CN207187090U - Travel aircraft and floating type is ridden aircraft - Google Patents

Abstract

The utility model provides that one kind travels aircraft and floating type is ridden aircraft, is related to recreation facility technical field.Aircraft of travelling includes：Double-air sac structure；Aircraft rides seat, and aircraft riding seat passes through the double-air sac structure floating after inflation；Aircraft control system, aircraft control system are installed on aircraft riding seat, for controlling aircraft riding seat to turn to and/or lift；Aircraft security component, the inner and outer air pressure and reply emergency of double-air sac structure can be balanced.Floating type aircraft of riding includes ground tackle, fixture and aircraft of travelling, the circumferential uniformly connection of the first floating air bag of one end of multiple ground tackles along aircraft of travelling, and the other end is connected the aircraft disengaging that prevents from travelling with fixture and travelled region.Travel aircraft and floating type aircraft of riding provides a kind of interesting recreation facility of novelty for consumer, very with intention, meet the higher and higher entertainment requirements of people, suit the actual demand of network operator again.

Description

Travel aircraft and floating type is ridden aircraft

Technical field

Recreation facility technical field is the utility model is related to, aircraft is travelled in particular to one kind and floating type is ridden Row aircraft.

Background technology

Unpowered recreation facility be for the various recreation 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 recreation facility speciality, facility.

Aerial bicycle, is a unpowered recreation 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 recreation facility that trip player can be allowed to be played in the air.

Simply in the case where nowadays quality of the life is become better and better, consumer for recreation facility demand than ever more Greatly, also more required for the novelty of recreation facility.

Therefore, it is necessary to which the designer of recreation facility constantly weeds out the old and bring forth the new, to adapt to consumer demand so that consumer's energy Enough have fun happy and safe.

Utility model content

The purpose of this utility model is to provide one kind and travelled aircraft, and it can provide a kind of brand-new trip for consumer Happy experience.

Another purpose of the present utility model is to provide a kind of floating type and ridden aircraft, and it can be more Side provides brand-new amusement experience for consumer.

What embodiment of the present utility model was realized in：

Embodiment of the present utility model provides one kind and travelled aircraft, including：

Double-air sac structure, the double-air sac structure include the first floating air bag and the second floating air bag, second floating Air bag is connected with the first floating air bag and positioned at the inside of the first floating air bag；

Aircraft rides seat, and the aircraft riding seat includes car body, gear unit and propulsion unit, and the car body is used for User is carried, the gear unit is used to the power that user applies passing to the propulsion unit and makes the aircraft Seat mass motion is rided, the aircraft riding seat passes through the double-air sac structure floating after inflation；

Aircraft control system, the aircraft control system include control stick, driving member and mobile rudder, the aircraft Steerable system is installed on the car body, and the control stick is used to the active force that user applies being transferred to by the driving member The mobile rudder, mobile rudder aircraft riding seat according to the direction controlling of active force turns to and/or lifting；With

Aircraft security component, the aircraft security component includes safety valve, vent valve and handle of deflating, the safety Valve is arranged at the second floating air bag and can balance the inner and outer air pressure of the first floating air bag, and the vent valve is arranged at The first floating air bag, described one end for deflating handle are connected with the vent valve, and other end extends to the aircraft Seat is rided, when pullling the deflation handle, the vent valve is opened and causes the first floating air bag deflation.

In addition, the aircraft of travelling provided according to embodiment of the present utility model, can also have technology additional as follows Feature：

In alternative embodiment of the present utility model, the car body includes vehicle body frame, seat and hook nail, the car body There is framework seat to multiply space, and the seat is arranged at the seat and multiplies space, and the hook nail is arranged at the top of the vehicle body frame Portion, the first floating air bag are connected with the hook nail.

In alternative embodiment of the present utility model, the vehicle body frame includes girder, and the girder takes the shape of the letter U, the collection Grommet is arranged at the girder.

In alternative embodiment of the present utility model, the gear unit includes power input mechanism, transmission device and changed To mechanism, the power input mechanism is used to exert a force for user, and the power that the transmission device is used to apply user passes It is handed to the changement.

