the upper casing back is provided with positioning strip and fixing piece, and the positioning strip is arranged in a rectangular parallelepiped shape,
Mounting groove is formed between the positioning strip, the reinforcement wooden case is inserted in mounting groove, and bar planting is provided on the fixing piece,
The bar planting is arranged through upper coverboard and lower coverboard, the bar planting end in semicircle shape setting, the positioning strip, fixing piece and under
Coverboard is bonded with upper coverboard, and the rib and reinforcement wooden case are perpendicular, and the carbon cloth is arranged in crosswise, the installation
Slot mutually agrees with reinforcement wooden case, and the upper coverboard and lower coverboard are made of fiberglass outer panels and wooden inner panel, the glass
Glass steel outer panels and the bonding of wooden inner panel, are provided with installing pipe on the reinforcement wooden case, the installing pipe through upper coverboard and
The side of lower coverboard setting, the upper coverboard and lower coverboard is at a stalemate flat with installation pipe end, in the bottom surface of the reinforcement wooden case
The peak of point and upper coverboard is located at same on the perpendicular straight line of lower casing back, and motor is provided on the upper coverboard
Mounting base, the motor mount are arranged with upper coverboard for integral type, and the motor mount is detachably connected with lower coverboard, institute
It states and is formed fluted between coverboard and lower coverboard, be provided with aileron in the groove, the aileron is articulated and connected with upper coverboard.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610709440.3A CN106043666B (en) | 2016-08-24 | 2016-08-24 | A kind of unmanned plane wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610709440.3A CN106043666B (en) | 2016-08-24 | 2016-08-24 | A kind of unmanned plane wing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106043666A CN106043666A (en) | 2016-10-26 |
| CN106043666B true CN106043666B (en) | 2018-10-26 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201610709440.3A Active CN106043666B (en) | 2016-08-24 | 2016-08-24 | A kind of unmanned plane wing |
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Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2019061100A1 (en) * | 2017-09-27 | 2019-04-04 | 深圳市大疆创新科技有限公司 | Wing assembly and unmanned aerial vehicle |
| CN118457967A (en) * | 2018-12-28 | 2024-08-09 | 深圳市道通智能航空技术股份有限公司 | Unmanned vehicles and wing subassembly thereof |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB201005308D0 (en) * | 2010-03-30 | 2010-05-12 | Airbus Operations Ltd | Composite structural member |
| CN103434638A (en) * | 2013-09-16 | 2013-12-11 | 哈尔滨工业大学 | Method for hybrid connection of center sill and reinforcing rib of wing of composite material |
| CN104590544A (en) * | 2015-01-28 | 2015-05-06 | 梧州晟裕科技有限公司 | Aerofoil structure of fixed-wing unmanned aerial vehicle |
| CN205131625U (en) * | 2015-11-10 | 2016-04-06 | 湖南云顶智能科技有限公司 | Small -size portable all -wing aircraft overall arrangement unmanned aerial vehicle |
| CN105398563A (en) * | 2015-11-13 | 2016-03-16 | 中国人民解放军国防科学技术大学 | Wing of membrane structure |
| CN205150216U (en) * | 2015-11-24 | 2016-04-13 | 中国航天时代电子公司 | Unmanned aerial vehicle's foam presss from both sides core wing |
| CN206031754U (en) * | 2016-08-24 | 2017-03-22 | 广州朱雀航空科技有限公司 | Unmanned aerial vehicle wing |
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2016
- 2016-08-24 CN CN201610709440.3A patent/CN106043666B/en active Active
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| Publication number | Publication date |
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| CN106043666A (en) | 2016-10-26 |
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