CN207286660U - Aircraft rides seat and aircraft of travelling - Google Patents
Aircraft rides seat and aircraft of travelling Download PDFInfo
- Publication number
- CN207286660U CN207286660U CN201721277078.3U CN201721277078U CN207286660U CN 207286660 U CN207286660 U CN 207286660U CN 201721277078 U CN201721277078 U CN 201721277078U CN 207286660 U CN207286660 U CN 207286660U
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- seat
- aircraft
- vehicle body
- body frame
- rides
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Abstract
The utility model provides a kind of aircraft riding seat and aircraft of travelling, and is related to amusement facility technical field.Aircraft riding seat includes:Car body, car body include vehicle body frame, seat and the hook nail for being connected with floating equipment, and there is vehicle body frame seat to multiply space, and seat is arranged at seat and multiplies space, and hook nail is arranged at vehicle body frame;Gear unit, gear unit include power input mechanism, transmission device and changement, and power input mechanism is used to exert a force for user, and transmission device is used to the power that user applies being transferred to changement;Propulsion unit, changement are used to the power that user applies passing to propulsion unit and aircraft is rided seat mass motion.Aircraft of travelling includes floating equipment and aircraft riding seat, and floating equipment is connected with hook nail and enables to aircraft riding seat hanging.Aircraft rides seat and aircraft of travelling enables to the people of different weight to enjoy very playing with interest, and cutting operating costs.
Description
Technical field
Amusement facility technical field is the utility model is related to, seat is rided in particular to a kind of aircraft and travels winged
Row device.
Background technology
Unpowered amusement facility be for the various amusement facilities using power supply, refer to not by it is any it is non-from
Right external force and the energy and possess the active experience type equipment of amusement facility speciality, facility.
Aerial bicycle, is a unpowered amusement facility, and many people as a child cross oneself and can fly by all free thought, can be in the air
Play.And aerial bicycle is exactly such amusement facility that trip player can be allowed to play in the air.
The too fat to move fuselage of existing facility, can only often allow thin weak person or children to operate, to adapt to adult or
The sturdy tourist of person's build plays, then need to put into higher into original meet demand.
This for consumer play experience it is unfavorable, the cost control also to the network operator of amusement facility is unfavorable.
Utility model content
The purpose of this utility model is to provide a kind of aircraft to ride seat, it disclosure satisfy that making for different weight rider
With.
Another purpose of the utility model is to provide one kind and travels aircraft, it includes above-mentioned aircraft riding
Seat, it can allow the user of different weight to enjoy the enjoyment played.
What the embodiment of the utility model was realized in:
The embodiment of the utility model provides a kind of aircraft riding seat, including:
Car body, the car body include vehicle body frame, seat and the hook nail for being connected with floating equipment, the car body frame
There is frame seat to multiply space, and the seat is arranged at the seat and multiplies space, and the hook nail is arranged at the vehicle body frame;
Gear unit, the gear unit include power input mechanism, transmission device and changement, the power input
Mechanism is used to exert a force for user, and the transmission device is used to the power that user applies being transferred to the changement, institute
It is foot pedal to state power input mechanism, and the transmission device is the chain gearing that can coordinate with the foot pedal, described
Foot pedal and the chain gearing may be contained within the vehicle body frame, and the foot pedal is located at the front of seat, and chain passes
Dynamic device includes the first chain and the second chain, and first chain is located at the under-seat, and second chain is located at institute
State seat rear;With
Propulsion unit, the changement are used to the power that user applies passing to the propulsion unit and make described
Aircraft rides seat mass motion, and the propulsion unit includes propeller and protective cover, and the propeller is arranged at the car body
The rear of frame, the protective cover cover the propeller, and the power that the changement scrunches rider passes to institute
State propeller.
In addition, the aircraft riding seat that embodiment according to the present utility model provides, can also have skill additional as follows
Art feature:
In the alternative embodiment of the utility model, the vehicle body frame includes girder, and the girder takes the shape of the letter U.
In the alternative embodiment of the utility model, the seat includes the bundling belt for protection staff safety.
In the alternative embodiment of the utility model, the aircraft riding seat further includes counterweight element, the counterweight list
Member is removable installed in the lower section of the vehicle body frame.
In the alternative embodiment of the utility model, the aircraft riding seat is used to reduce abrasion when being additionally included in ground
Pulley, the pulley is arranged at the lower section of the vehicle body frame.
