CN206528611U - A kind of wing structure of lightweight unmanned plane - Google Patents
A kind of wing structure of lightweight unmanned plane Download PDFInfo
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- CN206528611U CN206528611U CN201720021885.2U CN201720021885U CN206528611U CN 206528611 U CN206528611 U CN 206528611U CN 201720021885 U CN201720021885 U CN 201720021885U CN 206528611 U CN206528611 U CN 206528611U
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- wing
- centre section
- shell body
- fuselage
- horizontal tail
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Abstract
A kind of wing structure of lightweight unmanned plane of the utility model, the unmanned target drone includes fuselage(1), flat wing component(4), horizontal stabilizer assemblies(5)With vertical end component(6), the fuselage(1)For hollow structure inside, and fuselage(1)Shell body be made up of cellular board, the fuselage(1)Inner hollow cavity in polylith dividing plate is installed(2), so that by fuselage(1)Internal cavity is separated into multiple separate installation cavitys.A kind of wing structure of lightweight unmanned plane of the utility model, light weight, cost are low and flight maneuver is flexible.
Description
Technical field
The utility model is related to a kind of wing structure, more particularly, to a kind of wing structure applied on unmanned plane, category
In unmanned air vehicle technique field.
Background technology
At present, as microelectric technique, computer, communication remote sensing technology are continued to develop, unmanned plane is on military, civilian
It is obtained for extensive development;Unmanned plane has the advantages that quick maneuverability, reaction, unmanned flight, operation require low, can be wide
It is general to be applied to the fields such as agricultural, exploration, photography, border patrol, military surveillance, military attack;Simultaneously as unmanned plane is minimized
The requirement of development, its volume constantly reduces, and space in the still substantial amounts of machine of all kinds of remote controls, control, power-equipment, therefore fuel tank
Capacity constantly reduces, but is in order at continuation of the journey and requires, no matter military or civilian be both needed to require that unmanned plane has certain stagnant space-time
Between, therefore unmanned plane lightness becomes one and needs the problem captured badly;Meanwhile, unmanned plane perform each generic task when, it is necessary to
It has certain steering flexibility, and conventional unmanned plane governor motion not enough facilitates, so as to influence it to use scope.
The content of the invention
The purpose of this utility model is to overcome above-mentioned deficiency there is provided a kind of light weight, cost is low and flight maneuver is flexible
Lightweight unmanned plane wing structure.
What the purpose of this utility model was realized in:
A kind of wing structure of lightweight unmanned plane, the unmanned target drone includes fuselage, flat wing component, horizontal stabilizer assemblies and hung down
Straight tail component, the fuselage is hollow structure inside, and the shell body of fuselage is made up of cellular board, the inner hollow of the fuselage
Cavity in polylith dividing plate is installed, so that the cavity of fuselage interior is separated into multiple separate installation cavitys;
The flat wing component includes wing centre section, outer wing and wing tip, and the wing centre section includes the wing centre section upper plate by arcuate structure
Part and wing centre section lower plate bond and are provided with an anti-sump, and structure on the shell body for the hollow structure that pairing is constituted, wing centre section lower plate
Into shell body wing upper plate and wing centre section lower plate outer surface on staggeredly be pasted with a plurality of reinforcement, the reinforcement pacify
Equipped with wing centre section connector, connecting bolt, which is passed through, realizes wing centre section and fuselage in the pre-buried screw after wing centre section connector with screw-on machine
Connection, the shell body left and right sides is provided with connection strap, and the bottom of the shell body, which caves inward, to be formed with two and symmetrically set
An aileron is placed with the groove put, each groove, the aileron includes the aileron hollow body being made up of cellular board, institute
The top for stating aileron hollow body is provided with the wooden connection strap of aileron, and the two ends of the wooden connection strap of the aileron are separately installed with wing centre section
Rotary shaft and wing centre section power transmission shaft, the wing centre section rotary shaft activity are plugged on the cell wall of groove, and the wing centre section power transmission shaft passes through recessed
The cell wall of groove is inserted in anti-sump, and wing centre section power transmission shaft is fixedly connected with a driving lever on one end in anti-sump;
The outer wing includes outer wing body and is connected to the outer wing connection strap of outer wing body both sides, the outer wing body
For the hollow structure being made up of cellular board, and the outer wing connection strap is connected by bolt with the connection strap on wing centre section;It is described
The end of outer wing is installed by the wing tip by there is glass fiber material to be made;
The horizontal stabilizer assemblies include the horizontal tail shell body of hollow structure, and the horizontal tail shell body is provided at both ends with by glass
Be provided with installation storehouse on the outer apex of the wing of horizontal tail that fiber material is made, the lower surface of the horizontal tail shell body, the horizontal tail shell body by
Cellular board is made, and is staggeredly equipped with a plurality of horizontal tail reinforcement on two surfaces up and down of horizontal tail shell body, and the horizontal tail adds
Horizontal tail connector is installed, bolt passes through in the pre-buried screw after horizontal tail connector with screw-on machine and realizes horizontal tail shell in strengthening tendons
The connection of body and fuselage, the bottom of the horizontal tail shell body, which caves inward, is formed with two symmetrically arranged grooves, each groove
An elevator is inside placed with, the elevator includes in the elevator hollow body being made up of cellular board, the elevator
The top of empty body is provided with the wooden connection strap of elevator, and the two ends of the wooden connection strap of elevator are separately installed with elevator
Rotary shaft and elevator power transmission shaft, the elevator rotary shaft activity are plugged on the cell wall of horizontal tail shell body groove, and two rise
The elevator power transmission shaft of drop rudder passes through the end in insertion installation storehouse after cell wall to be connected by synchronous connecting shaft;
The vertical end component includes the vertical end housing being fixedly installed on fuselage, and the vertical end housing is by honeybee
The vertical end wing tip being made up of glass material is installed at the top of the hollow structure that nest plate is constituted, the vertical end housing, it is described
Two side external surfaces of vertical end wing tip are provided with vertical end reinforcement.
Assigned on a kind of wing structure of lightweight unmanned plane of the utility model, the vertical end housing static pressure liquid level meter and
Inlet connector, the static pressure liquid level meter and inlet connector are communicated to by the oil pipe in vertical end housing respectively to be located at
In fuel tank in fuselage.
Compared with prior art, the beneficial effects of the utility model are:
Wing structure of the present utility model(Flat wing component, horizontal stabilizer assemblies and vertical end component)Agent structure all use honeybee
Nest plate is made, and improves intensity with reinforcement in outer surface, meanwhile, flat wing component can easily realize steering by aileron regulation
Flight, and horizontal stabilizer assemblies realize takeoff and landing by the elevator of collaborative work;In addition, when in use, in hollow fuselage
Portion is separated out different chambers by dividing plate to be used to install all kinds of control elements and flight device, is easy to the later stage to change, safeguard.
Brief description of the drawings
Fig. 1 is a kind of side structure schematic view of lightweight unmanned plane of the utility model.
Fig. 2 is a kind of positive structure diagram of lightweight unmanned plane of the utility model.
Fig. 3 is a kind of sectional view of the airframe structure of lightweight unmanned plane of the utility model.
Fig. 4 is a kind of structural representation of the Al-alloy parts of lightweight unmanned plane of the utility model.
Fig. 5 is a kind of structural representation of the flat wing of the wing structure of lightweight unmanned plane of the utility model.
Fig. 6 is a kind of structural representation of the wing centre section of the wing structure of lightweight unmanned plane of the utility model.
Fig. 7 is a kind of side view of the wing centre section of the wing structure of lightweight unmanned plane of the utility model.
Fig. 8 is a kind of side view of the upper plate of the wing centre section of the wing structure of lightweight unmanned plane of the utility model.
Fig. 9 is a kind of side view of the lower plate of the wing centre section of the wing structure of lightweight unmanned plane of the utility model.
Figure 10 is a kind of partial sectional view of the aileron of the wing structure of lightweight unmanned plane of the utility model.
Figure 11 is a kind of structural representation of the outer wing of the wing structure of lightweight unmanned plane of the utility model.
Figure 12 is a kind of structural representation of the horizontal stabilizer assemblies of the wing structure of lightweight unmanned plane of the utility model.
Figure 13 is a kind of side view of the horizontal stabilizer assemblies of the wing structure of lightweight unmanned plane of the utility model.
Figure 14 is a kind of partial sectional view of the elevator of the wing structure of lightweight unmanned plane of the utility model.
Figure 15 is a kind of connection driving structure schematic diagram of the elevator of the wing structure of lightweight unmanned plane of the utility model.
Figure 16 is a kind of structural representation of the vertical end of the wing structure of lightweight unmanned plane of the utility model.
Wherein:
Fuselage 1, dividing plate 2, Al-alloy parts 3, flat wing component 4, horizontal stabilizer assemblies 5, vertical end component 6;
Damper 1.1;
Lightening hole 3.1;
Wing centre section 4.1, outer wing 4.2, wing tip 4.3;
Wing centre section upper plate 4.1.1, wing centre section lower plate 4.1.2, anti-sump 4.1.3, reinforcement 4.1.4, wing centre section connector
4.1.5, connection strap 4.1.6, aileron 4.1.7, wing centre section rotary shaft 4.1.8, wing centre section power transmission shaft 4.1.9, driving lever 4.1.10;
The wooden connection strap 4.1.7.2 of aileron hollow body 4.1.7.1, aileron;
Outer wing body 4.2.1, outer wing connection strap 4.2.2;
The outer apex of the wing 5.3 of horizontal tail shell body 5.1, horizontal tail reinforcement 5.2, horizontal tail, horizontal tail connector 5.4, elevator 5.5, liter
Rudder rotary shaft 5.6, elevator power transmission shaft 5.7, synchronous connecting shaft 5.8 drop;
Storehouse 5.1.1 is installed;
The wooden connection strap 5.5.2 of elevator hollow body 5.5.1, elevator;
Vertical end housing 6.1, vertical end wing tip 6.2, vertical end reinforcement 6.3, static pressure liquid level meter 6.4, inlet connector
6.5。
Embodiment
Referring to Fig. 1 ~ 16, a kind of wing structure for lightweight unmanned plane that the utility model is related to, the wing structure is included
There are flat wing component 4, horizontal stabilizer assemblies 5 and the vertical end component 6 being installed on fuselage 1, the bottom of fuselage 1 is provided with damper
1.1, the fuselage 1 is hollow structure inside(Concretely, the fuselage 1 is bonded by two housing sections pairing up and down
Hollow structure), and the shell body of fuselage 1 is made of cellular board(So as to serve loss of weight effect), in the inside of the fuselage 1
Polylith dividing plate 2 is installed in empty cavity, so that the cavity inside fuselage 1 is separated into multiple separate installation cavitys,
The automatically controlled component different for installing;
The Al-alloy parts 3 of one cyclic structure are installed on the head end plane of the fuselage 1, set on the Al-alloy parts 3
It is equipped with multiple lightening holes 3.1;The middle part of the fuselage 1 is provided with flat wing component 4, the tail of the fuselage 1 and is provided with horizontal tail
Component 5 and vertical end component 6;
The flat wing component 4 includes wing centre section 4.1, outer wing 4.2 and wing tip 4.3, and the wing centre section 4.1 includes by arc knot
The wing centre section upper plate 4.1.1 and wing centre section lower plate 4.1.2 of structure bond the shell body for the hollow structure that pairing is constituted, wing centre section lower plate
One anti-sump 4.1.3 is installed on 4.1.2, and constitutes the wing upper plate 4.1.1 and wing centre section lower plate 4.1.2 of shell body appearance
Staggeredly it is pasted with face on a plurality of reinforcement 4.1.4, the reinforcement 4.1.4 and wing centre section connector 4.1.5 is installed, connects spiral shell
Bolt passes through the connection for being screwed in after wing centre section connector 4.1.5 and wing centre section 4.1 and fuselage 1 being realized in the pre-buried screw on fuselage 1, described outer
The housing left and right sides is provided with connection strap 4.1.6, the bottom of the shell body cave inward be formed with two it is symmetrically arranged recessed
Aileron a 4.1.7, the aileron 4.1.7 is placed with groove, each groove and includes hollow of aileron being made up of cellular board
Body 4.1.7.1, the aileron hollow body 4.1.7.1 top are provided with the wooden connection strap 4.1.7.2 of aileron, and the aileron is wooden
Connection strap 4.1.7.2 two ends are separately installed with wing centre section rotary shaft 4.1.8 and wing centre section power transmission shaft 4.1.9, the wing centre section rotary shaft
4.1.8 activity is plugged on the cell wall of groove, and the cell wall of the wing centre section power transmission shaft 4.1.9 through groove is inserted in anti-sump
4.1.3 it is interior, and wing centre section power transmission shaft 4.1.9 is fixedly connected with a driving lever 4.1.10 on one end in anti-sump 4.1.3;Pass through
Driving lever 4.1.10 driving ailerons 4.1.7 is rotated, so as to realize the control turned to aircraft;Concretely, in use, peace can be passed through
Wing centre section power transmission shaft 4.1.9 rotations are driven loaded on the electric pushrod driving driving lever 4.1.10 in anti-sump 4.1.3;
The outer wing 4.2 includes outer wing body 4.2.1 and is connected to the outer wing connection strap of outer wing body 4.2.1 both sides
4.2.2, the outer wing body 4.2.1 is the hollow structure being made up of cellular board, and the outer wing connection strap 4.2.2 passes through bolt
It is connected with the connection strap 4.1.6 on wing centre section 4.1;The end of the outer wing 4.2 is installed by the wing tip by there is glass fiber material to be made
4.3;
The horizontal stabilizer assemblies 5 include the horizontal tail shell body 5.1 of hollow structure, and the two ends of the horizontal tail shell body 5.1 are set
It is equipped with the apex of the wing 5.3 outside the horizontal tail being made up of glass fiber material, the lower surface of the horizontal tail shell body 5.1 and is provided with installation storehouse
5.1.1, the horizontal tail shell body 5.1 is made up of cellular board, and is staggered on two surfaces up and down of horizontal tail shell body 5.1
Have and horizontal tail connector 5.4 is installed on a plurality of horizontal tail reinforcement 5.2, the horizontal tail reinforcement 5.2, bolt passes through horizontal tail connector
The connection that horizontal tail shell body 5.1 and fuselage 1 are realized in the pre-buried screw on fuselage 1, the horizontal tail shell body 5.1 are screwed in after 5.4
Bottom cave inward to be formed with two symmetrically arranged grooves, each groove and be placed with an elevator 5.5, the lifting
Rudder 5.5 includes the elevator hollow body 5.5.1, the elevator hollow body 5.5.1 that are made up of cellular board top peace
Equipped with the wooden connection strap 5.5.2 of elevator, the two ends of the wooden connection strap 5.5.2 of elevator are separately installed with elevator rotation
Axle 5.6 and elevator power transmission shaft 5.7, the activity of elevator rotary shaft 5.6 are plugged in the cell wall of the groove of horizontal tail shell body 5.1
On, the elevator power transmission shaft 5.7 of two elevators 5.5 passes through the end of insertion installation storehouse 5.1.1 after cell wall to pass through synchronized links
Axle 5.8 is connected;
The vertical end component 6 includes the vertical end housing 6.1 being fixedly installed on fuselage 1, the vertical end housing
6.1 be the hollow structure that is made up of cellular board, the top of the vertical end housing 6.1 be provided with by glass material be made it is vertical
Empennage point 6.2, two side external surfaces of the vertical end wing tip 6.2 are provided with vertical end reinforcement 6.3, the vertical end housing
Static pressure liquid level meter 6.4 and inlet connector 6.5 are assigned on 6.1, the static pressure liquid level meter 6.4 and inlet connector 6.5 are distinguished
It is communicated to by the oil pipe in vertical end housing 6.1 in the fuel tank in fuselage 1;For measuring the fluid amount in fuel tank
And fluid is filled in good time.
In addition:It should be noted that above-mentioned embodiment is only a prioritization scheme of this patent, the skill of this area
Any change or improvement that art personnel are done according to above-mentioned design, within the protection domain of this patent.
Claims (2)
1. a kind of wing structure of lightweight unmanned plane, the wing structure, which includes, is installed on fuselage(1)On flat wing component
(4), horizontal stabilizer assemblies(5)With vertical end component(6), it is characterised in that:
The flat wing component(4)Include wing centre section(4.1), outer wing(4.2)And wing tip(4.3), the wing centre section(4.1)Include by
The wing centre section upper plate of arcuate structure(4.1.1)With wing centre section lower plate(4.1.2)The shell body for the hollow structure that pairing is constituted is bonded,
Wing centre section lower plate(4.1.2)On an anti-sump is installed(4.1.3), and constitute the wing upper plate of shell body(4.1.1)And wing centre section
Lower plate(4.1.2)Outer surface on staggeredly be pasted with a plurality of reinforcement(4.1.4), the reinforcement(4.1.4)It is upper to install
There is wing centre section connector(4.1.5), connecting bolt pass through wing centre section connector(4.1.5)After screw in fuselage(1)On pre-buried screw in
Realize wing centre section(4.1)With fuselage(1)Connection, the shell body left and right sides is provided with connection strap(4.1.6), the shell body
Bottom cave inward to be formed with two symmetrically arranged grooves, each groove and be placed with an aileron(4.1.7), the pair
The wing(4.1.7)Include the aileron hollow body being made up of cellular board(4.1.7.1), the aileron hollow body(4.1.7.1)
Top the wooden connection strap of aileron is installed(4.1.7.2), the wooden connection strap of the aileron(4.1.7.2)Two ends be separately installed with
Wing centre section rotary shaft(4.1.8)With wing centre section power transmission shaft(4.1.9), the wing centre section rotary shaft(4.1.8)Activity is plugged in the groove of groove
On wall, the wing centre section power transmission shaft(4.1.9)Cell wall through groove is inserted in anti-sump(4.1.3)It is interior, and wing centre section power transmission shaft
(4.1.9)Positioned at anti-sump(4.1.3)A driving lever is fixedly connected with interior one end(4.1.10);
The outer wing(4.2)Include outer wing body(4.2.1)And it is connected to outer wing body(4.2.1)The outer wing connection of both sides
Bar(4.2.2), the outer wing body(4.2.1)For the hollow structure being made up of cellular board, and the outer wing connection strap(4.2.2)
Pass through bolt and wing centre section(4.1)On connection strap(4.1.6)It is connected;The outer wing(4.2)End install by there is glass material
Expect the wing tip being made(4.3);
The horizontal stabilizer assemblies(5)Include the horizontal tail shell body of hollow structure(5.1), the horizontal tail shell body(5.1)Two ends
It is provided with the apex of the wing outside the horizontal tail being made up of glass fiber material(5.3), the horizontal tail shell body(5.1)Lower surface on be provided with installation
Storehouse(5.1.1), the horizontal tail shell body(5.1)It is made up of cellular board, and horizontal tail shell body(5.1)Two surfaces up and down on
It is staggeredly equipped with a plurality of horizontal tail reinforcement(5.2), the horizontal tail reinforcement(5.2)On horizontal tail connector is installed(5.4), bolt
Through horizontal tail connector(5.4)After screw in fuselage(1)On pre-buried screw in realize horizontal tail shell body(5.1)With fuselage(1)'s
Connection, the horizontal tail shell body(5.1)Bottom cave inward to be formed with two symmetrically arranged grooves, each groove and put
It is equipped with an elevator(5.5), the elevator(5.5)Include the elevator hollow body being made up of cellular board(5.5.1), institute
State elevator hollow body(5.5.1)Top the wooden connection strap of elevator is installed(5.5.2), the wooden connection of the elevator
Bar(5.5.2)Two ends be separately installed with elevator rotary shaft(5.6)With elevator power transmission shaft(5.7), the elevator rotation
Axle(5.6)Activity is plugged in horizontal tail shell body(5.1)On the cell wall of groove, two elevators(5.5)Elevator power transmission shaft
(5.7)Storehouse is installed in insertion after through cell wall(5.1.1)End pass through synchronous connecting shaft(5.8)It is connected;
The vertical end component(6)Include and be fixedly installed in fuselage(1)On vertical end housing(6.1), the vertical end shell
Body(6.1)For the hollow structure being made up of cellular board, the vertical end housing(6.1)Top be provided with and be made up of glass material
Vertical end wing tip(6.2), the vertical end wing tip(6.2)Two side external surfaces be provided with vertical end reinforcement(6.3).
2. a kind of wing structure of lightweight unmanned plane as claimed in claim 1, it is characterised in that:The vertical end housing(6.1)
On assigned static pressure liquid level meter(6.4)And inlet connector(6.5), the static pressure liquid level meter(6.4)And inlet connector(6.5)
Respectively by positioned at vertical end housing(6.1)Interior oil pipe is communicated to positioned at fuselage(1)In interior fuel tank.
Priority Applications (1)
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CN201720021885.2U CN206528611U (en) | 2017-01-10 | 2017-01-10 | A kind of wing structure of lightweight unmanned plane |
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CN201720021885.2U CN206528611U (en) | 2017-01-10 | 2017-01-10 | A kind of wing structure of lightweight unmanned plane |
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CN206528611U true CN206528611U (en) | 2017-09-29 |
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CN201720021885.2U Active CN206528611U (en) | 2017-01-10 | 2017-01-10 | A kind of wing structure of lightweight unmanned plane |
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2017
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