In alternative embodiment of the present utility model, the power input mechanism is pedal, and the transmission device is energy Enough chain gearings coordinated with the pedal.

In alternative embodiment of the present utility model, the aircraft control system includes control command decomposer, described Driving member includes the first driving member and the second driving member, and the mobile rudder includes rudder and elevator, the control command point Solution device includes command input, the first instruction output end and the second instruction output end, the command input and the control stick Connection, first instruction output end are connected with first driving member, second instruction output end and the described second transmission Part connects；

When the control stick shakes to the left or to the right, first instruction output end is by first driving member to institute State the instruction that rudder transmission is swung to the left or to the right；

When the control stick shakes forward or backward, second instruction output end is by second driving member to institute State the instruction that elevator transmission is downward or is swung up.

In alternative embodiment of the present 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.

In alternative embodiment of the present utility model, the aircraft of travelling also includes folding and unfolding capstan arrangement, the folding and unfolding Capstan arrangement includes capstan winch and protection is restricted, and the capstan winch can protect rope described in folding and unfolding, and the protection rope is connected with the car body.

In alternative embodiment of the present utility model, the aircraft of travelling also includes filling air-extractor, described to fill pumping Equipment includes filling exhaust pipe, it is described fill exhaust pipe include being used for take out flexible pipe that inflator is connected, for double bolloon knot The fast-assembling gas tube and the adapter for making the flexible pipe be connected with the fast-assembling gas tube of structure connection.

Embodiment of the present utility model provides a kind of floating type and ridden aircraft, including ground tackle, fixture and on The aircraft of travelling any one of stated, the quantity of the ground tackle are multiple, and one end of multiple ground tackles is along the trip The circumferential uniformly connection of the first floating air bag of happy aircraft, the other end and the fixture of multiple ground tackles Connection, the fixture are used to prevent the aircraft of travelling from departing from region of travelling.

The beneficial effects of the utility model are：

Aircraft travel by meticulous design, provides a kind of interesting recreation facility of novelty for consumer, meets people Higher and higher entertainment requirements, masses can have fun freely, at the same have again safety it is supporting, ensure consumer safety, Rational design allow the operation cost of whole set of installation can also be well controlled, very with intention and suit consumption Person and the actual demand of network operator.Floating type aircraft of riding then allows the travel operation place of aircraft to be extended, Neng Gou More places provide the service of travelling for consumer.

Brief description of the drawings

, below will be to required use in embodiment in order to illustrate more clearly of the technical scheme of the utility model embodiment Accompanying drawing be briefly described, it will be appreciated that the following drawings illustrate only some embodiments of the present utility model, therefore should not be by Regard the restriction to scope as, for those of ordinary skill in the art, on the premise of not paying creative work, may be used also To obtain other related accompanying drawings according to these accompanying drawings.

Fig. 1 is the structural representation for the aircraft of travelling that embodiment 1 of the present utility model provides；

Fig. 2 is the structural representation of the aircraft riding seat shown in Fig. 1；

Fig. 3 is the structural representation of gear unit；

The connection diagram of the control command decomposer of Fig. 4 steerable systems；

Fig. 5 is the layout drawing of steerable system；

Fig. 6 is the schematic diagram of the rudder shown in Fig. 5；

Fig. 7 is the schematic diagram of the elevator shown in Fig. 5；

Fig. 8 is the schematic diagram of propulsion unit；

Fig. 9 is the structural representation of vent valve；

Figure 10 is the structural representation of Fig. 9 vent valve for eliminating cover lid；

Figure 11 is the structural representation at another visual angle of the vent valve shown in Fig. 9；

Figure 12 is the schematic diagram of manometric module；

Figure 13 is the schematic diagram of folding and unfolding capstan arrangement；

Figure 14 is the structural representation for filling exhaust pipe；

Figure 15 is to fill exhaust pipe and helium storage device and air bag connection diagram；

Figure 16 is that the floating type that embodiment 2 of the present utility model provides is ridden the schematic diagram of aircraft.

Icon：100- travels aircraft；10- the first floating air bags；11- the second floating air bags；30- aircraft ride seat； 312- vehicle body frames；314- seats；316- hook nails；33- gear units；3301- pedals；The fluted discs of 3302- first；3303- Second fluted disc；The fluted discs of 3304- the 3rd；The chains of 3306- first；33061- tensioning wheels；The chains of 3307- second；3308- axis； 3309- rear drums；3310- changements；35- propulsion units；352- propellers；354- protective covers；37- fixed mounts；50- flies Device steerable system；51- control sticks；The driving members of 530- first；The driving members of 531- second；55- moves rudder；550- rudders；551- Elevator；57- control command decomposers；70- aircraft security components；71- safety valves；73- vent valves；731- pressing plates；732- Bonnet；7321- valve plugs；733- first structure framves；7331- tie points；734- cover cylinders；735- cover lids；The structure-steel framings of 736- second； 75-, which deflates, to shake hands；77- manometric modules；771- pressure measuring tie-ins；772- pipelines；773- pressure gauges；80- folding and unfolding capstan arrangements；81- Fill exhaust pipe；812- flexible pipes；814- fast-assembling gas tubes；816- adapters；200- floating types are ridden aircraft；210- anchoring ropes Tool；220- fixtures.

Embodiment

It is new below in conjunction with this practicality to make the purpose, technical scheme and advantage of the utility model embodiment clearer Accompanying drawing in type embodiment, the technical scheme in the embodiment of the utility model is clearly and completely described, it is clear that is retouched The embodiment stated is the utility model part of the embodiment, rather than whole embodiments.Generally here described in accompanying drawing and The component of the utility model embodiment shown can be configured to arrange and design with a variety of.

Therefore, the detailed description of the embodiment of the present utility model to providing in the accompanying drawings is not intended to limit requirement below The scope of the utility model of protection, but it is merely representative of selected embodiment of the present utility model.Based in the utility model Embodiment, the every other embodiment that those of ordinary skill in the art are obtained under the premise of creative work is not made, all Belong to the scope of the utility model protection.

It should be noted that：Similar label and letter represents similar terms in following accompanying drawing, therefore, once a certain Xiang Yi It is defined, then it further need not be defined and explained in subsequent accompanying drawing in individual accompanying drawing.

, it is necessary to explanation, the orientation or position relationship of the instruction such as term " interior ", " outer " in description of the present 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, it 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 to limitation of the present 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 description of the present 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 electrical connection；Can be joined directly together, can also be indirectly connected by intermediary, Ke Yishi The connection of two element internals.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.

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 Figure 15 is refer to, one kind is present embodiments provided and travels aircraft 100, including：

Double-air sac structure, double-air sac structure include the first floating air bag 10 and the second floating air bag 11, the second floating air bag 11 are connected with the first floating air bag 10 and positioned at the inside of the first floating air bag 10；

Aircraft rides seat 30, and aircraft riding seat 30 includes car body, gear unit 33 and propulsion unit 35, and car body is used for User is carried, gear unit 33 is used to the power that user applies passing to propulsion unit 35 and aircraft is rided seat 30 Mass motion, aircraft riding seat 30 pass through the double-air sac structure floating after inflation；

Aircraft control system 50, aircraft control system 50 include control stick 51, driving member and mobile rudder 55, aircraft Steerable system 50 is installed on car body, and control stick 51 is used to the active force that user applies being transferred to mobile rudder by driving member 55, mobile rudder 55 rides seat 30 according to the direction controlling aircraft of active force and turns to and/or lift；With

Aircraft security component 70, aircraft security component 70 includes safety valve 71, vent valve 73 and handle 75 of deflating, peace Full valve 71 is arranged at the second floating air bag 11 and can balance the inner and outer air pressure of the first floating air bag 10, and vent valve 73 is arranged at One floating air bag 10, the one end for handle 75 of deflating are connected with vent valve 73, and other end extends to aircraft riding seat 30, pulls During deflation handle 75, vent valve 73 is opened and so that the first floating air bag 10 is deflated.

Specifically, the first floating air bag 10 selected by the present embodiment is 200m full of the volume after gas³, the first floating gas The surface area of capsule 10 is 165.6 ㎡.A diameter of 7260mm of first floating air bag 10.

It is 20m that the second floating air bag 11 selected by the present embodiment, which is full of the volume after gas,³, the table of the second floating air bag 11 Area is 23.88 ㎡.

The flying height relative to ground of first floating air bag 10 and the second floating air bag 11 is not more than 50m, it is general and Speech uses height above sea level, it is proposed that is 0-600m.

Car body includes vehicle body frame 312, seat 314 and hook nail 316, and there is vehicle body frame 312 seat to multiply space, seat 314, which are arranged at seat, multiplies space, and hook nail 316 is arranged at the top of vehicle body frame 312, the first floating air bag 10 and hook nail 316 Connection, is so advantageous to concentrfated load transmission.

Vehicle body frame 312 includes girder, and girder takes the shape of the letter U, and hook nail 316 is arranged at girder, and seat 314 includes being used to protect The bundling belt of personal security.Bundling belt with reference to binding mode during bungee jumping, uniform force, larger tensile impact can be born and It is uncomfortable to reduce human body.

Gear unit 33 includes power input mechanism, transmission device and changement 3310, and power input mechanism is used to supply User exerts a force, and transmission device is used to the power that user applies being transferred to changement 3310.

Power input mechanism is pedal 3301, and transmission device fills for the chain drive that can coordinate with pedal 3301 Put.

Detailed, gear unit 33 includes the first fluted disc 3302, the second fluted disc 3303, the 3rd fluted disc 3304 and the 4th tooth Disk, chain gearing include the first chain 3306 and the second chain 3307.The fluted disc 3302 of pedal 3301 and first is in Axle 3308 connects, and scrunching pedal 3301 can drive the first fluted disc 3302 to rotate.

Second fluted disc 3303 and the 3rd fluted disc 3304 are coaxially connected by rear drum 3309, and the first chain 3306 is set around One fluted disc 3302 and the second fluted disc 3303 simultaneously adjust tensioning degree by tensioning wheel 33061.

Second fluted disc 3303 drives the 3rd fluted disc 3304 to rotate, and the 3rd fluted disc 3304 passes through the second chain 3307 and the 4th tooth Disk is connected, and power is transferred to changement 3310 by the 4th fluted disc, and outputs power to propulsion by changement 3310 Unit 35.The 4th fluted disc is explained not separately shown at the back side of changement 3310 herein in figure.

Propulsion unit 35 includes propeller 352 and protective cover 354, and propeller 352 is arranged at the rear of vehicle body frame 312, Protective cover 354 covers propeller 352.

Propeller 352 can be double bladed paddle or three leaf oars, and oar footpath is 1m, weight 1.3kg, rotating speed 600r/min, Made using carbon fibre material, allomeric function is complete and quality is slim and graceful.The power transmission that changement 3310 scrunches rider To propeller 352, and the blade of propeller 352 is rotated, so that whole aircraft riding seat 30 moves.

Aircraft control system 50 includes control command decomposer 57, and driving member includes the first driving member 530 and second and passed Moving part 531, mobile rudder 55 include rudder 550 and elevator 551, and control command decomposer 57 includes command input, first Instruction output end and the second instruction output end, command input are connected with control stick 51, the first instruction output end and the first transmission Part 530 is connected, and the second instruction output end is connected with the second driving member 531.

Driving member, as power transmission carrier, forms flexible axle, one end of flexible axle passes through ball angle joint and manipulation using push-and-pull cable wire Command Resolution device 57 is connected, and other end is connected by pitching ear with mobile rudder 55.Push-and-pull cable wire why is selected, allows for shifting The rudder face torque of dynamic rudder 55 is smaller, and the strength and toughness of push-and-pull cable wire is enough the transmission for completing control command.Ball angle joint and fork Ear can refer to prior art, and here is omitted.

When control stick 51 shakes to the left or to the right, the first instruction output end is by the first driving member 530 to rudder 550 Transmit the instruction swung to the left or to the right；

When control stick 51 shakes forward or backward, the second instruction output end is by the second driving member 531 to elevator 551 Transmit the instruction downwards or being swung up.

Rudder 550 arranges that rudder 550 and elevator 551 are respectively provided with rotary shaft with elevator 551 in right-angled intersection Line, it is non-intersect between the pivot center of rudder 550 and the pivot center of elevator 551.

By manipulation bar 51, change the rudder face angle of rudder 550 and elevator 551, user can be existed Aerial to complete rise/fall/left/right turn/upper oblique turn/multiple actions such as oblique turn, operation is flexible and changeable, allows user half The aerial experience for having more interests, it is no longer dull as common aerial bicycle.

For for safing aircraft security component 70, vent valve 73 includes pressing plate 731, bonnet 732, is close in advance Fitting, first structure frame 733 and cover body, pressing plate 731 are used to be connected with the first floating air bag 10, and the middle part of pressing plate 731, which has, to be used In the through hole of exhaust, bonnet 732 is connected by pre- clamping joint with pressing plate 731 and with the pretightning force for closing through hole, and first Structure-steel framing 733 is arranged at the side inside the first floating air bag 10 of pressing plate 731, and cover body has the wind that supplied gas flows Hole, cover body are connected with pressing plate 731 and cover first structure frame 733.

Wherein, cover body includes cover cylinder 734 and cover lid 735, and cover lid 735 is detachably connected with cover cylinder 734.In the present embodiment In, pre- clamping joint is mainly spring, and one end of spring is connected with bonnet 732, and one end is connected with first structure frame 733, so as to Pretightning force is provided, first structure frame 733 there are three tie points 7331, in order to install three springs, both provides pretightning force, and can There is a relatively good stability, avoid bonnet 732 from being released when draught head need not be adjusted.It should be noted that to finish Structure is apparent easily to be distinguished, it is illustrated that in concealed spring.

Vent valve 73 also includes the second structure-steel framing 736, and the second structure-steel framing 736 is arranged at the other side of pressing plate 731.Second Structure-steel framing 736 is made up of three support arms, and three support arms are centrosymmetric distribution, and converge at centre.

Second structure-steel framing 736 offers the hole worn for handle 75 of deflating, and bonnet 732 has valve plug 7321, deflates Handle 75 wears hole and is connected with valve plug 7321.

By the second structure-steel framing 736, when handle 75 of deflating pulls valve plug 7321, the direction of active force can be with bonnet 732 opening direction is consistent, ensures that handle 75 of deflating is capable of the bonnet 732 of the vent valve 73 of very first time pulling when needed, real Now deflate operation.

Safety valve 71 is consistent with the structure of vent valve 73, and the difference of safety valve 71 and vent valve 73 is：Pre- clamping joint Pretightning force size.

The threshold value of safety valve 71 is the size of the pretightning force of pre- clamping joint, when the inner and outer air pressure difference of air bag is excessive, The pretightning force of pre- clamping joint bonnet 732 and then is squeezed by pressure by the counteracted by pressure of air pressure.So that the gas in air bag is released Put, until pretightning force again be more than draught head it is excessive caused by pressure.

There are safety valve 71, vent valve 73 and deflating as handle 75 on the basis of security component, in order that must travel Aircraft 100 preferably provides entertainment service for user, and aircraft security component 70 also includes manometric module 77, predominantly Face support personnel provides the means of monitoring air bag pressure difference.

Manometric module 77 includes pressure measuring tie-in 771, pipeline 772 and pressure gauge 773, and pressure gauge 773 is by pipeline 772 with surveying Crimp head 771 connects, and pressure measuring tie-in 771 is used for and the inflatable interface of the first floating air bag 10 or filling for the second floating air bag 11 Gas interface connects.

Pressure measuring tie-in 771 includes seal head and turriform joint, and seal head is used to be connected with gas-charging connection, and turriform joint is used for It is connected with pipeline 772.Particularly, the inflatable interface on the second floating air bag 11 or the first floating air bag 10 has for sealing Closure, the seal head of pressure measuring tie-in 771 is consistent with the structure of closure, this can just ensure carry out pressure measurement operation when, gas The gas in intracapsular portion will not leak in detection process, both ensured the accuracy of testing result, turn avoid inside air bag Gas leakage is excessive and causes the loss of the light gas (such as helium) for playing buoyance lift effect.

In order that the people of different weight can steadily play, aircraft riding seat 30 also includes counterweight element, counterweight element It is removable installed in the lower section of vehicle body frame 312.The lower section of vehicle body frame 312 has the fixed mount being used for counterweight element connection 37, the quantity of counterweight element is multiple, has different weight as the discus of dumbbell, can be screwed on fixed mount 37, Load is adjusted with body weight according to different riding personnel.

For reducing the pulley worn when aircraft riding seat 30 is additionally included in ground, pulley is arranged at vehicle body frame 312 Lower section, it is front and rear as the wheel of ordinary bicycle to have.

In order that aircraft 100 of entirely travelling can preferably be run, daily operation is ensured, is provided with following guarantee Measure.

Aircraft 100 of travelling also includes folding and unfolding capstan arrangement 80, and folding and unfolding capstan arrangement 80 includes capstan winch and protection is restricted, capstan winch Can folding and unfolding protection rope, protection rope be connected with car body.

Specifically, capstan winch and protection rope are the flight safeties in order to ensure aerial bicycle in certain space region, to it Car body and balloon can be retracted rapidly when recovery and generation special circumstances.

Aircraft 100 of travelling also includes filling air-extractor, and filling air-extractor includes filling exhaust pipe 81, fills exhaust pipe 81 Including for taking out flexible pipe 812 that inflator is connected, for the fast-assembling gas tube 814 that is connected with double-air sac structure and soft for making The adapter 816 that pipe 812 is connected with fast-assembling gas tube 814.

Take out inflator be used for run during supplement in the second floating air bag 11 air and remove receive after the first floating air bag 10 vacuumize, and are connected by filling exhaust pipe 81 with inflatable interface on two air bags.

, can be by packing case come packed and transported, such as chest dress double-air sac structure, a folding and unfolding capstan arrangement after removing receipts 80 and fill air-extractor etc., work accessory used in a chest dress counterweight element and some installing/dismountings etc..

The principle of the present embodiment is：

There can be a different amusement experiences to allow consumer, the utility model provides one kind and travelled aircraft 100.

In use, according to the body weight of user, the counterweight of counterweight element is carried out, 1-2kg net buoyancy is provided for user. User takes after seat 314 and carries out safe fix by bundling belt.

By control folding and unfolding capstan arrangement 80 can user with the slow buoyance lift of double-air sac structure, when floating to one Determine after height then no longer release guard rope, and it is constant make it that protection rope is fixed on a length.

After user's lift-off, pedal 3301 can be scrunched, power is transferred to propeller 352 by gear unit 33. The rotation of propeller 352 causes double-air sac structure to be travelled forward together with aircraft riding seat 30.

User can according to the emerging institute of oneself to, manipulate the travel direction of control stick 51 conversion, roam leisurely in the air, or Rise or drop, turn or row, by it is a kind of it is fresh it is interesting in a manner of, allow user enjoy travel the time.

Double-air sac structure can face the threat of the violent temperature change of comparison after certain altitude is raised to, and for example sunlight is prominent So it is exposed to the sun.At this moment the pressure inside and outside the first floating air bag 10 will change.

Pressure change is run into more than after certain value, in general air bag can even be burst because the pressure of inside is excessive, This is extremely disadvantageous to personal security.Therefore, the effect of the safety valve 71 of the present embodiment is just quite important.

