CN2516457Y - Aircraft composed of hydrogen balloon and flying control device - Google Patents
Aircraft composed of hydrogen balloon and flying control device Download PDFInfo
- Publication number
- CN2516457Y CN2516457Y CN 01266362 CN01266362U CN2516457Y CN 2516457 Y CN2516457 Y CN 2516457Y CN 01266362 CN01266362 CN 01266362 CN 01266362 U CN01266362 U CN 01266362U CN 2516457 Y CN2516457 Y CN 2516457Y
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- balloon
- front case
- aircraft
- propeller
- hydrogen
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Abstract
The utility model discloses a balloon aircraft, which is composed of a hydrogen balloon and a flying control device. Moreover, the hydrogen balloon and the flying control device is linked through a net rope, a net rope disk, a fixed pulley and a wire rope, wherein the inside of the flying control device is provided with an inflation system, a power system, a steering system, a balance system and a braking system. The power system and the hydrogen balloon are utilized for the balloon aircraft in the utility model to provide the rising and advancing motive powers. The steering system and the braking system are also utilized to achieve the effects of lifting, landing as well as steering. Thus the purpose of high-altitude sightseeing is obtained.
Description
Technical field
The utility model relates to a kind of flight tool, more particularly, relates to a kind of hydrogen balloon that utilizes and uses aircraft as promoting going sightseeing of power.
Background technology
The modern visit instrument that uses in tourist attractions has two kinds of crane and outing vehicles basically, and wherein crane is mainly used in the transportation visitor, and avoiding visitor's fatigue, but the speed of this crane is very fast, can't go sightseeing.Though and outing vehicle both can be used for replacing walking, can go sightseeing again, it can only carry out on the ground, can't watch the scenery at sight spot from eminence.
Therefore, in some tourist quarters, be equipped with some to be used for the visit instrument of watching in the high-altitude at present, such as: gondola, autogyro etc.But the difficult support of the control of gondola is held, and causes can not arbitrarily controlling in watching process, and the tourist is enjoyed oneself to heart's content inadequately.And the use autogyro, cost that it is expensive and huge energy charge, the customer is held be can't stand, therefore, how can be the aerial three-dimensional tourism of ground plane formula tourism becoming, the visitor can aloft be got a full view of the whole landscape by air, by plane, can comfortable enjoyment be the matter of utmost importance of the required solution of modern tourism industry under low expense again.
Summary of the invention
For this reason, the balloon aircraft in the utility model mainly is the problem that can't realize aerial sightseeing in the existing tourist attractions in order to solve under state with low cost.
Balloon aircraft in the utility model includes a hydrogen balloon, and this hydrogen balloon thereunder is connected with a flight control unit, and this flight control unit includes a housing, air-charging and air-discharging system, power system, steering swivel system and balanced system, wherein:
The shape of described housing and the appearance similar of existing aircraft, be divided into forward and backward housing two parts, and on the wing of its front case both sides, respectively be provided with a propeller, be provided with a propeller at the tail end of rear housing, simultaneously, described front case is provided with the support wheel that triangle distributes in three in its bottom;
Described power system includes a driving engine that is located at the inboard front end of front case, this driving engine is connected with propeller on being located at front case both sides wing by coupler, part-time case, drive axle and transmission shaft, simultaneously, inboard at described rear housing also is provided with a driving engine, and this driving engine is connected with the propeller that is located at the rear housing tail end by coupler;
Described air-charging and air-discharging system includes air collector, compressor, breather line and a master cock that is located at described front case inside bottom, wherein, air collector is communicated with described hydrogen balloon by compressor, breather line and master cock, and compressor links to each other with the driving engine that is located at the front case inboard by described part-time case;
Described steering swivel system includes the bearing circle that is located at described front case interior forward end, and this bearing circle links to each other by steering box, transmission shaft and the finishing bevel gear cuter that is located at the rear housing inboard, and simultaneously, this steering box is connected with the support wheel that is located at front case front end below;
Described balanced system includes and is located at front case in-to-in sliding rail, and is provided with floating saddle on this sliding rail, and this floating saddle is connected with joystick by drive link.
