CN206327570U - A kind of spherical aircraft - Google Patents
A kind of spherical aircraft Download PDFInfo
- Publication number
- CN206327570U CN206327570U CN201621470202.3U CN201621470202U CN206327570U CN 206327570 U CN206327570 U CN 206327570U CN 201621470202 U CN201621470202 U CN 201621470202U CN 206327570 U CN206327570 U CN 206327570U
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- annulus
- rotating shaft
- motor
- spherical
- cabinet
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Abstract
The utility model is related to a kind of aircraft; in particular it is a kind of spherical aircraft; belong to unmanned plane during flying device field; not only C60 spherical housings can effectively protect spiral single-blade, motor and video camera; and it overcomes the anti-twisted power of fuselage by inclined rudder face; simpler using bi-motor double helix single-blade structure compared to helicopter, cost is also lower.Rotating disk includes connecting rod, round seat and annulus.Rudder plate includes bull stick, pull bar, rudder face, axostylus axostyle, fixed seat, connecting plate and steering wheel.Annulus I is movably connected on C60 spherical housings by rotating shaft I, and annulus II is movably connected on annulus I by rotating shaft II, and rotating disk is movably connected on annulus II by rotating shaft III.Rudder plate is arranged on the connecting rod of rotating disk.Cabinet and motor are installed in round seat, and motor obtains upper end and is provided with spiral single-blade, and video camera is arranged on the lower end of cabinet.
Description
Technical field
The utility model is related to a kind of aircraft, is in particular a kind of spherical aircraft, belongs to unmanned plane during flying dress
Put field.
Background technology
In recent years, the development of domestic unmanned plane was very fast.In addition to military use, due to unmanned plane advantage of lower cost,
The advantage such as risk that no one was injured, survival ability are strong, mobility is good, easy to use so that unmanned plane is in Aerial photography, address
The civil area application prospects such as measurement, freeway management, forest fire protection inspection and emergency management and rescue, rescue are extremely wide.Rotor
Formula unmanned plane is divided into single rotor and many rotor structures.Single rotor refers mainly to the type of helicopter class, and the adjustment of its flight attitude is main
By pitch, its spiral single-blade is exposed fragile, and elimination spiral single-blade reaction torque structure is complex, unfavorable under severe conditions
In flight and land, it is relatively simple for multiaxis its control of flying, but cost is higher, therefore a kind of spherical aircraft of design is with regard to ten
Divide necessity.
The content of the invention
The utility model is mainly solving the technical problems that provide a kind of spherical aircraft, and not only C60 spherical housings can be with
Effectively protection spiral single-blade, motor and video camera, and it overcomes the anti-twisted power of fuselage by inclined rudder face, compared to helicopter
Simpler using bi-motor double helix single-blade structure, cost is also lower.
In order to solve the above technical problems, the utility model is related to a kind of aircraft, in particular it is a kind of spherical flight
Device, belongs to unmanned plane during flying device field, including C60 spherical housings, bolted node sphere, rotating shaft I, annulus I, annulus II, rotating disk, rudder
Plate, cabinet, rotating shaft II, rotating shaft III, motor, spiral single-blade and video camera, not only C60 spherical housings can effectively protect spiral list
Oar, motor and video camera, and it overcomes the anti-twisted power of fuselage by inclined rudder face, compared to helicopter using the double spiral shells of bi-motor
Rotation single-blade structure is simpler, and cost is also lower.
Rotating disk includes connecting rod, round seat and annulus, and wherein connecting rod has four, one end connection round seat of connecting rod, connecting rod it is another
End connection annulus.Rudder plate includes one end connection of bull stick, pull bar, rudder face, axostylus axostyle, fixed seat, connecting plate and steering wheel, wherein pull bar
Bull stick, the other end connection fixing base of pull bar, bull stick is arranged on steering wheel, and steering wheel is arranged on connecting plate, and fixed seat is arranged on
On rudder face.Annulus I is movably connected on C60 spherical housings by rotating shaft I, and annulus II is movably connected in annulus I by rotating shaft II
On, rotating disk is movably connected on annulus II by rotating shaft III.Rudder plate is arranged on the connecting rod of rotating disk.Cabinet and motor are installed in
In round seat, motor obtains upper end and is provided with spiral single-blade, and video camera is arranged on the lower end of cabinet.
As the further optimization of the technical program, it is provided with the cabinet described in a kind of spherical aircraft of the utility model
Lithium battery.
It is used as the further optimization of the technical program, bull stick, pull bar described in a kind of spherical aircraft of the utility model, rudder
Face, axostylus axostyle, fixed seat, connecting plate and steering wheel have 4.
As the further optimization of the technical program, it is provided with the cabinet described in a kind of spherical aircraft of the utility model
Lithium battery and control device, wherein lithium battery are connected with steering wheel, motor and video camera electric wire.
