CN208031877U - A kind of self-control aircraft amusement device - Google Patents
A kind of self-control aircraft amusement device Download PDFInfo
- Publication number
- CN208031877U CN208031877U CN201820141939.3U CN201820141939U CN208031877U CN 208031877 U CN208031877 U CN 208031877U CN 201820141939 U CN201820141939 U CN 201820141939U CN 208031877 U CN208031877 U CN 208031877U
- Authority
- CN
- China
- Prior art keywords
- aircraft
- upside
- self
- shaft
- sensing device
- 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.)
- Expired - Fee Related
Links
Abstract
The utility model is related to a kind of self-control aircraft amusement devices,It includes pedestal,Chassis interior is provided with motor,Output shaft is provided on motor,Boss is provided on output shaft,It is provided with the first swivel bearing on the upside of pedestal,It is provided with shaft on the upside of first swivel bearing,Fluted A is set in the middle part of rotating shaft bottom surface,Boss is connected with groove A,It is provided with supporting rack on the downside of shaft,Cylinder is provided on supporting rack,Upside is provided with fixing end in shaft,Outwardly extending large arm is provided in fixing end,Fluted B and mounting hole are set in large arm,Inside cylinder connecting groove B,Large arm end connects aircraft,Direction switch is provided on aircraft,Track and sensing device A,It is provided with laser gun on the upside of track,Sensing device is arranged in the middle part of the rear side of aircraft,It is provided with the second swivel bearing on the upside of shaft,It is provided with head cover on the upside of second swivel bearing,Sensing device B is provided on head cover;The utility model has the advantages that reasonable for structure, level of comfort is high, easy to spread.
Description
Technical field
The utility model belongs to amusement device technical field, and in particular to a kind of self-control aircraft amusement device.
Background technology
Self-control aircraft is a kind of around the rotation of vertical axis center, the free lifting aircraft class amusement facility of lifting;Aircraft surrounds
Center rocket or the rotation of the decoration of other moulding, and rising is freely controlled, it is that tourist experience flies general feeling, obtains tourist's
Like;Although self-control aircraft has obtained extensive development, there is also deficiencies, such as:Transmission structures are complicated, repair and peace
Falling speed is not easy to control after dress is complicated, aircraft rises, and causes tourist's discomfort, amusement facility not abundant etc. enough;Therefore it provides one
It is kind reasonable for structure, installation is simple, level of comfort height, good economy performance, self-control aircraft amusement device easy to spread are that have very much must
It wants.
Invention content
The purpose of this utility model is to overcome the deficiencies in the prior art, and offer one kind is reasonable for structure, installation is simple,
Level of comfort height, good economy performance, self-control aircraft amusement device easy to spread.
What the purpose of this utility model was realized in:A kind of self-control aircraft amusement device, it includes pedestal, the bottom
Seat is internally provided with motor, and output shaft is provided on the motor, boss, the pedestal are provided on the output shaft
Upside is provided with the first swivel bearing, and shaft is provided on the upside of first swivel bearing, is set in the middle part of the rotating shaft bottom surface
It is equipped with groove A, the boss is connected with groove A, is provided with supporting rack on the downside of the shaft, is set on the supporting rack
It is equipped with cylinder, upside is provided with fixing end in the shaft, and outwardly extending large arm is provided in the fixing end, described
Large arm on fluted B and mounting hole be set, inside the cylinder connecting groove B, the large arm end connects aircraft, institute
It is provided with direction switch, track and sensing device A on the aircraft stated, laser gun, the sense are provided on the upside of the track
It answers device A to be arranged in the middle part of the rear side of aircraft, the second swivel bearing, second rotary shaft is provided on the upside of the shaft
It holds upside and is provided with head cover, sensing device B is provided on the head cover.
The interior of aircraft is provided with signal receiver, control device, music player and solenoid valve.
The motor is decelerating motor.
The track is curved track.
The groove A contour lines are rectangle and circle and are connect with boss that the groove B is rectangular recess.
The large arm is that pin is connect with the connection type of cylinder and fixing end.
The sensing device B can be designed to different shapes.
The beneficial effects of the utility model:The utility model uses motor, in use, motor is started to work, motor drives
Output shaft rotates, and output shaft drives boss rotation, because boss and groove A are combined, so shaft starts to rotate, flies to drive
Machine rotates, simple and reasonable, for ease of maintenaince and installs;Using cylinder, achieve the purpose that aircraft raising and lowering, cylinder connect
It is provided with electrically operated valve on the tracheae connect, speed can voluntarily be controlled when declining by having reached aircraft, avoided aircraft and declined
Cause tourist uncomfortable suddenly;Using head cover, sensing device A, sensing device B, aircraft, direction switch, laser gun and track, tourist
Oneself direction switch can be controlled, then solenoid valve is controlled by direction switch again, aircraft is made to reach the effect of lifting
Fruit, head cover are fixed, and sensing device A is provided on the sensing device B and aircraft being provided on head cover, push up sensing device
B may be designed to different shapes, and to increase liking for tourist, these shapes can be similar to the decoration on respective aircraft, these bands
It is exactly to represent which aircraft to have the sensing device B of similar fitgures, and the laser gun on track can carry out position rotation, to head cover
On sensing device B or aircraft on sensing device A be shot at, if be fired upon, have the letter of corresponding interior of aircraft
Number receiver receives signal and passes to control device, and control device controls electrically operated valve, and so that aircraft is carried out without work unexpected
Decline rapidly and along with corresponding music to punish, the overall situation can be controlled in this way by having reached, and be not limited to
Front aircraft enriches enjoyment of playing, and only direction switch can just make aircraft slowly be landed, and control device makes aircraft carry out
Decline, can cause to decline rapid;It is attached with cylinder using groove B and mounting hole, then is fixed by pin, make company in this way
The place of connecing is hardly damaged, is easy for installation, is safe;The utility model is with reasonable for structure, installation is simple, level of comfort is high, warp
Good, the easy to spread advantage of Ji property.
Description of the drawings
Fig. 1 is a kind of structural schematic diagram of self-control aircraft amusement device of the utility model.
Fig. 2 is a kind of structural schematic diagram of self-control aircraft amusement device motor of the utility model.
Fig. 3 is a kind of structural schematic diagram of self-control aircraft amusement device shaft bottom of the utility model.
Fig. 4 is a kind of large arm partial structural diagram of self-control aircraft amusement device of the utility model.
Fig. 5 is a kind of structural schematic diagram of self-control aircraft amusement device aircraft of the utility model.
In figure:1, pedestal 2, motor 3, output shaft 4, boss 5, the first swivel bearing 6, shaft 7, groove
A 8, it supporting rack 9, cylinder 10, fixing end 11, large arm 12, groove B 13, mounting hole 14, aircraft 15, rises
Switch 16, track 17, sensing device A 18, laser gun 19, the second swivel bearing 20, head cover 21, induction dress drop
Set B.
Specific implementation mode
The utility model is described further below in conjunction with the accompanying drawings.
Embodiment 1
As shown in Figs. 1-5, a kind of self-control aircraft amusement device, it includes pedestal 1, and the pedestal 1 is internally provided with electricity
Machine 2 is provided with output shaft 3 on the motor 2, and boss 4, the 1 upside setting of pedestal are provided on the output shaft 3
There are the first swivel bearing 5,5 upside of the first swivel bearing to be provided with shaft 6, be provided in the middle part of 6 bottom surface of shaft
Groove A7, the boss 4 are connected with groove A7, and 6 downside of the shaft is provided with supporting rack 8, on the supporting rack 8
It is provided with cylinder 9, upside is provided with fixing end 10 in the shaft 6, is provided in the fixing end 10 outwardly extending
Large arm 11, is arranged fluted B12 and mounting hole 13 in the large arm 11, described inside the 9 connecting groove B12 of cylinder
11 end of large arm connect aircraft 14, be provided with direction switch 15, track 16 and sensing device A17, institute on the aircraft 14
16 upside of track stated is provided with laser gun 18, and the sensing device A17 is arranged in the middle part of the rear side of aircraft 14, and described turns
The upside of axis 6 is provided with the second swivel bearing 19, and 19 upside of the second swivel bearing is provided with head cover 20, on the head cover
It is provided with sensing device B21.
The utility model uses motor 1, in use, motor 1 is started to work, motor 1 drives output shaft 3 to rotate, output shaft 3
Boss 4 is driven to rotate, because boss 4 and groove A7 are combined, so shaft 6 starts to rotate, and to drive aircraft 14 to rotate, structure
Advantages of simple for ease of maintenaince and is installed;Using cylinder 9,14 raising and lowering of aircraft, the gas that cylinder 9 connects are achieved the purpose that
Electrically operated valve is provided on pipe, reached aircraft 14 decline when can voluntarily control speed, avoid aircraft 14 decline it is too quickly
Cause tourist uncomfortable;Using head cover 20, sensing device A17, sensing device B21, aircraft 14, direction switch 15, laser gun 18
With track 16, tourist oneself can control direction switch 15, then be controlled solenoid valve, be made by direction switch 15 again
Aircraft 14 achievees the effect that lifting, and head cover 20 is fixed, on the sensing device B21 and aircraft 14 being provided on head cover 20
It is provided with sensing device A17, sensing device B21 may be designed to different shapes, and to increase liking for tourist, these shapes can be with
Decoration on respective aircraft 14 is similar, these sensing device B21 with similar fitgures are exactly to represent which aircraft 14, track
Laser gun 18 on 16 can carry out position rotation, to the sensing device B21 on the head cover 20 or sensing device A17 on aircraft 14
It is shot at, if be fired upon, has the signal receiver inside corresponding aircraft 14 and receive signal and pass to control dress
It sets, control device controls electrically operated valve makes aircraft carry out rapid suddenly decline and along with corresponding music without work
To punish, the overall situation can be controlled in this way by having reached, and be not limited to front aircraft, enriched enjoyment of playing, only rise
Drop switch can just make aircraft slowly be landed, and control device makes aircraft be declined, and can cause to decline rapid;Using groove
B12 and mounting hole 13 are attached with cylinder 9, then are fixed by pin, be in this way hardly damaged junction, be easy for installation,
It is safe;The utility model has the advantages that reasonable for structure, installation is simple, level of comfort height, good economy performance, easy to spread.
