CN207286660U - Aircraft rides seat and aircraft of travelling - Google Patents

Aircraft rides seat and aircraft of travelling Download PDF

Info

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
Authority
CN
China
Prior art keywords
seat
aircraft
vehicle body
body frame
rides
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.)
Active
Application number
CN201721277078.3U
Other languages
Chinese (zh)
Inventor
苏小东
赖贞华
鲍志明
梁杰
杨军
张凡
王龙
李辉
徐雷
舒欣
罗贤斌
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
China Special Vehicle Research Institute
Original Assignee
China Special Vehicle Research Institute
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by China Special Vehicle Research Institute filed Critical China Special Vehicle Research Institute
Priority to CN201721277078.3U priority Critical patent/CN207286660U/en
Application granted granted Critical
Publication of CN207286660U publication Critical patent/CN207286660U/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

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

Aircraft rides seat and aircraft of travelling
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.
CN201721277078.3U 2017-09-28 2017-09-28 Aircraft rides seat and aircraft of travelling Active CN207286660U (en)

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
CN (1) CN207286660U (en)

Similar Documents

Publication Publication Date Title
TW479038B (en) Aircraft with rotary wings
CN101033005B (en) Suspension type gliding wing manpower flight driving device and ground surface simulated training rack for the same
TWM393460U (en) Improved kick scooter
CN104485034B (en) The wing fills aircraft simulation device
CN106994874A (en) Suspended and promoted and the dual-purpose novel intelligent walking-replacing tool of ground roll-out based on wind-force
CN207286660U (en) Aircraft rides seat and aircraft of travelling
CN1349907A (en) Three similar kinds of flyer and their orbit facilities
CN203767057U (en) Screw ship driven by elliptical machine
CN101670889A (en) Land, water and air human-power vertical lifting air vehicle
JPH09508836A (en) Steerable swing device
CN202087051U (en) Remote control capable of being operated by one hand and toy
US8979660B2 (en) Helicopter amusement apparatus
CN205574286U (en) Wing oil electricity that verts thoughtlessly moves aircraft
CN102160933B (en) Rotary-tower game device with flight chambers arranged in circular matrix
CN102417035A (en) Coaxial helicopter capable of controlling flying speed change completely by buttons
CN109731346B (en) Safe seesaw of variable speed
CN201338727Y (en) Power aircraft with delta wing
CN207187090U (en) Travel aircraft and floating type is ridden aircraft
KR20230036937A (en) Buoyancy aircraft using the power of pedals
US1965039A (en) Amusement device
CN204352545U (en) A kind of game machine wave ship structure
CN214465715U (en) Manual deceleration braking device of monorail tackle
CN220834092U (en) Universal game simulator
CN210278239U (en) Air assault recreational machine
CN207187091U (en) Aircraft control system and aircraft of travelling

Legal Events

Date Code Title Description
GR01 Patent grant
GR01 Patent grant