In the alternative embodiment of the utility model, the aircraft riding seat includes actuation unit, the actuation unit
Including:Control stick, the control command decomposer being connected with one end of the control stick and can be by the action of the control stick point
Solution including the driving member including rudder of the first driving member and the second driving member and the mobile rudder of elevator, first transmission
Part and second driving member are separately connected with the control command decomposer, the rudder and the described first transmission
Part connects, and the elevator is connected with second driving member, and the control stick can be used in controlling the flight for user
Device rides the steering and/or lifting of seat.
In the alternative embodiment of the utility model, the rudder is arranged with the elevator in right-angled intersection, described
Rudder and the elevator are respectively provided with pivot center, the pivot center of the rudder with described turn of the elevator
It is non-intersect between shaft line.
The embodiment of the utility model provides one kind and travels aircraft, includes the flight of floating equipment and any of the above-described
Device rides seat, and the floating equipment is connected with the hook nail of aircraft riding seat and enables to the aircraft to ride
Carriage is hanging.
The beneficial effects of the utility model are:
Aircraft rides seat, and seat is mounted with vehicle body frame, can be connected by hook nail with floating equipment, with reference to
Counterweight element, after enabling to the rider of different weight to go up to the air by floating equipment, all with a stable buoyancy, with reference to
Gear unit, propulsion unit and actuation unit, rider can advance, turn and lift in the air, there is provided have very much
Interesting experience.Aircraft riding seat integral strength is secure, can ensure the safety of rider, and the structure energy of lightweight
The requirement for floating equipment is enough reduced, without completing floating using prohibitively expensive floating equipment.
Aircraft of travelling rides seat by using aircraft, and enable to the people of different weight to enjoy has interest very much
Taste is played, and due to riding the rational in infrastructure of seat, can be saved the spending in floating equipment, be cut operating costs,
It is very practical.
Brief description of the drawings
, below will be to required use in embodiment in order to illustrate more clearly of the technical solution of the utility model embodiment
Attached drawing be briefly described, it will be appreciated that the following drawings illustrate only some embodiments of the utility model, therefore should not be by
Regard the restriction to scope as, for those of ordinary skill in the art, without creative efforts, may be used also
To obtain other relevant attached drawings according to these attached drawings.
Fig. 1 is the structure diagram that the aircraft that the embodiment 1 of the utility model provides rides seat;
Fig. 2 is the structure diagram of the gear unit shown in Fig. 1;
Fig. 3 is the connection diagram of the control command decomposer of the actuation unit shown in Fig. 1;
Fig. 4 is the fundamental diagram of actuation unit;
Fig. 5 is the schematic diagram of the propulsion unit shown in Fig. 1;
Fig. 6 is the schematic diagram for the aircraft of travelling that the embodiment 2 of the utility model provides.
Icon:100- aircraft ride seat;11- vehicle body frames;112- fixed frames;13- seats;132- bundling belts;15- collection
Grommet;30- gear units;301- foot pedals;The first fluted discs of 302-;The second fluted discs of 303-;The 3rd fluted discs of 304-;The first chains of 306-
Bar;3061- tensioning wheels;The second chains of 307-;308- axis;309- rear drums;310- changements;50- propulsion units;51-
Propeller;52- protective covers;70- actuation units;71- control sticks;72- control command decomposers;The first driving members of 73-;74-
Two driving members;75- rudders;76- elevators;101- pulleys;200- travels aircraft;210- floating equipment.
Embodiment
It is new below in conjunction with this practicality to make the purpose, technical scheme and advantage of the utility model embodiment clearer
Attached drawing in type embodiment, the technical scheme in the utility model embodiment is clearly and completely described, it is clear that is retouched
The embodiment stated is the utility model part of the embodiment, instead of all the embodiments.Usually here described in attached drawing and
The component of the utility model embodiment shown can be arranged and designed with a variety of configurations.
Therefore, requirement is not intended to limit to the detailed description of the embodiment of the utility model provided in the accompanying drawings below
The scope of the utility model of protection, but it is merely representative of the selected embodiment of the utility model.Based in the utility model
Embodiment, those of ordinary skill in the art's all other embodiments obtained without creative efforts, all
Belong to the scope of the utility model protection.
It should be noted that:Similar label and letter represents similar terms in following attached drawing, therefore, once a certain Xiang Yi
It is defined, then it further need not be defined and explained in subsequent attached drawing in a attached drawing.