Wherein, described flight control unit also within it portion be provided with a brake system, this brake system includes a brake rod, this brake rod links to each other with brake wheel in being located at described front case both sides wing propeller by brake cable pull.
Wherein, described hydrogen balloon can thereunder be provided with many nettles, and this nettle is concentrated and is fixed in the nettle dish, and this nettle dish thereunder is set with a fixed pulley, this fixed pulley and described steel rope sliding block joint.Utilize this fixed pulley to make whole flight control unit when flight, can adjust the tension force size and the length of fixed pulley front and back two steel ropes at any time, to keep the balance of described flight control unit.
In addition, described coupler is a universal coupling.
In addition, also can on described three support wheels, be provided with a bumper, thereby can reduce the vibrations of whole flight instruments under landing.
During balloon aircraft in using the utility model, at first the hydrogen in the air collector is filled in the hydrogen balloon, start the driving engine of front case inboard again, the propeller that drives on the wing of both sides is rotated, and adds the effect of hydrogen balloon, and the balloon aircraft is up risen.Start the driving engine of rear housing inboard subsequently, the propeller that drives the rear housing end is rotated, and under the thrust of this propeller, the balloon aircraft moves forward.Balloon aircraft in the utility model not only can the change of flight direction in flight course, and can do the ascending, descending action according to the scenery in the sight spot, reaches the purpose of going sightseeing in the high-altitude.
Description of drawings
The specific embodiment of the utility model is described in further detail below in conjunction with accompanying drawing.
Fig. 1 is the perspective view of balloon aircraft in the utility model;
Fig. 2 is the cross-sectional schematic of flight control unit in the utility model;
Fig. 3 is the principle schematic of flight control unit internally-powered system and brake system in the utility model.
The specific embodiment
As shown in Figure 1, the balloon aircraft in the utility model constitutes main body by hydrogen balloon 1 and flight control unit 2, is connected with steel rope 6 by nettle 3, nettle dish 4, fixed pulley 5 between hydrogen balloon 1 and flight control unit 2.The nettle 3 that extends out from hydrogen balloon 1 below is concentrated and is fixed in the nettle dish 4, be set with a fixed pulley 5 again below this nettle dish 4, and steel rope 6 is connected mutually with the suspension ring 7 of flight control unit 2 rear and front ends after passing fixed pulley 5.
As shown in Figure 2, flight control unit 2 includes the profile housing similar to existing aircraft, and this housing is divided into forward and backward two housings 218,217, wherein front case 218 within it portion be provided with a support 219, utilize this support 219 and rear housing 217 to be articulated.And be provided with air-charging and air-discharging system, power system, steering swivel system, balanced system and the brake system that can charge and discharge hydrogen in this enclosure interior to hydrogen balloon 1.
As depicted in figs. 1 and 2, front case 218 respectively is provided with a propeller 210 on the wing 212,213 of its both sides, simultaneously, is provided with a propeller 211 at the tail end of rear housing 217 by bracing frame 214.Front case 218 support 219 of portion within it is provided with a sliding rail 250, is provided with the support wheel 216,215 of three distributions triangular in shape in its bottom, and wherein front side support wheel 216 is for turning to support wheel, and rear side two support wheels 215 are the motion support wheel.
As Fig. 3 and shown in Figure 2, power system includes the driving engine 230 that is located at front case 218 the place aheads and is located at rear housing 217 in-to-in driving engines 231, wherein, driving engine 230 links to each other with propeller 210 on being located at front case 218 both sides wings 212,213 by universal coupling 232, part-time case 233, drive axle 234 and transmission shaft 235,236, and driving engine 231 links to each other with the propeller 211 that is located at rear housing 217 tail ends by universal coupling 237, and drives this propeller 211 rotations.