A kind of the utility model spherical aircraft has the beneficial effect that：
A kind of spherical aircraft of the utility model, not only C60 spherical housings can effectively protect spiral single-blade, motor and take the photograph
Shadow machine, and it overcomes the anti-twisted power of fuselage by inclined rudder face, and bi-motor double helix single-blade structure is used compared to helicopter
Simpler, cost is also lower.
Brief description of the drawings
The utility model is described in more detail with specific implementation method below in conjunction with the accompanying drawings.
Fig. 1 is a kind of structural representation of spherical aircraft of the utility model.
Fig. 2 is the structural representation of rotating disk 6.
Fig. 3 is A-A direction views in Fig. 1.
Fig. 4 is a kind of partial structural diagram of spherical aircraft of the utility model.
In figure：C60 spherical housings 1；Bolted node sphere 2；Rotating shaft I 3；Annulus I 4；Annulus II 5；Rotating disk 6；Connecting rod 6-1；Round seat 6-
2；Annulus 6-3；Rudder plate 7；Bull stick 7-1；Pull bar 7-2；Rudder face 7-3；Axostylus axostyle 7-4；Fixed seat 7-5；Connecting plate 7-6；Steering wheel 7-7；
Cabinet 8；Rotating shaft II 9；Rotating shaft III 10；Motor 11；Spiral single-blade 12；Video camera 13.
Embodiment
Embodiment one：
Illustrate present embodiment with reference to Fig. 1,2,3,4, the utility model is related to a kind of aircraft, is in particular
A kind of spherical aircraft, belongs to unmanned plane during flying device field, including C60 spherical housings 1, bolted node sphere 2, rotating shaft I 3, annulus I 4,
Annulus II 5, rotating disk 6, rudder plate 7, cabinet 8, rotating shaft II 9, rotating shaft III 10, motor 11, spiral single-blade 12 and video camera 13, not only
C60 spherical housings can effectively protect spiral single-blade, motor and video camera, and it overcomes the anti-of fuselage by inclined rudder face
Torsion, simpler using bi-motor double helix single-blade structure compared to helicopter, cost is also lower.
Rotating disk 6 includes connecting rod 6-1, round seat 6-2 and annulus 6-3, and wherein connecting rod 6-1 has four, connecting rod 6-1 one end connection
Round seat 6-2, connecting rod 6-1 other end connection annulus 6-3.Rudder plate 7 include bull stick 7-1, pull bar 7-2, rudder face 7-3, axostylus axostyle 7-4,
Fixed seat 7-5, connecting plate 7-6 and steering wheel 7-7, wherein pull bar 7-2 one end connection bull stick 7-1, pull bar 7-2 other end connection
Fixed seat 7-5, bull stick 7-1 are arranged on steering wheel 7-7, and steering wheel 7-7 is arranged on connecting plate 7-6, and fixed seat 7-5 is arranged on rudder face
On 7-3, rudder face 7-3 angle of inclination is adjusted by steering wheel 7-7 and pull bar 7-2.Some nodes are provided with C60 spherical housings 1
Ball 2, annulus I 4 is movably connected on C60 spherical housings 1 by rotating shaft I 3, and annulus II 5 is movably connected in annulus by rotating shaft II 9
On I 4, rotating disk 6 is movably connected on annulus II 5 by rotating shaft III 10.Rudder plate 7 is arranged on the connecting rod 6-1 of rotating disk 6, and C60 is spherical
Shell 1 can effectively protect spiral single-blade 12, motor 11 and video camera 13.Cabinet 8 and motor 11 are installed on round seat 6-2,
Motor 11 obtains upper end and is provided with spiral single-blade 12, and video camera 13 is arranged on the lower end of cabinet 8, and video camera 13 is used for observing.Spiral
The blowing downwards of single-blade 12 produces lift and provides power, while air-flow is oriented to by the inclined rudder face 7-3 of following two, produces moment of torsion
To overcome spin, simpler using bi-motor double helix single-blade structure compared to helicopter, cost is also lower, and at the same time also two
Individual rudder face 7-3 can be flown by the control of the control device in cabinet 8 to change of flight attitude and side.
Embodiment two：
Illustrate present embodiment with reference to Fig. 1,2,3,4, present embodiment is described further to embodiment one, institute
Lithium battery and control device are provided with the cabinet 8 stated.
Embodiment three：
Illustrate present embodiment with reference to Fig. 1,2,3,4, present embodiment is described further to embodiment one, institute
Bull stick 7-1, pull bar 7-2, rudder face 7-3, axostylus axostyle 7-4, fixed seat 7-5, connecting plate 7-6 and the steering wheel 7-7 stated has 4.