When causing the internal pressure of the first floating air bag 10 to raise due to the temperature difference, the bonnet 732 of safety valve 71 can quilt Pressure top inside first floating air bag 10 is opened, and discharges some gases inside the second floating air bag 11, to reach interior external pressure Power difference is returned to the effect in normal range (NR).

And when running into emergency (as met with high wind), it is necessary to during forced landing, user can pull with hand deflation and draw Hand 75 so that primarily serve the gas quick release in the first floating air bag 10 of buoyance lift effect, tie surface staff control Folding and unfolding capstan arrangement 80 processed realizes forced landing.

By such security mechanism, aircraft 100 of travelling can keep a good air pressure balance in day-to-day operation, And can is enough to become operation in case of emergency allowing user also to have at certain response, with the safety of support personnel.

In daily operation, the air pressure inside situation of the first floating air bag 10 can also be detected by manometric module 77, And according to circumstances carry out the supplement of light gas.

In addition, the outside of the first floating air bag 10 has the bowknot of ground tackle 210, when not runing, can pass through rope Tool and conventional ground holdfast or expansion bolt anchor double-air sac structure and aircraft riding seat 30, and keep steady It is fixed, light gas is released without special, can both ensure the safety of equipment, again can be with the saving of cost of implementation.

The system of the aircraft 100 by complete set of travelling of the present embodiment, it can be provided to consumer a kind of brand-new Aerial amusement experience, while possessing sufficient interesting, also with good safety guarantee, it can also lead in cost Cross the saving to main light gas and realize good cost control, can also pass through a series of guarantee in day-to-day operation Measure ensures the stable operation of equipment, is runed beneficial to promoting.

Embodiment 2

Figure 16 is refer to, floating type is present embodiments provided and rides aircraft 200, including ground tackle 210, fixture 220 and embodiment 1 in aircraft 100 of travelling.

Specifically, the quantity of ground tackle 210 is multiple, one end of multiple ground tackles 210 is along aircraft 100 of travelling Circumferential uniformly connection, the other end of multiple ground tackles 210 of first floating air bag 10 are connected with fixture 220, fixture 220 For preventing from travelling, aircraft 100 departs from region of travelling.

The principle of the present embodiment is：

Fixture 220 can be some objects that are heavier and can moving, even as the stone pier.Ground tackle 210 length long enough, it disclosure satisfy that the first floating air bag 10 drives user's buoyance lift, rather than length to be only sufficient to live on ground It is dynamic.

By the cooperation of some such parts, floating type aircraft 200 of riding can be consumer in more places The amusement experience roamed leisurely in the air is provided.

For example, can configures the floating type of the present embodiment and ridden aircraft 200 on some large-scale pleasure boats, allow travel it is winged The popularization operation of row device 100 is more extensive.And fixture 220 can then be designed to the pattern of more operator characteristic, consumption is allowed Person for aircraft 100 of travelling it is with deep impression while, to network operator also can impression, promote industry development.

In summary, aircraft 100 of the present utility model of travelling is provided a kind of new by meticulous design for consumer The interesting recreation facility of grain husk, meets the higher and higher entertainment requirements of people, masses can have fun freely, while have peace again It is complete supporting, ensure consumer safety, rational design allow the operation cost of whole set of installation can also be well controlled, ten Divide with intention and suit the actual demand of consumer and network operator.Floating type aircraft 200 of riding then allows aircraft of travelling 100 operation place is extended, and the service of travelling can be provided for consumer in more places.

Preferred embodiment of the present utility model is the foregoing is only, is not limited to the utility model, for this For the technical staff in field, the utility model can have various modifications and variations.It is all in the spirit and principles of the utility model Within, any modification, equivalent substitution and improvements made etc., it should be included within the scope of protection of the utility model.

Claims (10)

1. The aircraft 1. one kind is travelled, it is characterised in that including：

   Double-air sac structure, the double-air sac structure include the first floating air bag and the second floating air bag, the second floating air bag It is connected with the first floating air bag and positioned at the inside of the first floating air bag；

   Aircraft rides seat, and the aircraft riding seat includes car body, gear unit and propulsion unit, and the car body is used to carry User, the gear unit are used to the power that user applies passing to the propulsion unit and ride the aircraft Seat mass motion, the aircraft riding seat pass through the double-air sac structure floating after inflation；

   Aircraft control system, the aircraft control system include control stick, driving member and mobile rudder, the aircraft control System is installed on the car body, and the control stick is described for the active force that user applies to be transferred to by the driving member Mobile rudder, mobile rudder aircraft riding seat according to the direction controlling of active force turns to and/or lifting；With

   Aircraft security component, the aircraft security component includes safety valve, vent valve and handle of deflating, the safety valve are set It is placed in the second floating air bag and the inner and outer air pressure of the first floating air bag can be balanced, the vent valve is arranged at described First floating air bag, described one end for deflating handle are connected with the vent valve, and other end extends to the aircraft riding Seat, when pullling the deflation handle, the vent valve is opened and causes the first floating air bag deflation.
2. 2. aircraft according to claim 1 of travelling, it is characterised in that the car body includes vehicle body frame, seat and collection There is seat to multiply space for grommet, the vehicle body frame, and the seat is arranged at the seat and multiplies space, and the hook nail is arranged at described The top of vehicle body frame, the first floating air bag are connected with the hook nail.
3. 3. aircraft according to claim 2 of travelling, it is characterised in that the vehicle body frame includes girder, the girder Take the shape of the letter U, the hook nail is arranged at the girder.
4. 4. aircraft according to claim 1 of travelling, it is characterised in that the gear unit include power input mechanism, Transmission device and changement, the power input mechanism are used to exert a force for user, and the transmission device is used for user The power of application is transferred to the changement.
5. 5. aircraft according to claim 4 of travelling, it is characterised in that the power input mechanism is pedal, described Transmission device is the chain gearing that can coordinate with the pedal.
6. 6. aircraft according to claim 1 of travelling, it is characterised in that the aircraft control system includes control command Decomposer, the driving member include the first driving member and the second driving member, and the mobile rudder includes rudder and elevator, described Control command decomposer includes command input, the first instruction output end and the second instruction output end, the command input with The control stick connection, first instruction output end are connected with first driving member, second instruction output end and institute State the connection of the second driving member；

   When the control stick shakes to the left or to the right, first instruction output end is by first driving member to the side The instruction swung to the left or to the right to rudder transmission；

   When the control stick shakes forward or backward, second instruction output end is by second driving member to the liter The instruction that rudder transmission is downward or is swung up is dropped.
7. 7. aircraft according to claim 6 of travelling, it is characterised in that the rudder is handed over the elevator in cross Fork arrangement, the rudder and the elevator are respectively provided with pivot center, the pivot center and the liter of the rudder It is non-intersect between the pivot center of drop rudder.
8. 8. aircraft according to claim 1 of travelling, it is characterised in that the aircraft of travelling also includes folding and unfolding capstan winch and filled Put, the folding and unfolding capstan arrangement includes capstan winch and protection is restricted, and the capstan winch can protect rope, the protection rope and institute described in folding and unfolding State car body connection.
9. 9. aircraft according to claim 1 of travelling, it is characterised in that the aircraft of travelling also is set including filling pumping Standby, the air-extractor that fills includes filling exhaust pipe, and the exhaust pipe that fills includes being used for taking out flexible pipe, the use that inflator is connected In the fast-assembling gas tube being connected with double-air sac structure and the adapter for making the flexible pipe be connected with the fast-assembling gas tube.
10. The aircraft 10. a kind of floating type is ridden, it is characterised in that including any one of ground tackle, fixture and claim 1-9 Described aircraft of travelling, the quantity of the ground tackle be it is multiple, one end of multiple ground tackles along it is described travel it is winged The circumferential uniformly connection of the first floating air bag of row device, the other end and the fixture of multiple ground tackles connect Connect, the fixture is used to prevent the aircraft of travelling from departing from region of travelling.