Embodiment 2
A kind of self-control aircraft amusement device as shown in Figs. 1-5, it includes pedestal 1, and the pedestal 1 is internally provided with motor
2, output shaft 3 is provided on the motor 2, boss 4 is provided on the output shaft 3, and 1 upside of pedestal is provided with
First swivel bearing 5,5 upside of the first swivel bearing are provided with shaft 6, are provided in the middle part of 6 bottom surface of shaft recessed
Slot A7, the boss 4 are connected with groove A7, and 6 downside of shaft is provided with supporting rack 8, is set on the supporting rack 8
It is equipped with cylinder 9, upside is provided with fixing end 10 in the shaft 6, is provided in the fixing end 10 outwardly extending big
Arm 11, is arranged fluted B12 and mounting hole 13 in the large arm 11, described inside the 9 connecting groove B12 of cylinder
11 end of large arm connects aircraft 14, and direction switch 15, track 16 and sensing device A17 are provided on the aircraft 14, described
The upside of track 16 be provided with laser gun 18, the sensing device A17 is arranged in the middle part of the rear side of aircraft 14, the shaft
6 upsides are provided with the second swivel bearing 19, and 19 upside of the second swivel bearing is provided with head cover 20, is set on the head cover
It is equipped with sensing device B21.
In order to reach better effect, the interior of aircraft is provided with signal receiver, control device, music dress
It sets and solenoid valve, enriches the enjoyment played.
In order to reach better effect, the motor is decelerating motor, has that small, to bear overload capacity strong, right
The advantages of environmental suitability is strong, with small vibration, low noise.
In order to reach better effect, the track is curved track, substantially reduces tourist and is turned round because playing laser gun
The long caused discomfort of body.
In order to reach better effect, the groove A contour lines are rectangle and circle and are connect with boss that described is recessed
Slot B is rectangular recess, has reached junction and has been hardly damaged, good economy performance, safe advantage.
In order to reach better effect, the large arm is that pin is connect with the connection type of cylinder and fixing end, is reached
The advantages of being easily installed and dismantle.
In order to reach better effect, the sensing device being arranged on the head cover can be designed to different shapes, rise
To effect that is beautiful and causing guests to pay attention to.
The utility model uses motor 1, in use, motor 1 is started to work, motor 1 drives output shaft 3 to rotate, output shaft 3
Boss 4 is driven to rotate, because boss 4 and groove A7 are combined, so shaft 6 starts to rotate, and to drive aircraft 14 to rotate, structure
Advantages of simple for ease of maintenaince and is installed;Using cylinder 9,14 raising and lowering of aircraft, the gas that cylinder 9 connects are achieved the purpose that
Electrically operated valve is provided on pipe, reached aircraft 14 decline when can voluntarily control speed, avoid aircraft 14 decline it is too quickly
Cause tourist uncomfortable;Using head cover 20, sensing device A17, sensing device B21, aircraft 14, direction switch 15, laser gun 18
With track 16, tourist oneself can control direction switch 15, then be controlled solenoid valve, be made by direction switch 15 again
Aircraft 14 achievees the effect that lifting, and head cover 20 is fixed, on the sensing device B21 and aircraft 14 being provided on head cover 20
It is provided with sensing device A17, sensing device B21 may be designed to different shapes, and to increase liking for tourist, these shapes can be with
Decoration on respective aircraft 14 is similar, these sensing device B21 with similar fitgures are exactly to represent which aircraft 14, track
Laser gun 18 on 16 can carry out position rotation, to the sensing device B21 on the head cover 20 or sensing device A17 on aircraft 14
It is shot at, if be fired upon, has the signal receiver inside corresponding aircraft 14 and receive signal and pass to control dress
It sets, control device controls electrically operated valve makes aircraft carry out rapid suddenly decline and along with corresponding music without work
To punish, the overall situation can be controlled in this way by having reached, and be not limited to front aircraft, enriched enjoyment of playing, only rise
Drop switch can just make aircraft slowly be landed, and control device makes aircraft be declined, and can cause to decline rapid;Using groove
B12 and mounting hole 13 are attached with cylinder 9, then are fixed by pin, be in this way hardly damaged junction, be easy for installation,
It is safe;The utility model has the advantages that reasonable for structure, installation is simple, level of comfort height, good economy performance, easy to spread.
