CN206031754U - Unmanned aerial vehicle wing - Google Patents
Unmanned aerial vehicle wing Download PDFInfo
- Publication number
- CN206031754U CN206031754U CN201620926037.1U CN201620926037U CN206031754U CN 206031754 U CN206031754 U CN 206031754U CN 201620926037 U CN201620926037 U CN 201620926037U CN 206031754 U CN206031754 U CN 206031754U
- Authority
- CN
- China
- Prior art keywords
- coverboard
- wooden case
- unmanned plane
- reinforcement
- reinforcement wooden
- Prior art date
- 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.)
- Withdrawn - After Issue
Links
Landscapes
- Toys (AREA)
Abstract
The utility model discloses an unmanned aerial vehicle wing, including last coverboard and lower coverboard, it all is provided with the carbon cloth to go up coverboard and inferior valve backboard face, it all binds with the carbon cloth with lower coverboard to go up the coverboard, go up the coverboard and be formed with the cavity down between the coverboard, be provided with rib and reinforcement wooden case in the cavity, the reinforcement wooden case is the cavity setting, rib and reinforcement wooden case are all adhere with the carbon cloth, this unmanned aerial vehicle wing light in weight is full of.
Description
Technical field
This utility model is related to a kind of unmanned plane wing.
Background technology
UAV referred to as " unmanned plane ", is manipulated using radio robot and the presetting apparatus provided for oneself
Not manned aircraft.Without driving cabin on machine, but the equipment such as automatic pilot, presetting apparatus are installed.On ground, naval vessels or
Machine tool remote control station personnel by the equipment such as radar, which is tracked, is positioned, remote control, remote measurement and Digital Transmission.Can be in radio
As conventional airplane take off or launched with booster rocket under remote control, also aerial input can be taken to by machine tool and be flown.Reclaim
When, the mode automatic Landing as conventional airplane landing mission is can use, also can be passed through remote control parachute or block is reclaimed.Can
Repetitiousness is using 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 with higher intensity, so often having inside wing substantial amounts of
Rib, causes wing overall weight larger, it is difficult to meet the demand on market.
Utility model content
The technical problems to be solved in the utility model is to provide a kind of slim and graceful unmanned plane wing of weight.
For solving the above problems, this utility model is adopted the following technical scheme that：
A kind of unmanned plane wing, is provided with carbon fibre including upper coverboard and lower coverboard, the upper coverboard and lower casing back
Wei Bu, the upper coverboard and lower coverboard are bonded with carbon cloth, are formed with cavity between the upper coverboard and lower coverboard, described
Rib and reinforcement wooden case is provided with cavity, and the reinforcement wooden case is hollow setting, and the rib and reinforcement wooden case are fine with carbon
Wei Bu is bonded.
Preferably, the upper casing back is provided with positioning strip and fixture, the positioning strip is arranged in rectangular-shape,
Mounting groove is formed between the positioning strip, and the reinforcement wooden case is inserted in mounting groove, is provided with bar planting on the fixture,
The bar planting runs through upper coverboard and lower coverboard and arranges, and the bar planting end is provided by mounting groove in semicircle shape setting, can be with
Convenient use person installs, and greatly improves the success rate of reinforcement wooden case installation, and by being provided with bar planting on fixture,
Stability Analysis of Structures reliability, bar planting can be used for connecting fuselage so that dismount between fuselage and wing convenient.
Preferably, the positioning strip, fixture and lower coverboard are bonded with upper coverboard, Stability Analysis of Structures is easy to process, even
Connect reliability.
Preferably, the rib is perpendicular with reinforcement wooden case, Stability Analysis of Structures, rib are coordinated with reinforcement wooden case and can be lifted
The overall stress performance of wing.
Preferably, the carbon cloth is arranged in crosswise, rib can be facilitated to install with reinforcement wooden case, can be effective
Material-saving, reduces cost, and and reinforcement can be played a part of.
Preferably, the mounting groove is mutually agreed with reinforcement wooden case, occur after reinforcement wooden case insertion mounting groove can be prevented
The situation of displacement and cause decrease in yield.
Preferably, the upper coverboard and lower coverboard are constituted by fiberglass outer panels and wooden wainscot, the glass
Steel outer panels and the bonding of wooden wainscot, weight are slim and graceful, and intensity is high.
Preferably, being provided with installing pipe on the reinforcement wooden case, the installing pipe runs through upper coverboard and lower coverboard is arranged,
The side of the upper coverboard and lower coverboard is at a stalemate with installation pipe end flat, and installing pipe can be used for being connected with fuselage, and upper casing
The side of plate and lower coverboard with install pipe end it is at a stalemate it is flat wing can be caused to install with fuselage after globality it is more preferable.
Preferably, the peak of the bottom surface midpoint of the reinforcement wooden case and upper coverboard is 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
Arrange, the motor mount is detachably connected with lower coverboard, and overall structure is reliable and stable, between the upper coverboard and lower coverboard
Form fluted, in the groove, be provided with aileron, the aileron is articulated and connected with upper coverboard, with certain turning power, is made
Good, the stable connection with effect.
The beneficial effects of the utility model are：It is formed between upper coverboard and lower coverboard in cavity, and cavity and arranges
There are a rib and reinforcement wooden case to replace the structure of traditional multiple ribs, stringer and spar, greatly reduce overall 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, knot
Structure intensity is high, and stress performance is good, additionally, upper casing back is provided with positioning strip and fixture, positioning strip is arranged in rectangular-shape,
Mounting groove being formed between positioning strip, reinforcement wooden case is inserted in mounting groove, being provided with bar planting on fixture, bar planting runs through upper casing
Plate and lower coverboard are arranged, and bar planting end is arranged in semicircle shape, is provided by mounting groove, can be installed with convenient use person, greatly
The success rate that improve the installation of reinforcement wooden case, and by being provided with bar planting on fixture, Stability Analysis of Structures reliability, bar planting can
For connect fuselage so that dismount between fuselage and wing it is convenient, positioning strip, fixture and lower coverboard with upper coverboard
Bonding, Stability Analysis of Structures is easy to process, and connection is reliable, and rib is perpendicular with reinforcement wooden case, Stability Analysis of Structures, rib and reinforcement wooden case
Cooperation can lift the overall stress performance of wing, and carbon cloth is arranged in crosswise, and rib can be facilitated to pacify with reinforcement wooden case
Dress, can effective material-saving, reduces cost, and and reinforcement can be played a part of, mounting groove is mutually agreed with reinforcement wooden case,
There is the situation of displacement and cause decrease in yield after reinforcement wooden case insertion mounting groove can be prevented, upper coverboard and lower coverboard by
Fiberglass outer panels and wooden wainscot composition, fiberglass outer panels and the bonding of wooden wainscot, weight are slim and graceful, and intensity is high, mends
Be provided with installing pipe on strong wooden case, installing pipe runs through upper coverboard and lower coverboard is arranged, the side of upper coverboard and lower coverboard with peace
Tubulature end mutually maintains an equal level, and installing pipe can be used for being connected with fuselage, and the side of upper coverboard and lower coverboard with install pipe end
The globality after wing can be caused to install with fuselage that mutually maintains an equal level is more preferable, the peak position of the bottom surface midpoint of reinforcement wooden case and upper coverboard
On same with the perpendicular straight line of lower casing back, outstanding support force can be played, the highest of coverboard can be prevented
Point is depressed into deformation, and stress performance is good, is provided with motor mount on upper coverboard, and motor mount is set for integral type with upper coverboard
Put, motor mount is detachably connected with lower coverboard, and overall structure is reliable and stable, be formed between upper coverboard and lower coverboard recessed
Groove, is provided with aileron in groove, aileron is articulated and connected with upper coverboard, and with certain turning power, using effect is good, and connection is steady
It is fixed.
Description of the drawings
For the technical scheme being illustrated more clearly that in this utility model embodiment, below will be to needed for embodiment description
Accompanying drawing to be used is briefly described, it should be apparent that, drawings in the following description are only some realities of the present utility model
Example is applied, for those of ordinary skill in the art, on the premise of not paying creative work, can be with according to these accompanying drawings
Obtain other accompanying drawings.
Fig. 1 is a kind of overall structure diagram of unmanned plane wing of this utility model；
Fig. 2 is a kind of partial sectional view of unmanned plane wing of this utility model.
Specific embodiment
Embodiment 1
As shown in Figure 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 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
Cavity is formed between plate 2（It is not shown）, rib 4 and reinforcement wooden case 5 is provided with the cavity, during the reinforcement wooden case 5 is
Empty setting, the rib 4 and reinforcement wooden case 5 are bonded with carbon cloth 3, form free between upper coverboard 1 and lower coverboard 2
The structure that a rib 4 and reinforcement wooden case 5 replace traditional multiple ribs, stringer and spar is provided with chamber, and cavity, greatly
Overall 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, and cavity between upper coverboard and lower coverboard and is provided with
One rib and reinforcement wooden case replace the structure of traditional multiple ribs, stringer and spar, greatly reduce overall 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 Figure 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 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
Cavity is formed between plate 2（It is not shown）, rib 4 and reinforcement wooden case 5 is provided with the cavity, during the reinforcement wooden case 5 is
Empty 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 consolidates
Determine part（It is not shown）, the positioning strip 6 in rectangular-shape arrange, be formed with mounting groove between the positioning strip 6（It is not shown）, institute
State reinforcement wooden case 5 to be inserted in mounting groove, on the fixture, be provided with bar planting 7, 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, is provided by mounting groove, can be installed with convenient use person, greatly
The success rate of the installation of reinforcement wooden case 5 is improve, and by being provided with bar planting 7, Stability Analysis of Structures reliability, bar planting 7 on fixture
Can be used for connect fuselage so that dismount between fuselage and wing it is convenient, the positioning strip 6, fixture and lower coverboard 2 it is equal
Bond with upper coverboard 1, Stability Analysis of Structures is easy to process, connection is reliable, the rib 4 is perpendicular with reinforcement wooden case 5, Stability Analysis of Structures,
Rib 4 is coordinated with reinforcement wooden case 5 and can lift the overall stress performance of wing, and the carbon cloth 3, can be with crosswise setting
Facilitate rib 4 to install with reinforcement wooden case 5, can effective material-saving, reduces cost, and and can play a part of reinforcement,
The mounting groove is mutually agreed with reinforcement wooden case 5, the situation of displacement is occurred and is caused after can preventing the insertion mounting groove of reinforcement wooden case 5
Decrease in yield, the upper coverboard 1 and lower coverboard 2 are by fiberglass outer panels（It is not shown）Constitute with wooden wainscot（Do not scheme
Show）, the fiberglass outer panels and the bonding of wooden wainscot, weight be slim and graceful, and intensity is high, is provided with peace on the reinforcement wooden case 5
Tubulature 8, the installing pipe 8 run through upper coverboard 1 and lower coverboard 2 and arrange, 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 being connected 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 cause the installation of wing and fuselage after globality more preferably, the bottom surface midpoint of the reinforcement wooden case 5 and upper coverboard 1
Peak is located on the same straight line perpendicular with lower 2 back side of coverboard, can be played outstanding support force, can be prevented upper casing
The peak of plate 1 is depressed into deformation, and stress performance is good, is provided with motor mount on the upper coverboard 1（It is not shown）, the electricity
Machine mounting seat is arranged for integral type with upper coverboard 1, and the motor mount is detachably connected with lower coverboard 2, and overall structure is stable
It is reliable, form fluted between the upper coverboard 1 and lower coverboard 2（It is not shown）, in the groove, it is provided with aileron 9, the pair
The wing 9 is articulated and connected with upper coverboard 1, and with certain turning power, using effect is good, stable connection, in upper coverboard 1 and lower coverboard 2
Between be formed with cavity, and cavity be provided with a rib 4 and reinforcement wooden case 5 replace traditional multiple ribs, stringer and
The structure of spar, greatly reduces overall 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, and cavity between upper coverboard and lower coverboard and is provided with
One rib and reinforcement wooden case replace the structure of traditional multiple ribs, stringer and spar, greatly reduce overall 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 fixture, and positioning strip is arranged in rectangular-shape, positioning strip
Between be formed with mounting groove, reinforcement wooden case is inserted in mounting groove, is provided with bar planting on fixture, bar planting through upper coverboard and under
Coverboard is arranged, and bar planting end is arranged in semicircle shape, is provided by mounting groove, can be installed with convenient use person, is greatly improved
The success rate that reinforcement wooden case is installed, and by being provided with bar planting on fixture, Stability Analysis of Structures reliability, bar planting can be used for
Connection fuselage so that dismount between fuselage and wing it is convenient, positioning strip, fixture and lower coverboard with upper coverboard bond,
Stability Analysis of Structures, easy to process, connection is reliable, and rib is perpendicular with reinforcement wooden case, Stability Analysis of Structures, and rib is coordinated with reinforcement wooden case can
The stress performance overall to lift wing, carbon cloth are arranged in crosswise, can facilitate rib and the installation of reinforcement wooden case, can be with
Effective material-saving, reduces cost, and and reinforcement can be played a part of, mounting groove is mutually agreed with reinforcement wooden case, can in case
Only there is the situation of displacement and cause decrease in yield after reinforcement wooden case insertion mounting groove, upper coverboard and lower coverboard are by fiberglass
Outer panels and wooden wainscot composition, fiberglass outer panels and the bonding of wooden wainscot, weight are slim and graceful, and intensity is high, reinforcement wooden case
On be provided with installing pipe, installing pipe runs through upper coverboard and lower coverboard is arranged, 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 being connected with fuselage, and the side of upper coverboard and lower coverboard is at a stalemate with installation pipe end flat
After wing can be caused to install with fuselage, more preferably, the peak of the bottom surface midpoint of reinforcement wooden case and upper coverboard is positioned at same for globality
On bar and the perpendicular straight line of lower casing back, outstanding support force can be played, can prevent the peak of coverboard from being pressed
To deforming, stress performance is good, is provided with motor mount on upper coverboard, and motor mount is arranged for integral type with upper coverboard, electricity
Machine mounting seat is detachably connected with lower coverboard, and overall structure is reliable and stable, forms fluted, groove between upper coverboard and lower coverboard
Aileron is provided with inside, aileron is articulated and connected with upper coverboard, with certain turning power, using effect is good, stable connection.
The above, specific embodiment only of the present utility model, but protection domain of the present utility model do not limit to
In this, any change or replacement expected without creative work should all be covered within protection domain of the present utility model.
Claims (10)
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
Carbon cloth is equipped with, the upper coverboard and lower coverboard are bonded with carbon cloth, be formed between the upper coverboard and lower coverboard
Cavity, is provided with rib and reinforcement wooden case in the cavity, the reinforcement wooden case is hollow setting, the rib and reinforcement wooden case
Bond with carbon cloth.
2. unmanned plane wing according to claim 1, it is characterised in that：The upper casing back is provided with positioning strip and consolidates
Determine part, the positioning strip is arranged in rectangular-shape, is formed with mounting groove between the positioning strip, and the reinforcement wooden case is inserted in peace
In tankage, bar planting on the fixture, is provided with, the bar planting runs through upper coverboard and lower coverboard is arranged, and the bar planting end is in partly
Round shape is arranged.
3. unmanned plane wing according to claim 2, it is characterised in that：The positioning strip, fixture and lower coverboard with
Upper coverboard bonding.
4. unmanned plane wing according to claim 3, it is characterised in that：The rib is perpendicular with reinforcement wooden case.
5. unmanned plane wing according to claim 4, it is characterised in that：The carbon cloth is arranged in crosswise.
6. unmanned plane wing according to claim 5, it is characterised in that：The mounting groove is mutually agreed with reinforcement wooden case.
7. unmanned plane wing according to claim 6, it is characterised in that：The upper coverboard and lower coverboard by fiberglass outside
Panel and wooden wainscot composition, the fiberglass outer panels and the bonding of wooden wainscot.
8. unmanned plane wing according to claim 7, it is characterised in that：Installing pipe is provided with the reinforcement wooden case, institute
State installing pipe to arrange through upper coverboard and lower coverboard, the side of the upper coverboard and lower coverboard is at a stalemate with installation pipe end flat.
9. unmanned plane wing according to claim 8, it is characterised in that：The bottom surface midpoint of the reinforcement wooden case and upper coverboard
Peak be located on same and the perpendicular straight line of lower casing back.
10. unmanned plane wing according to claim 9, it is characterised in that：Motor mount is provided with the upper coverboard,
The motor mount is arranged for integral type with upper coverboard, and the motor mount is detachably connected with lower coverboard, the upper casing
Form fluted between plate and lower coverboard, in the groove, be provided with aileron, the aileron is articulated and connected with upper coverboard.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620926037.1U CN206031754U (en) | 2016-08-24 | 2016-08-24 | Unmanned aerial vehicle wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620926037.1U CN206031754U (en) | 2016-08-24 | 2016-08-24 | Unmanned aerial vehicle wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206031754U true CN206031754U (en) | 2017-03-22 |
Family
ID=58302854
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620926037.1U Withdrawn - After Issue CN206031754U (en) | 2016-08-24 | 2016-08-24 | Unmanned aerial vehicle wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206031754U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106043666A (en) * | 2016-08-24 | 2016-10-26 | 广州朱雀航空科技有限公司 | Wing of unmanned plane |
-
2016
- 2016-08-24 CN CN201620926037.1U patent/CN206031754U/en not_active Withdrawn - After Issue
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106043666A (en) * | 2016-08-24 | 2016-10-26 | 广州朱雀航空科技有限公司 | Wing of unmanned plane |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN207346075U (en) | A kind of outer wing structure of fixed-wing unmanned plane | |
| CN206031754U (en) | Unmanned aerial vehicle wing | |
| CN202429344U (en) | Unmanned aerial vehicle | |
| CN106043666B (en) | A kind of unmanned plane wing | |
| CN107826264B (en) | A kind of vehicle-mounted unmanned aerial vehicle landing control system and its control method | |
| CN108016602B (en) | Honeycomb wing and aircraft | |
| CN206031796U (en) | Unmanned aerial vehicle's parachute structure | |
| CN205216194U (en) | But fixed -wing aircraft of VTOL | |
| CN205406707U (en) | Aircraft antenna setting support and quick -witted connection structure who carries on back | |
| CN209956208U (en) | A connection structure that is used for between unmanned aerial vehicle main wing and outer wing | |
| CN203666969U (en) | Bonded aerofoil architecture | |
| CN102849218A (en) | Mounting beam for auxiliary power unit of aircraft | |
| CN206031763U (en) | Unmanned aerial vehicle plug -in type undercarriage | |
| CN106081125A (en) | A kind of parachute construction of unmanned plane | |
| CN210882584U (en) | Survey and drawing unmanned vehicles wing leading edge protection architecture | |
| CN206031775U (en) | A unmanned aerial vehicle for transportation | |
| CN209535437U (en) | A kind of aircraft frame and its aircraft | |
| CN206031759U (en) | Unmanned aerial vehicle vertical tail | |
| CN211435086U (en) | Novel power model airplane | |
| CN207292369U (en) | A kind of aircraft conversion deckle board | |
| CN109733590A (en) | A kind of connection structure between unmanned plane main wing and outer wing | |
| CN206050071U (en) | It is a kind of to lift easily unmanned plane | |
| CN207843310U (en) | A kind of more rotor airframe structures of full carbon fiber riveting | |
| CN207242025U (en) | A kind of laterally folded quadrotor unmanned aerial vehicle body | |
| CN213109761U (en) | Composite material fuselage skin and skeleton connecting structure |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20170322 Effective date of abandoning: 20181026 |
|
| AV01 | Patent right actively abandoned |