CN209441605U - A kind of Novel movable fixed wing aircraft wing - Google Patents
A kind of Novel movable fixed wing aircraft wing Download PDFInfo
- Publication number
- CN209441605U CN209441605U CN201822236946.4U CN201822236946U CN209441605U CN 209441605 U CN209441605 U CN 209441605U CN 201822236946 U CN201822236946 U CN 201822236946U CN 209441605 U CN209441605 U CN 209441605U
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- CN
- China
- Prior art keywords
- wing
- aileron
- novel movable
- movable fixed
- main support
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- 239000000203 mixture Substances 0.000 claims abstract description 4
- 238000009434 installation Methods 0.000 claims description 14
- 239000000463 material Substances 0.000 claims description 6
- 229910000737 Duralumin Inorganic materials 0.000 claims description 3
- 229910045601 alloy Inorganic materials 0.000 claims description 3
- 239000000956 alloy Substances 0.000 claims description 3
- 238000012423 maintenance Methods 0.000 description 7
- 238000010586 diagram Methods 0.000 description 5
- 238000000034 method Methods 0.000 description 3
- 239000000446 fuel Substances 0.000 description 1
- 239000002828 fuel tank Substances 0.000 description 1
- 230000006641 stabilisation Effects 0.000 description 1
- 238000011105 stabilization Methods 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
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Abstract
The utility model discloses a kind of Novel movable fixed wing aircraft wings, including wing root and connecting rod, connecting rod is provided on the left of the wing root, the two sides up and down of the connecting rod are provided with connector, interior aileron is provided on the right side of the wing root, the bottom of the interior aileron is provided with tire device, and external aileron is provided on the right side of interior aileron, the outer rim wing is provided on the right side of the external aileron, the side of the outer rim wing is provided with navigation lights, wing flap is provided between the wing root and the outer rim wing, the wing root, interior aileron, external aileron and the outer rim wing are by rear wall, stringer, covering, spar, front wall and rib composition, more ribs are provided between the front wall and rear wall, the top of the more ribs is equipped with more stringers, and spar is provided at the upper middle position of more ribs, the utility model is on the basis of existing It has installed connector and connecting rod additional, the utility model can be assisted to be installed and replaced, improved the service efficiency of the utility model.
Description
Technical field
The utility model belongs to space flight and aviation correlative technology field, and in particular to a kind of Novel movable fixed wing aircraft machine
The wing.
Background technique
Wing is one of important component of aircraft, is mounted on fuselage.Its main effect is generation lift, while can also
To set ammunition cabins and fuel tank inside wing, undercarriage can be awing collected.In addition, being also equipped on wing improves
Fly the aileron with the wing flap of landing data and for aircraft lateral control, some also increases lift equipped with slat etc. in the leading edge of a wing
Device.
Existing fixed wing aircraft wing technology has the following problems: existing fixed wing aircraft wing is welded on fuselage more
On, it is larger for wing maintenance difficulty during the maintenance of aircraft, inconvenience is brought for user, especially in machine
Wing failure needs to carry out fuselage whole dismantling in the case where needing replacing, and has aggravated the work difficulty and workload of user.
Utility model content
The purpose of this utility model is to provide a kind of Novel movable fixed wing aircraft wings, to solve above-mentioned background skill
The difficult problem of the wing maintenance replacement proposed in art.
To achieve the above object, the utility model provides the following technical solutions: a kind of Novel movable fixed wing aircraft machine
The wing, including wing root and connecting rod are provided with connecting rod on the left of the wing root, and the two sides up and down of the connecting rod, which are provided with, to be connect
Head is provided with interior aileron on the right side of the wing root, and the bottom of the interior aileron is provided with tire device, and sets on the right side of interior aileron
It is equipped with external aileron, the outer rim wing is provided on the right side of the external aileron, the side of the outer rim wing is provided with navigation lights, the wing root
Be provided with wing flap between the outer rim wing, the wing root, interior aileron, external aileron and the outer rim wing by rear wall, stringer, covering, spar,
Front wall and rib composition, are provided with more ribs, the top of the more ribs is equipped with more between the front wall and rear wall
Stringer, and spar is provided at the upper middle position of more ribs, the rear wall, stringer, spar, front wall and rib coat
In covering.
Preferably, the wing flap is made of fixed pin, wing body, flow-disturbing slot and installation axle, and the both ends of the wing body are all provided with
It is equipped with fixed pin, and is provided with flow-disturbing slot on the upper surface of wing body, the side of the wing body is provided with installation axle.
Preferably, the tire device is by shaft, Extension support, idler wheel, secondary hydraulic stem, master hydraulic bar, main support and peace
Composition is shelved, the bottom of the mounting rack is provided with shaft, and main support is provided in the shaft, and the end of the main support is set
It is equipped with Extension support, the main support is fixedly connected with Extension support by hinge, and the middle position of the main support is provided with master
Hydraulic stem is provided with secondary hydraulic stem on the Extension support, and the end of Extension support is provided with idler wheel.
Preferably, a length of 1200mm of the wing flap, width 180mm.
Preferably, the material of the rear wall, spar and front wall is extra super duralumin alloy.
Preferably, the shapes and sizes of described two fixed pins are all the same, and the middle position of the installation axle is set
It is equipped with installation through-hole.
Preferably, the specification and shape of the master hydraulic bar and secondary hydraulic stem are all the same.
Preferably, the main support is identical with the making material of Extension support, and main support is identical with the shape of Extension support, institute
The length for stating main support is two times of Extension support length.
Compared with prior art, the utility model provides a kind of Novel movable fixed wing aircraft wing, has following
The utility model has the advantages that the movable fixed wing aircraft wing of the utility model has installed connecting rod additional and has been connect on the basis of existing equipment
The utility model can be fixed on fuselage by connecting rod and connector during use, be made by head, user
When user needs to carry out maintenance to the utility model, user can be by connecting rod and connector by the utility model
Carry out maintenance is removed with slave, the workload of user is greatly saved, further improves the utility model
Service efficiency.
Detailed description of the invention
Attached drawing is used to provide a further understanding of the present invention, and constitutes part of specification, practical with this
Novel embodiment is used to explain the utility model together, does not constitute limitations of the present invention, in the accompanying drawings:
Fig. 1 be the utility model proposes a kind of Novel movable fixed wing aircraft wing structure schematic diagram；
Fig. 2 be the utility model proposes a kind of Novel movable fixed wing aircraft wing side structure schematic diagram；
Fig. 3 be the utility model proposes wing root structural schematic diagram；
Fig. 4 be the utility model proposes flap configurations schematic diagram；
Fig. 5 be the utility model proposes tire device structural schematic diagram；
In figure: 1, wing root；2, interior aileron；3, wing flap；4, the outer rim wing；5, navigation lights；6, external aileron；7, tire device；8,
Connector；9, connecting rod；10, rear wall；11, stringer；12, covering；13, spar；14, front wall；15, rib；31, fixed pin；32, the wing
Body；33, flow-disturbing slot；34, installation axle；71, shaft；72, Extension support；73, idler wheel；74, secondary hydraulic stem；75, master hydraulic bar；76,
Main support；77, mounting rack.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Fig. 1-5 is please referred to, the utility model provides a kind of technical solution: a kind of Novel movable fixed wing aircraft wing,
Including wing root 1 and connecting rod 9, the left side of wing root 1 is provided with connecting rod 9, and the two sides up and down of connecting rod 9 are provided with connector 8, the wing
The right side of root 1 is provided with interior aileron 2, and the bottom of interior aileron 2 is provided with tire device 7, and the right side of interior aileron 2 is provided with outer pair
The wing 6, the right side of external aileron 6 are provided with the outer rim wing 4, and the side of the outer rim wing 4 is provided with navigation lights 5, between wing root 1 and the outer rim wing 4
It is provided with wing flap 3, wing root 1, interior aileron 2, external aileron 6 and the outer rim wing 4 are by rear wall 10, stringer 11, covering 12, spar 13, preceding
Wall 14 and rib 15 form, and more ribs 15 are provided between front wall 10 and rear wall 14, the top of more ribs 15 is equipped with more
Root stringer 11, and spar 13 is provided at the upper middle position of more ribs 15, rear wall 10, stringer 11, spar 13, front wall 14
It is coated in covering 12 with rib 15.
Further, wing flap 3 is made of fixed pin 31, wing body 32, flow-disturbing slot 33 and installation axle 34, and the both ends of wing body 32 are equal
It is provided with fixed pin 31, and is provided with flow-disturbing slot 33 on the upper surface of wing body 32, the side of wing body 32 is provided with installation axle 34.
Further, tire device 7 is by shaft 71, Extension support 72, idler wheel 73, secondary hydraulic stem 74, master hydraulic bar 75, main branch
Frame 76 and mounting rack 77 form, and the bottom of mounting rack 77 is provided with shaft 71, main support 76, main support 76 are provided in shaft 71
End be provided with Extension support 72, main support 76 is fixedly connected with Extension support 72 by hinge, the middle position of main support 76
It is provided with master hydraulic bar 75, secondary hydraulic stem 74 is provided on Extension support 72, and the end of Extension support 72 is provided with idler wheel 73.
Further, a length of 1200mm of wing flap 3, width 180mm.
Further, the material of rear wall 10, spar 13 and front wall 14 is extra super duralumin alloy.
Further, the shapes and sizes of two fixed pins 31 are all the same, and the middle position of installation axle 34 is provided with installation
Through-hole.
Further, the specification and shape of master hydraulic bar 75 and secondary hydraulic stem 74 are all the same.
Further, main support 76 is identical with the making material of Extension support 72, and the shape phase of main support 76 and Extension support 72
Together, the length of main support 76 is two times of 72 length of Extension support.
The working principle and process for using of the utility model: after the utility model installs, the utility model is moved to
Then the utility model is fixedly mounted on fixed wing aircraft, so by required position by connector 8 and connecting rod 9
When aircraft starts to start to take off afterwards, interior aileron 2, external aileron 6 and the meeting second-mission aircraft of the outer rim wing 4 on the utility model fly
Row, navigation lights 5, which is started to work, during flight shows aircraft navigation state, and wing flap 3 is turned to and gone up and down in aircraft
It carries out to navigate by water with second-mission aircraft in the process, wing flap 3 is fixed on the utility model by fixed pin 31 and installation axle 34, can be with
It is rotated upwardly and downwardly, while the flow-disturbing slot 33 on wing flap 3 effectively reduces air drag of aircraft during navigation, both saves
The fuel for having saved aircraft also improves the stability of aircraft navigation, and interior 2 lower section of aileron is mounted on when aircraft landing
Tire device 7 can smoothly be landed with second-mission aircraft on the ground, the master hydraulic bar 75 in tire device 7 and secondary hydraulic stem 74
The stabilization of main support 76 and Extension support 72 can be effectively kept, the stability of the utility model during the work time is improved,
During the utility model needs to be serviced maintenance or replacement, user can be by connecting rod 9 and connector 8 by this reality
With dismantling with novel slave, maintenance or replacement then are carried out to the utility model.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (8)
1. a kind of Novel movable fixed wing aircraft wing, including wing root (1) and connecting rod (9), it is characterised in that: the wing root
(1) it is provided on the left of connecting rod (9), the two sides up and down of the connecting rod (9) are provided with connector (8), the wing root (1)
Right side is provided with interior aileron (2), and the bottom of the interior aileron (2) is provided with tire device (7), and is set on the right side of interior aileron (2)
It is equipped with external aileron (6), is provided with the outer rim wing (4) on the right side of the external aileron (6), the side of the outer rim wing (4) is provided with boat
Portable lighter (5) is provided with wing flap (3) between the wing root (1) and the outer rim wing (4), the wing root (1), interior aileron (2), external aileron
(6) it is made of with the outer rim wing (4) rear wall (10), stringer (11), covering (12), spar (13), front wall (14) and rib (15),
More ribs (15) are provided between the front wall (14) and rear wall (10), the top of the more ribs (15) is equipped with more
Stringer (11), and spar (13) are provided at the upper middle position of more ribs (15), it is described after wall (10), stringer (11),
Spar (13), front wall (14) and rib (15) are coated in covering (12).
2. a kind of Novel movable fixed wing aircraft wing according to claim 1, it is characterised in that: the wing flap (3)
It is made of fixed pin (31), wing body (32), flow-disturbing slot (33) and installation axle (34), the both ends of the wing body (32) are provided with
Fixed pin (31), and flow-disturbing slot (33) are provided on the upper surface of wing body (32), the side of the wing body (32) is provided with installation
Axis (34).
3. a kind of Novel movable fixed wing aircraft wing according to claim 1, it is characterised in that: the tire device
It (7) is by shaft (71), Extension support (72), idler wheel (73), secondary hydraulic stem (74), master hydraulic bar (75), main support (76) and peace
(77) composition is shelved, the bottom of the mounting rack (77) is provided with shaft (71), is provided with main support on the shaft (71)
(76), the end of the main support (76) is provided with Extension support (72), and the main support (76) and Extension support (72) pass through hinge
It is fixedly connected, the middle position of the main support (76) is provided with master hydraulic bar (75), is provided on the Extension support (72)
Secondary hydraulic stem (74), and the end of Extension support (72) is provided with idler wheel (73).
4. a kind of Novel movable fixed wing aircraft wing according to claim 1, it is characterised in that: the wing flap (3)
A length of 1200mm, width 180mm.
5. a kind of Novel movable fixed wing aircraft wing according to claim 1, it is characterised in that: wall after described
(10), the material of spar (13) and front wall (14) is extra super duralumin alloy.
6. a kind of Novel movable fixed wing aircraft wing according to claim 2, it is characterised in that: described two described
The shapes and sizes of fixed pin (31) are all the same, and the middle position of the installation axle (34) is provided with installation through-hole.
7. a kind of Novel movable fixed wing aircraft wing according to claim 3, it is characterised in that: the master hydraulic bar
(75) and the specification of secondary hydraulic stem (74) and shape it is all the same.
8. a kind of Novel movable fixed wing aircraft wing according to claim 3, it is characterised in that: the main support
(76) identical with the making material of Extension support (72), and main support (76) is identical with the shape of Extension support (72), the main support
(76) length is two times of Extension support (72) length.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822236946.4U CN209441605U (en) | 2018-12-28 | 2018-12-28 | A kind of Novel movable fixed wing aircraft wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201822236946.4U CN209441605U (en) | 2018-12-28 | 2018-12-28 | A kind of Novel movable fixed wing aircraft wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209441605U true CN209441605U (en) | 2019-09-27 |
Family
ID=68015875
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201822236946.4U Active CN209441605U (en) | 2018-12-28 | 2018-12-28 | A kind of Novel movable fixed wing aircraft wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209441605U (en) |
-
2018
- 2018-12-28 CN CN201822236946.4U patent/CN209441605U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PP01 | Preservation of patent right | ||
| PP01 | Preservation of patent right |
Effective date of registration: 20240624 Granted publication date: 20190927 |
|
| PD01 | Discharge of preservation of patent | ||
| PD01 | Discharge of preservation of patent |
Date of cancellation: 20240805 Granted publication date: 20190927 |