Claims (7)
1. a kind of self-control aircraft amusement device, it includes pedestal, it is characterised in that:The chassis interior is provided with motor, institute
It is provided with output shaft on the motor stated, boss is provided on the output shaft, the first rotation is provided on the upside of the pedestal
Bearing, first swivel bearing upside are provided with shaft, fluted A are arranged in the middle part of the rotating shaft bottom surface, described is convex
Platform is connected with groove A, and supporting rack is provided on the downside of the shaft, and cylinder is provided on the supporting rack, and described turns
Upside is provided with fixing end in axis, and outwardly extending large arm is provided in the fixing end, is provided in the large arm recessed
Slot B and mounting hole, inside the cylinder connecting groove B, the large arm end connects aircraft, is provided on the aircraft
Direction switch, track and sensing device A, track upside are provided with laser gun, and the sensing device is arranged in aircraft
Rear side in the middle part of, the second swivel bearing is provided on the upside of the shaft, head cover is provided on the upside of second swivel bearing,
Sensing device B is provided on the head cover.
2. a kind of self-control aircraft amusement device according to claim 1, it is characterised in that:The interior of aircraft is provided with
Signal receiver, control device, music player and solenoid valve.
3. a kind of self-control aircraft amusement device according to claim 1, it is characterised in that:The motor is the electricity that slows down
Machine.
4. a kind of self-control aircraft amusement device according to claim 1, it is characterised in that:The track is curved rail
Road.
5. a kind of self-control aircraft amusement device according to claim 1, it is characterised in that:The groove A contour lines are
Rectangle and circle are simultaneously connect with boss, and the groove B is rectangular recess.
6. a kind of self-control aircraft amusement device according to claim 1, it is characterised in that:The large arm is with cylinder and admittedly
The connection type of fixed end connects for pin.
7. a kind of self-control aircraft amusement device according to claim 1, it is characterised in that:The sensing device B can be with
It is designed to different shapes.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820141939.3U CN208031877U (en) | 2018-01-29 | 2018-01-29 | A kind of self-control aircraft amusement device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201820141939.3U CN208031877U (en) | 2018-01-29 | 2018-01-29 | A kind of self-control aircraft amusement device |
Publications (1)
Publication Number | Publication Date |
---|---|
CN208031877U true CN208031877U (en) | 2018-11-02 |
Family
ID=63954593
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201820141939.3U Expired - Fee Related CN208031877U (en) | 2018-01-29 | 2018-01-29 | A kind of self-control aircraft amusement device |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN208031877U (en) |
-
2018
- 2018-01-29 CN CN201820141939.3U patent/CN208031877U/en not_active Expired - Fee Related
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN206343330U (en) | Gardens decoration energy-saving fountain device | |
CN208031877U (en) | A kind of self-control aircraft amusement device | |
CN201168431Y (en) | Helicopter simulating recreational and training dual-purpose system | |
CN208893612U (en) | Game experiencing chair | |
CN201643661U (en) | Portable type movable laser target | |
CN206695059U (en) | A kind of liftable stage matrix lamp | |
CN208611769U (en) | The innovative emulation snowfield of one kind is walked around | |
CN210674221U (en) | Electronic arborescent track ball toy | |
CN206980105U (en) | Interesting electric slide plate toy and its remote control | |
CN207856303U (en) | A electric top with propeller | |
CN208049387U (en) | One kind blowing gas-powered toy car | |
CN206404302U (en) | Suspending gyrorotor | |
CN206508534U (en) | A kind of new big torsion width chairoplane swing | |
CN108970127A (en) | A kind of town squares children pitching amusement equipment | |
CN2329406Y (en) | Electric rotary flying saucer | |
CN205129866U (en) | But arm wobbling wedding celebration etiquette service robot | |
CN219295094U (en) | Swing type solar windmill | |
CN219091092U (en) | Movable puppet theatre structure | |
CN204671899U (en) | Novel flying toy | |
CN217430801U (en) | Double-deck aircraft of amusement equipment | |
CN204367971U (en) | Portable caravan envelope | |
CN208660326U (en) | A kind of gyro and gyrounit | |
CN217187837U (en) | Water surface rotating disk and system | |
CN202951247U (en) | Electronic toy dump truck | |
CN201308777Y (en) | Multi-layer toy windmill |
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: 20181102 Termination date: 20190129 |
|
CF01 | Termination of patent right due to non-payment of annual fee |