, it is necessary to the orientation or position relationship of the instruction such as explanation, term " on ", " under " in the description of the utility model
For based on orientation shown in the drawings or position relationship, or the utility model product using when the orientation or position usually put
Relation, is for only for ease of description the utility model and simplifies description, rather than indicates or imply that signified device or element must
There must be specific orientation, with specific azimuth configuration and operation, therefore it is not intended that limitation to the utility model.This
Outside, term " first ", " second " etc. are only used for distinguishing description, and it is not intended that instruction or hint relative importance.
In the description of the utility model, it is also necessary to which explanation, unless otherwise clearly defined and limited, term " are set
Put ", " connection " should be interpreted broadly, for example, it may be being fixedly connected or being detachably connected, or be integrally connected;Can
To be mechanical connection or be electrically connected;It can be directly connected, can also be indirectly connected by intermediary, Ke Yishi
Connection inside two elements.For the ordinary skill in the art, with concrete condition above-mentioned term can be understood at this
Concrete meaning in utility model.
In the utility model, unless otherwise clearly defined and limited, fisrt feature is on or below second feature
Can directly it be contacted including the first and second features, it is not directly to contact but pass through it that can also include the first and second features
Between other characterisation contact.Moreover, fisrt feature is on second feature, top and above include fisrt feature the
Directly over two features and oblique upper, or be merely representative of fisrt feature level height and be higher than second feature.Fisrt feature is special second
Under sign, lower section and fisrt feature included below are immediately below second feature and obliquely downward, or are merely representative of fisrt feature level
Highly it is less than second feature.
Embodiment 1
Fig. 1 to Fig. 5 is refer to, present embodiments provides a kind of aircraft riding seat 100, including:
Car body, car body include vehicle body frame 11, seat 13 and the hook nail 15 for being connected with floating equipment, vehicle body frame
11 there is seat to multiply space, and seat 13 is arranged at seat and multiplies space, and hook nail 15 is arranged at vehicle body frame 11;
Gear unit 30, gear unit 30 include power input mechanism, transmission device and changement 310, power input
Mechanism is used to exert a force for user, and transmission device is used to the power that user applies being transferred to changement 310;With
Propulsion unit 50, changement 310 are used to the power that user applies passing to propulsion unit 50 and make flight
Device rides 100 mass motion of seat.
Specifically, power input mechanism is foot pedal 301, transmission device passes for the chain that can coordinate with foot pedal 301
Dynamic device.
Detailed, gear unit 30 includes the first fluted disc 302, the second fluted disc 303, the 3rd fluted disc 304 and the 4th fluted disc, chain
Bar transmission device includes the first chain 306 and the second chain 307.Foot pedal 301 is connected with the first fluted disc 302 by axis 308,
Scrunching foot pedal 301 can drive the first fluted disc 302 to rotate.
Second fluted disc 303 and the 3rd fluted disc 304 are coaxially connected by rear drum 309, and the first chain 306 is set around the first tooth
302 and second fluted disc 303 of disk simultaneously adjusts tensioning degree by tensioning wheel 3061.
Second fluted disc 303 drives the 3rd fluted disc 304 to rotate, and the 3rd fluted disc 304 is passed by the second chain 307 and the 4th fluted disc
Dynamic connection, power is transferred to changement 310 by the 4th fluted disc, and is outputed power by changement 310.4th fluted disc in figure
At 310 back side of changement, explain herein not separately shown.
Vehicle body frame 11 includes girder, and girder takes the shape of the letter U.The material selection of car body entirety uses 7075 aviation aluminum pipes, is protecting
Also make overall quality slim and graceful while hindering enough intensity.
Seat 13 includes the bundling belt 132 for protection staff safety.Bundling belt 132 with reference to binding side during bungee jumping
Formula, uniform force, can bear larger tensile impact and reduce human body discomfort.
Aircraft riding seat 100 further includes counterweight element, and counterweight element is removable installed in the lower section of vehicle body frame 11.
The lower section of vehicle body frame 11 has the fixed frame 112 being used for counterweight element connection, and the quantity of counterweight element is multiple, such as dumbbell
Discus generally have different weight, can be screwed on fixed frame 112, be adjusted with weight according to different riding personnel
Load.
For reducing the pulley 101 worn when aircraft riding seat 100 is additionally included in ground, pulley 101 is arranged at car body
The lower section of frame 11.
Aircraft riding seat 100 includes actuation unit 70, and actuation unit 70 includes:Control stick 71, one with control stick 71
Hold the control command decomposer 72 of connection and the movement decomposition of control stick 71 including the first driving member 73 and second can be driven
The driving member including rudder 75 of part 74 and the mobile rudder of elevator 76, the first driving member 73 and the second driving member 74 are only respectively
On the spot it is connected with control command decomposer 72, rudder 75 is connected with the first driving member 73,76 and second driving member 74 of elevator
Connection, control stick 71 can be used in controlling the steering and/or lifting of aircraft riding seat 100 for user.
Control stick 71 is arranged at the front of seat 13, and when user manipulates, control stick 71 is located between the both legs of user
Position.
Rudder 75 arranges that rudder 75 and elevator 76 are respectively provided with pivot center with elevator 76 in right-angled intersection, side
Pivot center to rudder 75 and between the pivot center of elevator 76 it is non-intersect.
Propulsion unit 50 includes propeller 51 and protective cover 52, and propeller 51 is arranged at the rear of vehicle body frame 11, protection
Cover 52 covers propeller 51.
Propeller 51 can be double bladed paddle or three leaf paddles, and paddle footpath is 1m, and weight 1.3kg, rotating speed 600r/min, is adopted
Made of carbon fibre material, allomeric function is complete and quality is slim and graceful.The power that changement 310 scrunches rider passes to spiral shell
Paddle 51 is revolved, and 51 blade of propeller is rotated, so that whole aircraft riding seat 100 moves.
The principle of the present embodiment is:
Whole aircraft rides seat 100 under conditions of corresponding structure design, its light quality, seat is rided by aircraft
100 when applying to floating equipment, can be connected by hook nail 15 with floating equipment, the slim and graceful quality of aircraft riding seat 100
Its floating is enabled to be more prone to.
Vehicle body frame 11 is overall small with the contact surface of wind, when propulsion unit 50 promotes, windage can be reduced, easy to transport
It is dynamic.More installation spaces are also provided at the same time, are allowed some leeway to improve and optimizate in the future.
And the structure of U-shaped girder causes entirety in the case where intensity is secure, also a space is drawn for rider's circle
Abundant seat multiplies space, this just meets the riding demand of the people of different building shape, particularly, the aircraft riding seat of the present embodiment
100 disclosure satisfy that the rider within weight 100kg uses.
Before floating, the weight of counterweight element according to the weight of rider, can also be adjusted so that, can during floating
The net buoyancy of 1-2kg is provided with reference to floating equipment for rider.And during rider's heavier-weight, counterweight element can also be dismantled
Fall, to maintain a fixed buoyancy.
The aircraft riding seat 100 of the present embodiment, on the basis of the enough seating spaces of rider have been ensured, passes through conjunction
The structure design of reason so that the structural strength of whole car body is guaranteed, has good support effect, in use, the weight of lightweight
Be more conducive to floating, relatively low windage also allow for propulsion unit 50 promote and the control of actuation unit 70 turn to either lifting or
It is common to adjust.The counterweight element for different weight of arranging in pairs or groups, can ensure that the rider of different weight can smoothly floating and holding one
A metastable buoyancy.
Embodiment 2
Fig. 6 is refer to, one kind is present embodiments provided and travels in aircraft 200, including floating equipment 210 and embodiment 1
Aircraft riding seat 100, the hook nail 15 that floating equipment 210 and aircraft ride seat 100 is connected and enables to aircraft
It is hanging to ride seat 100.
Floating equipment 210 is balloon in the present embodiment.
Seat 100 is rided by using the aircraft in embodiment 1, aircraft 200 of travelling enables to making for different weight
User's floating, user can be ridden by scrunching foot pedal 301 and control control stick 71 in the aerial of certain altitude, and
It can turn to or lift.There is interest very much.
In conclusion the aircraft riding seat 100 of the utility model, is mounted with seat 13 on vehicle body frame 11, can
It is connected by hook nail 15 with floating equipment 210, with reference to counterweight element, enables to the rider of different weight to be set by floating
After standby 210 lift-off, all with a stable buoyancy, with reference to gear unit 30, propulsion unit 50 and actuation unit 70, riding
Person can advance, turn and lift in the air, there is provided have very much interesting experience.Aircraft riding seat 100 is overall strong
Spend secure, can ensure the safety of rider, and the structure of lightweight can reduce the requirement for floating equipment 210, no
Floating is completed with using prohibitively expensive floating equipment 210.
Aircraft 200 of travelling rides seat 100 by using aircraft, and enabling to the people of different weight can enjoy very
Play with interesting, and due to riding the rational in infrastructure of seat, the spending in floating equipment 210 can be saved, reduce
Operation cost, it is very practical.
The above descriptions are merely preferred embodiments of the present invention, is not intended to limit the present invention, for this
For the technical staff in field, various modifications and changes may be made to the present invention.It is all in the spirit and principles of the utility model
Within, any modification, equivalent replacement, improvement and so on, should be included within the scope of protection of this utility model.
Claims (8)
1. a kind of aircraft rides seat, it is characterised in that including:
Car body, the car body include vehicle body frame, seat and the hook nail for being connected with floating equipment, the vehicle body frame tool
There is seat to multiply space, the seat is arranged at the seat and multiplies space, and the hook nail is arranged at the vehicle body frame;
Gear unit, the gear unit include power input mechanism, transmission device and changement, the power input mechanism
For exerting a force for user, the transmission device is used to the power that user applies being transferred to the changement, described dynamic
Power input mechanism is foot pedal, and the transmission device is the chain gearing that can coordinate with the foot pedal, described foot-operated
Plate and the chain gearing may be contained within the vehicle body frame, and the foot pedal is located at the front of seat, chain drive dress
Put including the first chain and the second chain, first chain is located at the under-seat, and second chain is located at the seat
Chair rear;With
Propulsion unit, the changement are used to the power that user applies passing to the propulsion unit and make the flight
Device rides seat mass motion, and the propulsion unit includes propeller and protective cover, and the propeller is arranged at the vehicle body frame
Rear, the protective cover covers the propeller, and the power that the changement scrunches rider passes to the spiral shell
Revolve paddle.
2. aircraft according to claim 1 rides seat, it is characterised in that the vehicle body frame includes girder, the master
Beam takes the shape of the letter U.
3. aircraft according to claim 1 rides seat, it is characterised in that the seat includes being used for protection staff safety
Bundling belt.
4. aircraft according to claim 1 rides seat, it is characterised in that the aircraft riding seat further includes counterweight list
Member, the counterweight element are removable installed in the lower section of the vehicle body frame.
5. aircraft according to claim 1 rides seat, it is characterised in that the aircraft riding seat is additionally included in ground
When for reducing the pulley of abrasion, the pulley is arranged at the lower section of the vehicle body frame.
6. aircraft according to claim 1 rides seat, it is characterised in that the aircraft riding seat includes manipulating single
Member, the actuation unit include:Control stick, the control command decomposer being connected with one end of the control stick and can will described in
The movement of the driving member including rudder and elevator of the movement decomposition of control stick including the first driving member and the second driving member
Rudder, first driving member and second driving member are separately connected with the control command decomposer, the direction
Rudder is connected with first driving member, and the elevator is connected with second driving member, and the control stick can be used in for making
User controls the steering and/or lifting of the aircraft riding seat.
7. aircraft according to claim 6 rides seat, it is characterised in that the rudder and the elevator are in cross
Arranged crosswise, the rudder and the elevator are respectively provided with pivot center, the pivot center of the rudder with it is described
It is non-intersect between the pivot center of elevator.
The aircraft 8. one kind is travelled, it is characterised in that ridden including floating equipment and claim 1-7 any one of them aircraft
Carriage, the floating equipment are connected with the hook nail of aircraft riding seat and enable to the aircraft riding seat
Vacantly.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721277078.3U CN207286660U (en) | 2017-09-28 | 2017-09-28 | Aircraft rides seat and aircraft of travelling |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201721277078.3U CN207286660U (en) | 2017-09-28 | 2017-09-28 | Aircraft rides seat and aircraft of travelling |
Publications (1)
Publication Number | Publication Date |
---|---|
CN207286660U true CN207286660U (en) | 2018-05-01 |
Family
ID=62440598
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201721277078.3U Active CN207286660U (en) | 2017-09-28 | 2017-09-28 | Aircraft rides seat and aircraft of travelling |
Country Status (1)
Country | Link |
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CN (1) | CN207286660U (en) |
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2017
- 2017-09-28 CN CN201721277078.3U patent/CN207286660U/en active Active
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