As shown in Figure 2, air-charging and air-discharging system includes a hydrogen air collector 220, hydrogen compressor 221, breather line 222 and master cock 223,224, wherein hydrogen air collector 220 is located at the bottom of front case 218 inboards, and it is fixing by support 219, this hydrogen air collector 220 links to each other with hydrogen compressor 221 by breather line 222, master cock 224, and this hydrogen compressor 221 is connected with hydrogen balloon 1 by breather line 222, simultaneously, hydrogen balloon 1 links to each other with hydrogen air collector 220 by breather line, master cock 223 again, forms a loop.Wherein, hydrogen compressor 221 is connected with driving engine 230 by part-time case 233.When to hydrogen balloon 1 inflation, open master cock 223, hydrogen in the hydrogen air collector 220 enters in the hydrogen balloon 1 along breather line, when stopping to fly, closing control switch 223 utilizes driving engine 230 to drive hydrogen compressor 221 work, and opens another master cock 224, under the effect of hydrogen compressor 221, the hydrogen in the hydrogen balloon 1 is failed back in the air collector 220 along pipeline, in order to next repeated usage.In addition, on breather line 222, be provided with a pressure indicating device 225, utilize this pressure indicating device 225 can understand the interior Hydrogen Vapor Pressure of air-charging and air-discharging system, to support the pressure-bearing situation of holding hydrogen balloon at any time.
As shown in Figure 2, steering swivel system in the flight control unit 2 includes the bearing circle 241 that is located at the inboard front end of housing, this bearing circle 241 is connected by steering box 242, universal coupling 243 and the finishing bevel gear cuter 244 that is located at housing rear housing 217 inboards, this finishing bevel gear cuter 244 is meshed with another finishing bevel gear cuter 245, finishing bevel gear cuter 245 then is connected by bracing frame 214 and rear housing 217, articulates with support 219 again simultaneously.By the engagement of this two finishing bevel gear cuter 245 and 244, can drive rear housing 217 rotations.Steering box 242 is connected with the support wheel 216 that is located at housing the place ahead downside simultaneously, and control the hand of rotation of support wheel 216 by steering box 242, the hand of rotation of support wheel 216 matches with the rotation of housing latter half of 217, thereby realizes the direction controllable function of whole balloon aircraft.
The balanced system of balloon aircraft includes the slide rail 250 that is located at support 219 tops, and is provided with two floating saddles 251 on this slide rail 250.This two floating saddle 251 is connected with the joystick 253 that is located at front case 218 front ends by a drive link 252.Under the operation of joystick 253, can adjust the front and back position of floating saddle 251, thereby adjust the center-of-gravity position of whole balloon aircraft, reach the purpose of balloon aircraft pitch balance.
As shown in Figures 2 and 3, the brake system of balloon aircraft includes brake rod 261, this brake rod 261 by brake cable pull 262 respectively be located at housing both sides wing 212,213 on brake wheel 263,264 link to each other, can change the rotating speed of propeller 210 by control brake bar 261, thereby adjust the left and right sides balance of whole balloon aircraft.
During balloon aircraft in using the utility model, at first the hydrogen in the hydrogen air collector 220 is filled in the hydrogen balloon 1, restart the driving engine 230 of front case 218 inboards, and the propeller 210 that drives on the both sides wing 212,213 is rotated, add the effect of hydrogen balloon 1, the balloon aircraft up rises.Start the driving engine 231 of rear housing 217 inboards subsequently, the propeller 211 that drives rear housing 217 ends is rotated, under the thrust of this propeller 211, the balloon aircraft moves forward, this balloon aircraft is in flight course forward, control the rotative speed of propeller 211 by the throttle size of control driving engine 231, thereby control the flying speed that balloon flies.Simultaneously, this balloon aircraft changes its heading by the control steering swivel system in flight course, and control the rotative speed of propeller 210 by the throttle size of control driving engine 230, thereby the flying height of control balloon aircraft realizes the purpose of high-altitude sightseeing tour.
In sum, balloon aircraft in the utility model has functions such as existing autogyro takes off at any time, landing at any time, and have simultaneously turn to, function such as lifting, in addition, balloon aircraft in the utility model is not only easy and simple to handle, and cost is more much lower than existing autogyro.
In addition; above-mentionedly only the preferred embodiment in the utility model is illustrated; can not be as protection domain of the present utility model, every equivalence of having done according to the design spirit in the utility model changes or modifies all should be thought and fall into protection domain of the present utility model.
Claims (10)
1. a balloon aircraft includes a hydrogen balloon, it is characterized in that: this hydrogen balloon thereunder is connected with a flight control unit, and this flight control unit includes a housing, air-charging and air-discharging system, power system, steering swivel system and balanced system, wherein:
The shape of described housing and the appearance similar of existing aircraft, be divided into forward and backward housing two parts, and on the wing of front case both sides, respectively be provided with a propeller, be provided with a propeller at the tail end of rear housing, simultaneously, described front case is provided with the support wheel of three distributions triangular in shape in its bottom;
Described power system includes a driving engine that is located at the inboard front end of front case, this driving engine is connected with propeller on being located at front case both sides wing by coupler, part-time case, drive axle and transmission shaft, simultaneously, also be provided with a driving engine in described rear housing inboard, this driving engine is connected with the propeller that is located at the rear housing tail end by coupler;
Described air-charging and air-discharging system includes air collector, compressor, breather line and a master cock that is located at the front case inside bottom, wherein, air collector is communicated with described hydrogen balloon by compressor, breather line and master cock, and compressor links to each other with the driving engine that is located at the front case inboard by described part-time case;
Described steering swivel system includes the bearing circle that is located at described front case interior forward end, and this bearing circle links to each other by steering box, transmission shaft and the finishing bevel gear cuter that is located at the rear housing inboard, and simultaneously, this steering box is connected with the support wheel that is located at front case front end below;
Described balanced system includes and is located at front case in-to-in sliding rail, and is provided with floating saddle on this sliding rail, and this floating saddle is connected with joystick by drive link.
2. according to the balloon aircraft described in the claim 1, it is characterized in that: described flight control unit portion within it is provided with a brake system, this brake system includes a brake rod, and this brake rod links to each other with brake wheel in being located at front case both sides wing propeller by brake cable pull.
3. according to the balloon aircraft described in claim 1 or 2, it is characterized in that: described hydrogen balloon thereunder is provided with many nettles, and this nettle is concentrated and is fixed in the nettle dish, and this nettle dish is connected with described flight control unit by steel rope.
4. according to the balloon aircraft described in the claim 3, it is characterized in that: described nettle dish thereunder is set with a fixed pulley, this fixed pulley and described steel rope sliding block joint.
5. according to the balloon aircraft described in claim 1 or 2, it is characterized in that: described coupler is a universal coupling.
6. according to the balloon aircraft described in the claim 3, it is characterized in that: described coupler is a universal coupling.
7. according to the balloon aircraft described in the claim 4, it is characterized in that: described coupler is a universal coupling.
8. according to the balloon aircraft described in claim 1 or 2, it is characterized in that: on described three support wheels, be equipped with bumper.
9. according to the balloon aircraft described in the claim 3, it is characterized in that: on described three support wheels, be equipped with bumper.
10. according to the balloon aircraft described in the claim 4, it is characterized in that: on described three support wheels, be equipped with bumper.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 01266362 CN2516457Y (en) | 2001-11-30 | 2001-11-30 | Aircraft composed of hydrogen balloon and flying control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 01266362 CN2516457Y (en) | 2001-11-30 | 2001-11-30 | Aircraft composed of hydrogen balloon and flying control device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2516457Y true CN2516457Y (en) | 2002-10-16 |
Family
ID=33673060
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 01266362 Expired - Fee Related CN2516457Y (en) | 2001-11-30 | 2001-11-30 | Aircraft composed of hydrogen balloon and flying control device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2516457Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103192977A (en) * | 2013-04-18 | 2013-07-10 | 杨礼诚 | High-speed floating aircraft |
| CN106895765A (en) * | 2017-04-18 | 2017-06-27 | 北京林业大学 | A kind of portable precision tree measurement instrument high |
-
2001
- 2001-11-30 CN CN 01266362 patent/CN2516457Y/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103192977A (en) * | 2013-04-18 | 2013-07-10 | 杨礼诚 | High-speed floating aircraft |
| CN106895765A (en) * | 2017-04-18 | 2017-06-27 | 北京林业大学 | A kind of portable precision tree measurement instrument high |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |