CN208947583U - Wing, empennage and aircraft - Google Patents
Wing, empennage and aircraft Download PDFInfo
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- CN208947583U CN208947583U CN201820754524.3U CN201820754524U CN208947583U CN 208947583 U CN208947583 U CN 208947583U CN 201820754524 U CN201820754524 U CN 201820754524U CN 208947583 U CN208947583 U CN 208947583U
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- wing
- snap ring
- main operation
- empennage
- aerofoil
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Abstract
The utility model relates to a kind of wings, including wing-body and the main operation rudder face being arranged on wing-body and/or main operation mechanism, fixed holder assembly is arranged in the wing-body side, bearing assembly is set in the main operation rudder face and/or main operation mechanism, the main operation rudder face and/or main operation mechanism and wing-body are detachably connected by the bearing assembly and fixed holder assembly, and the main operation rudder face and/or main operation mechanism can be rotated relative to the wing-body.In addition, the utility model additionally provides a kind of empennage and aircraft, the wing, empennage and aircraft of the utility model, assembly is easy, facilitates maintenance maintenance, advantageously reduce maintenance cost.
Description
Technical field
The utility model relates to aircraft fields, and in particular to a kind of fast assembling-disassembling, the wing for facilitating maintenance, empennage and fly
Row device.
Background technique
In recent years, aircraft (such as fixed-wing unmanned plane) has had a wide range of applications in every field.However, due to
In the use process of aircraft, aircraft component (such as wing, elevator, rudder) is easily damaged, and needs to repair and more
It changes, then current component assembling manufactures difficult, and maintenance is inconvenient, and maintenance cost is high, limits the use of aircraft.
Utility model content
For the deficiencies in the prior art, this application provides a kind of wing, empennage and aircraft, and there is assembly to hold
Easily, facilitate maintenance maintenance, and the advantage that maintenance cost is low.
One aspect according to the present utility model provides a kind of wing, including wing-body and setting in wing-body
On main operation rudder face and/or main operation mechanism, the wing-body side fixed holder assembly, the main operation rudder face are set
And/or bearing assembly is set in main operation mechanism, the main operation rudder face and/or main operation mechanism and wing-body pass through described
Bearing assembly and fixed holder assembly are detachably connected, and the main operation rudder face and/or main operation mechanism can be relative to described
Wing-body rotation.
A preferred embodiment according to the present utility model, the main operation mechanism are wing flap, and the wing flap includes the
One aerofoil, the second aerofoil and side rib, first aerofoil and the second aerofoil are coated on the outside of the side rib.
A preferred embodiment according to the present utility model, the bearing assembly include bearing and bearing block, the axis
It holds and is mounted on the bearing block, the bearing block is fixedly mounted on the side rib along wing flap extension direction.
A preferred embodiment according to the present utility model, the wing further includes shaft, and the shaft is threaded through institute
It states on the rib of side, the bearing block is arranged in the roller end.
A preferred embodiment according to the present utility model, the fixed holder assembly include the first snap ring and block with first
The second snap ring that ring is correspondingly arranged, second snap ring are fixed on the wing-body, and first snap ring is rotatably arranged on
On second snap ring.
A preferred embodiment according to the present utility model, the fixed holder assembly further includes shipping and reselling on another market, first card
Ring and the second snap ring pass through rotation connection of shipping and reselling on another market.
A preferred embodiment according to the present utility model, first snap ring and second snap ring at least with one
Bearing assembly matches.
A preferred embodiment according to the present utility model, the main operation rudder face includes spoiler.
Other side according to the present utility model provides a kind of empennage, including empennage ontology and setting in empennage sheet
Main operation rudder face on body, empennage ontology side are arranged fixed holder assembly, bearing assembly are arranged on the main operation rudder face,
The main operation rudder face and empennage ontology are detachably connected by the bearing assembly and fixed holder assembly, and the main operation
Rudder face can be rotated relative to the empennage ontology.
A preferred embodiment according to the present utility model, the empennage include vertical empennage and/or tailplane.
A preferred embodiment according to the present utility model, the fixed holder assembly include the first snap ring and block with first
The second snap ring that ring is correspondingly arranged, second snap ring are fixed on the empennage ontology, and first snap ring is rotatably arranged on
On second snap ring.
A preferred embodiment according to the present utility model, the empennage further includes shipping and reselling on another market, first snap ring and
Two snap rings pass through rotation connection of shipping and reselling on another market.
A preferred embodiment according to the present utility model, the main operation rudder face are elevator and/or rudder, institute
Stating elevator includes third aerofoil, the 4th aerofoil and side rib, and the third aerofoil and the 4th aerofoil are coated on the side rib
Outside；And/or the rudder includes third aerofoil, the 4th aerofoil and side rib, the third aerofoil and the 4th aerofoil packet
It overlays on the outside of the side rib.
A preferred embodiment according to the present utility model, the bearing assembly include bearing and bearing block, the axis
It holds and is mounted on the bearing block.
A preferred embodiment according to the present utility model, the bearing assembly further includes shaft, and the shaft is worn
On the side rib, the bearing block is arranged in the roller end.
Other side according to the present utility model provides a kind of aircraft, including fuselage, further includes being arranged in fuselage
On such as above-mentioned wing, and such as above-mentioned empennage.
Wing, empennage and aircraft according to the present utility model, assembly are easy, facilitate maintenance maintenance, advantageously reduce dimension
Protect cost.
Detailed description of the invention
The preferred embodiment of the utility model is described in detail below in conjunction with attached drawing, in figure:
Fig. 1 shows the structural schematic diagram of the wing of one embodiment according to the present utility model；
Fig. 2 shows the stereogram exploded view of the wing of one embodiment according to the present utility model；
Assembling structure schematic diagram when Fig. 3 shows the installation of the structure in Fig. 2；
Assembling structure schematic diagram when Fig. 4 shows the installation of the structure in Fig. 2；
Fig. 5 is the structural schematic diagram after the wing assembling of one embodiment according to the present utility model；
Fig. 6 is the structural schematic diagram after the empennage assembling of one embodiment according to the present utility model；
Fig. 7 is the structural schematic diagram of the aircraft of one embodiment according to the present utility model.
The attached drawing is not drawn according to the actual ratio.
Specific embodiment
In order to which the technical solution of the utility model and advantage is more clearly understood, below in conjunction with attached drawing to the utility model
Exemplary embodiment be described in more detail.Obviously, described embodiment is only a part of the utility model
Embodiment, rather than the exhaustion of all embodiments.And in the absence of conflict, the embodiments of the present invention and implementation
Feature in example can be combined with each other.
Fig. 1 shows the structural schematic diagram of the wing of one embodiment according to the present utility model.
One aspect according to the present utility model provides a kind of wing, including wing-body 1 and setting in wing-body
Fixed holder assembly, main operation rudder face and/or main behaviour is arranged in main operation rudder face and/or main operation mechanism on 1, wing-body side
Make that bearing assembly is arranged in mechanism, main operation rudder face and/or main operation mechanism and wing-body 1 pass through bearing assembly and fixing seat
Component is detachably connected, and main operation rudder face and/or main operation mechanism can be rotated relative to the wing-body.
Above-mentioned and/or should be understood as including following situation: wing-body 1 only includes main operation rudder face, and wing-body 1 is only
Including main operation mechanism, wing-body 1 includes main operation rudder face and main operation mechanism simultaneously.
In the specific embodiment of Fig. 1, a main operation mechanism is set, which is the flap on wing-body 1
The wing 2 also sets up two main operation rudder faces on wing-body 1, is the first aileron 3 and the second aileron 4 respectively.1 side of wing-body
Aileron 12 is set, four fixed holder assemblies are set on aileron 12, is to fix holder assembly 13 positioned at the first of two sides and be located at respectively
The fixed holder assembly 11 of intermediate second.First bearing component 21 is set on wing flap 2, the is arranged on the first aileron 3, the second aileron 4
Two bearing assemblies 31.
By above structure, wing flap 2, the first aileron 3, the second aileron 4 can promptly be installed to wing-body 1 respectively
Or dismantled from wing-body 1, disassembly wing flap 2, the first aileron 3, any one in the second aileron 4 will not influence other two
It is a, facilitate maintenance maintenance.
Fig. 2 shows the stereogram exploded view of the wing of one embodiment according to the present utility model.
In the following, being illustrated by taking wing flap 2 as an example.Wing flap 2 includes the first aerofoil 22, the second aerofoil 25 and two side ribs 23,
First aerofoil 22 and the second aerofoil 25 are coated on 23 outside of side rib.Side rib 23 is that the first aerofoil 22 and the second aerofoil 25 provide support
Intensity.First bearing component 21 includes bearing 211 and bearing block 212, and bearing 211 is mounted on bearing block 212, bearing block 212
It is fixedly mounted on the side rib 23 along 2 extension direction of wing flap, in this way, a first bearing component is respectively arranged at two side ribs 23
21。
More specifically, wing flap 2 further includes shaft 24, shaft 24 is threaded through on side rib 23, and bearing block 212 is arranged in shaft 24
End.Bearing block 212 is fixed on side rib 23, and 212 one end of bearing block is connect with bearing 211, and other end is inserted in shaft 24, is turned
The rotation of axis 24 drives wing flap 2 to rotate relative to wing-body 1.
Two first bearing components 21 of wing flap 2 respectively with one first fixed holder assembly 13 and a second fixing seat group
Part 11 is corresponding.Be illustrated by taking the first fixed holder assembly 13 as an example, the first fixed holder assembly 13 include the first snap ring 131 and with
The second snap ring 133 that first snap ring 131 is correspondingly arranged, the second snap ring 133 are fixed on wing-body 1, more specifically, the second card
Ring 133 is fixed on aileron 12, and the first snap ring 131 is rotatably arranged on the second snap ring 133.
First fixed holder assembly 13 can also include shipping and reselling on another market 132, and the first snap ring 131 and the second snap ring 133 are by shipping and reselling on another market 132
Realize rotation connection.
Similarly, the second fixed holder assembly 11 also includes the first snap ring 111 and the second card being correspondingly arranged with the first snap ring 111
Ring 113, the second snap ring 113 are fixed on wing-body 1, more specifically, the second snap ring 113 is fixed on aileron 12, the first card
Ring 111 is rotatably arranged on the second snap ring 113.Second fixed holder assembly 11 can also include shipping and reselling on another market 112, the first snap ring 111 with
Second snap ring 113 passes through 112 realizations rotation connection of shipping and reselling on another market.
Since the two sides of wing flap 2 are adjacent with wing-body 1 and the first aileron 3 respectively, the second fixed holder assembly 11 is in addition to needing
It to be matched with the first bearing component 21 being arranged on wing flap 2, it is also necessary to the second bearing component 31 being arranged on the first aileron 3
It matches, that is, the first snap ring 111 and the second snap ring 113 can match with first bearing component 21 and second bearing component 31 simultaneously
Close, and the first snap ring 131 and the second snap ring 133 need to match with a first bearing component 21 being arranged on wing flap 2 or
A second bearing component (not shown) being arranged on person and the second aileron 4 matches.
Assembling structure schematic diagram when Fig. 3 shows the installation of the structure in Fig. 2.
It is illustrated by taking the structure between wing flap 2, the first aileron 3 as an example.First snap ring 111 and the second snap ring 113 are simultaneously
It is matched with first bearing component 21 and second bearing component 31.
Second bearing component 31 is identical as 21 structure of first bearing component, and second bearing component 31 includes bearing 311 and axis
Seat 312 is held, bearing 311 is mounted on bearing block 312, and bearing block 312 is fixedly mounted on the first pair along 3 extension direction of the first aileron
On the side rib 33 of the wing 3, in this way, a first bearing component 31 is respectively arranged at two side ribs 33 of the first aileron 3.
Bearing block 312 and bearing block 212 are respectively provided with connecting rod 312.1 and connecting rod 212.1, when 111 He of the first snap ring
When second snap ring 113 is matched with first bearing component 21 and second bearing component 31 simultaneously, bearing 311 and bearing 211 are located at
Between first snap ring 111 and the second snap ring 113,312 one side of bearing block is connect with bearing 311, the connecting rod of bearing block 312
312.1 pass through the shaft (not shown) that side rib 33 is inserted in the first aileron 3, and 212 one side of bearing block is connect with bearing 211, bearing block
212 connecting rod 212.1 passes through the shaft 24 that side rib 23 is inserted in wing flap 2.Second snap ring 113 is equipped with bolt hole 113.1, makes the
One snap ring 111 is along 112 rotations closure of shipping and reselling on another market, then makes between the first snap ring 111 and the second snap ring 113 by the way that bolt is screwed into bolt
Installation is completed to lock bearing 211 and bearing 311 in hole 113.1.
Assembling structure schematic diagram when Fig. 4 shows the installation of the structure in Fig. 2.
Specifically, when illustrating the first bearing component 21 being arranged on wing flap 2 and the first fixed installation of holder assembly 13 in Fig. 4
Structural schematic diagram.
When installation, bearing block 212 is fixed on side rib 23, bearing 211 is mounted on one end of bearing block 212, bearing
The connecting rod 212.1 of seat 212 is inserted in the shaft 24 (being not shown in Fig. 4) of wing flap 2 after side rib 23.211, the bearing of wing flap 2
Between the first snap ring 131 and the second snap ring 133, structure as shown in Figure 4 is formed.Later, make the first snap ring 131 around shipping and reselling on another market
132 rotations are completed to install between the first snap ring 131 and the second snap ring 133 by the way that bolt to be screwed into after bolt hole 133.1.
Fig. 5 is the structural schematic diagram after the wing assembling of one embodiment according to the present utility model.
The structure between wing flap 2, the first aileron 3 and first bearing component 21 and first has been described in detail above to fix
Structure when holder assembly 13 is installed, it is identical as above-mentioned installation principle, wing flap 2, the first aileron 3, the second aileron 4 can be installed
To wing-body 1, complete wing as shown in Figure 5 is formed.
In the above description, (in a specific embodiment, main operation rudder face is the first aileron 3 and to main operation rudder face
Two ailerons 4) it include spoiler.
Fig. 6 is the structural schematic diagram after the empennage assembling of one embodiment according to the present utility model.
It in the above description, is as explanation by taking wing as an example, the utility model is also possible to outside common wing,
It is also possible to empennage.
Empennage may include vertical empennage and/or tailplane.
Vertical empennage or tailplane as shown in FIG. 6, including empennage ontology 1a and the master being arranged on empennage ontology 1a
Operate rudder face 2a, fixed holder assembly is arranged in the empennage side ontology 1a, bearing assembly is set on main operation rudder face, main operation rudder face and
Empennage ontology is detachably connected by bearing assembly and fixed holder assembly, and main operation rudder face can turn relative to empennage ontology 1a
It is dynamic.
Specifically, a main operation rudder face 2a is set on empennage ontology 1a, two fixing seat groups are set on empennage ontology 1a
Part is the fixation holder assembly 13a positioned at two sides respectively.Bearing assembly (not shown) is set on the two sides main operation rudder face 2a.It is fixed
Holder assembly 13a is identical as the above-mentioned first fixed 13 structure of holder assembly, bearing assembly and above-mentioned 21 structure of first bearing component
It is identical.That is, fixed holder assembly 13a also includes the first snap ring and the second snap ring being correspondingly arranged with the first snap ring, the second snap ring is solid
It is scheduled on empennage ontology 1a, the first snap ring is rotatably arranged on second snap ring.Fixed holder assembly 13a further includes shipping and reselling on another market, the
One snap ring and the second snap ring pass through rotation connection of shipping and reselling on another market.
Main operation rudder face 2a is elevator and/or rudder, and elevator includes third aerofoil, the 4th aerofoil and side rib, institute
It states third aerofoil and the 4th aerofoil is coated on the outside of the rib of side；And/or the rudder includes third aerofoil, the 4th aerofoil
With side rib, the third aerofoil and the 4th aerofoil are coated on the outside of the side rib.Third aerofoil, the 4th aerofoil and side rib it
Between positional relationship it is identical as the positional relationship of the first above-mentioned aerofoil 22, the second aerofoil 25 and side rib 23.
Fig. 7 is the structural schematic diagram of the aircraft of one embodiment according to the present utility model.
Aircraft 100 includes two wings, 200, two tailplanes 300 and a vertical tail 400, and wing 200 can be with
It is wing shown in fig. 5 or its improvement structure, tailplane 300 and vertical tail 400 can be tailplane shown in fig. 6
Or vertical empennage or its improve structure.
Although the preferred embodiment of the utility model has been described, once a person skilled in the art knows basic
Creative concept, then additional changes and modifications may be made to these embodiments.Therefore, the following claims are intended to be interpreted as wraps
It includes preferred embodiment and falls into having altered and/or modifying, embodiment according to the present utility model for the scope of the utility model
The change and/or modification made should be covered within the scope of the utility model.
Claims (16)
1. a kind of wing, special including wing-body and the main operation rudder face being arranged on wing-body and/or main operation mechanism
Sign is that fixed holder assembly is arranged in the wing-body side, and bearing is arranged in the main operation rudder face and/or main operation mechanism
Component, the main operation rudder face and/or main operation mechanism and wing-body are removable by the bearing assembly and fixed holder assembly
It connects with unloading, and the main operation rudder face and/or main operation mechanism can be rotated relative to the wing-body.
2. wing according to claim 1, which is characterized in that the main operation mechanism is wing flap, and the wing flap includes the
One aerofoil, the second aerofoil and side rib, first aerofoil and the second aerofoil are coated on the outside of the side rib.
3. wing according to claim 2, which is characterized in that the bearing assembly includes bearing and bearing block, the axis
It holds and is mounted on the bearing block, the bearing block is fixedly mounted on the side rib along wing flap extension direction.
4. wing according to claim 3, which is characterized in that it further include shaft, the shaft is threaded through on the side rib,
The bearing block is arranged in the roller end.
5. wing according to claim 1, which is characterized in that the fixed holder assembly includes the first snap ring and blocks with first
The second snap ring that ring is correspondingly arranged, second snap ring are fixed on the wing-body, and first snap ring is rotatably arranged on
On second snap ring.
6. wing according to claim 5, which is characterized in that further include shipping and reselling on another market, first snap ring and the second snap ring are logical
Cross rotation connection of shipping and reselling on another market.
7. wing according to claim 5, which is characterized in that first snap ring and second snap ring at least with one
Bearing assembly matches.
8. wing according to claim 1-7, which is characterized in that the main operation rudder face includes spoiler.
9. a kind of empennage, including empennage ontology and the main operation rudder face being arranged on empennage ontology, which is characterized in that the empennage
Fixed holder assembly is arranged in ontology side, and bearing assembly, the main operation rudder face and empennage ontology is arranged on the main operation rudder face
It is detachably connected by the bearing assembly and fixed holder assembly, and the main operation rudder face can be relative to the empennage ontology
Rotation.
10. empennage according to claim 9, which is characterized in that the empennage includes vertical empennage and/or tailplane.
11. empennage according to claim 9 or 10, which is characterized in that the fixed holder assembly include the first snap ring and with
The second snap ring that first snap ring is correspondingly arranged, second snap ring are fixed on the empennage ontology, the first snap ring rotation
It is arranged on second snap ring.
12. empennage according to claim 11, which is characterized in that it further include shipping and reselling on another market, first snap ring and the second snap ring
Pass through rotation connection of shipping and reselling on another market.
13. empennage according to claim 9 or 10, which is characterized in that the main operation rudder face is elevator and/or direction
Rudder, the elevator include third aerofoil, the 4th aerofoil and side rib, and the third aerofoil and the 4th aerofoil are coated on described
On the outside of the rib of side；And/or
The rudder includes third aerofoil, the 4th aerofoil and side rib, and the third aerofoil and the 4th aerofoil are coated on institute
It states on the outside of the rib of side.
14. empennage according to claim 13, which is characterized in that the bearing assembly includes bearing and bearing block, described
Bearing is mounted on the bearing block.
15. empennage according to claim 14, which is characterized in that further include shaft, the shaft is threaded through the side rib
On, the bearing block is arranged in the roller end.
16. a kind of aircraft, including fuselage, which is characterized in that further include being arranged on fuselage such as any one of claim 1-8 institute
The wing stated, and such as the described in any item empennages of claim 9-15.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820754524.3U CN208947583U (en) | 2018-05-21 | 2018-05-21 | Wing, empennage and aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820754524.3U CN208947583U (en) | 2018-05-21 | 2018-05-21 | Wing, empennage and aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN208947583U true CN208947583U (en) | 2019-06-07 |
Family
ID=66730330
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201820754524.3U Active CN208947583U (en) | 2018-05-21 | 2018-05-21 | Wing, empennage and aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN208947583U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108609159A (en) * | 2018-05-21 | 2018-10-02 | 顺丰科技有限公司 | Wing, empennage and aircraft |
-
2018
- 2018-05-21 CN CN201820754524.3U patent/CN208947583U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108609159A (en) * | 2018-05-21 | 2018-10-02 | 顺丰科技有限公司 | Wing, empennage and aircraft |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20210716 Address after: 518000 5th floor, block B, building 1, software industry base, Yuehai street, Nanshan District, Shenzhen City, Guangdong Province Patentee after: Fengyi Technology (Shenzhen) Co.,Ltd. Address before: 518000 Xuefu Road (south) and Baishi Road (east) intersection of Nanshan District, Shenzhen City, Guangdong Province, 6-13 floors, Block B, Shenzhen Software Industry Base Patentee before: SF TECHNOLOGY Co.,Ltd. |