Embodiment four：
Illustrate present embodiment with reference to Fig. 1,2,3,4, present embodiment is described further to embodiment one, institute
Lithium battery and control device, wherein lithium battery and steering wheel 7-7, motor 11 and the electric wire of video camera 13 are provided with the outer cabinet 8 stated
Connection.
Embodiment five：
Illustrate present embodiment with reference to Fig. 1,2,3,4, present embodiment is described further to embodiment one, institute
Annulus I 4, annulus II 5 and the rotating disk 6 stated constitute gyroscope mechanical structure.
A kind of operation principle of spherical aircraft of the utility model：It is spherical that annulus I 4 is movably connected in C60 by rotating shaft I 3
On shell 1, annulus II 5 is movably connected on annulus I 4 by rotating shaft II 9, and rotating disk 6 is movably connected in annulus by rotating shaft III 10
On II 5, make the holding level of spiral single-blade 12, it is ensured that stability during flight.Rudder plate 7 is arranged on the connecting rod 6-1 of rotating disk 6, C60
Spherical housing 1 can effectively protect cabinet 8, spiral single-blade 12, motor 11 and video camera 13.Lithium battery in cabinet 8 is steering wheel
7-7 and motor 11 fix rudder face 7-3, spiral single-blade 12 after providing power, two of which steering wheel 7-7 adjustment rudder faces 7-3 angle
Blowing produces lift and provides power downwards, while air-flow is oriented to by the inclined rudder face 7-3 of following two, produces moment of torsion to overcome
Spin, at the same time also two rudder face 7-3 can be used to change of flight attitude by the control of the control device in cabinet 8 and side fly.
Certainly, described above is not limitation of the utility model, and the utility model is also not limited to the example above, this skill
Change, remodeling, addition or replacement that the those of ordinary skill in art field is made in essential scope of the present utility model, also belong to
In protection domain of the present utility model.
Claims (4)
1. a kind of spherical aircraft, including C60 spherical housings (1), bolted node sphere (2), rotating shaft I (3), annulus I (4), annulus II
(5), rotating disk (6), rudder plate (7), cabinet (8), rotating shaft II (9), rotating shaft III (10), motor (11), spiral single-blade (12) and photography
Machine (13), it is characterised in that：Rotating disk (6) includes connecting rod (6-1), round seat (6-2) and annulus (6-3), and wherein connecting rod (6-1) has four
It is individual, one end connection round seat (6-2) of connecting rod (6-1), the other end connection annulus (6-3) of connecting rod (6-1)；Rudder plate (7) includes turning
Bar (7-1), pull bar (7-2), rudder face (7-3), axostylus axostyle (7-4), fixed seat (7-5), connecting plate (7-6) and steering wheel (7-7), wherein
One end connection bull stick (7-1) of pull bar (7-2), the other end connection fixing base (7-5) of pull bar (7-2), bull stick (7-1) is arranged on
On steering wheel (7-7), steering wheel (7-7) is arranged on connecting plate (7-6), and fixed seat (7-5) is arranged on rudder face (7-3)；Annulus I
(4) it is movably connected in by rotating shaft I (3) on C60 spherical housings (1), annulus II (5) is movably connected in circle by rotating shaft II (9)
On ring I (4), rotating disk (6) is movably connected on annulus II (5) by rotating shaft III (10)；Rudder plate (7) is arranged on the company of rotating disk (6)
On bar (6-1)；Cabinet (8) and motor (11) are installed in round seat (6-2), and motor (11) obtains upper end and is provided with spiral single-blade
(12), video camera (13) is arranged on the lower end of cabinet (8).
2. a kind of spherical aircraft according to claim 1, it is characterised in that：Lithium electricity is provided with described cabinet (8)
Pond and control device.
3. a kind of spherical aircraft according to claim 1, it is characterised in that：Described bull stick (7-1), pull bar (7-2),
Rudder face (7-3), axostylus axostyle (7-4), fixed seat (7-5), connecting plate (7-6) and steering wheel (7-7) have 4.
4. a kind of spherical aircraft according to claim 1, it is characterised in that：Lithium electricity is provided with described cabinet (8)
Pond and control device, wherein lithium battery are connected with steering wheel (7-7), motor (11) and video camera (13) electric wire.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621470202.3U CN206327570U (en) | 2016-12-30 | 2016-12-30 | A kind of spherical aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621470202.3U CN206327570U (en) | 2016-12-30 | 2016-12-30 | A kind of spherical aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206327570U true CN206327570U (en) | 2017-07-14 |
Family
ID=59292834
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621470202.3U Expired - Fee Related CN206327570U (en) | 2016-12-30 | 2016-12-30 | A kind of spherical aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206327570U (en) |
-
2016
- 2016-12-30 CN CN201621470202.3U patent/CN206327570U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170714 Termination date: 20171230 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |