CN200974614Y - Internal capsule inflatable free aircraft - Google Patents
Internal capsule inflatable free aircraft Download PDFInfo
- Publication number
- CN200974614Y CN200974614Y CN 200620022095 CN200620022095U CN200974614Y CN 200974614 Y CN200974614 Y CN 200974614Y CN 200620022095 CN200620022095 CN 200620022095 CN 200620022095 U CN200620022095 U CN 200620022095U CN 200974614 Y CN200974614 Y CN 200974614Y
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- CN
- China
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- boss
- lifting device
- lift device
- base
- utility
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- Expired - Fee Related
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Abstract
An internal bag pneumatic free aircraft of the utility model relates to a free flying device. A lifting device is formed by an upper cover of the lifting device being combined with a lifting device base. A main body is a cylinder with a front end protruding forward into a sharp shape and a tail part opened with an air valve upward and downward respectively, the air valve is equipped with an air valve plug, an isolating air bag is between the upper cover of the lifting device and the lifting device base, a boss is provided in an outer part center of a lifting device base board, a stiffened plate is arranged every 90 degrees around the boss, three circular rings are provided on the boss and connected with a waist belt of the people through three cords, a dynamic device is an arc sheet provided with a soft belt in a hemline center; a boss 1/3 upwards the hemline and a handle is provided on the boss which is assembled with radiating stiffened plates around to connect the handle with a human palm and connect the soft belt with a human arm. The utility model adopts the air bag with a unique form and the air bag full of hydrogen can freely control the taking off and the descending of the aircraft with the help of the dynamic device. The utility model can be used for both recreational and exercising purposes and a unique three-line design ensures the security.
Description
Technical field
The utility model relates to a kind of free flight device, in particular for the capsula interna inflatable aircraft of entertainment body-building.
Background technology
At present, existing aircraft adopts the structure of parafoil mostly, and the top canopy is closed by upper and lower slot and forms, and utilizes front opening size and angle to control flight and landing during flight.This aircraft by means of wind-force is difficult to allow the user operate freely, and the flight resistance that gets up is bigger, and canopy is fragile, and other FYA usefulness only, purposes is single, and cost is higher.
Summary of the invention
The purpose of this utility model is to overcome the weak point that exists in the above-mentioned technology, provides a kind of reasonable in design, easy to use, durable in use, integrates recreational and capsula interna inflatable free flight device gymnastics.
In order to achieve the above object, the technical solution adopted in the utility model is: the lift device closes button by lift device loam cake and lift device base and forms, base portion is a cylinder, the outstanding forward formation of front end is pointed, on the afterbody, respectively open a valve down, and be fitted with the valve plug, folder one trapping capsule between lift device loam cake and base, the outside centre of lift device base plate is established a boss, be evenly equipped with gusset every 90 ° on every side, boss is provided with three annulus, links to each other with people's waist belt by three ropes, dynamic equipment is a curved thin plate, the base central part is provided with the moccasin band, and upwards 1/3 place is provided with boss apart from the base, and boss is provided with handle, be furnished with the divergent shape gusset around the boss, handle and moccasin band join with people's palm and arm respectively.
The utility model has the advantages that:
Because the utility model has adopted the air bag of unique profile, in be full of hydrogen after, can take off, descend by free control by dynamic equipment, in amusement, also can take exercise, unique three-way design has guaranteed safety, and is reasonable in design, easy to process.
Description of drawings
Fig. 1 is the utility model structural representation;
Fig. 2 is the utility model lift device structural representation;
Fig. 3 is the birds-eye view of the utility model lift device;
Fig. 4 is the right elevation of the utility model lift device;
Fig. 5 is the upward view of the utility model lift device;
Fig. 6 is the front elevation of the utility model dynamic equipment;
Fig. 7 is the lateral plan of the utility model dynamic equipment;
The specific embodiment
Below in conjunction with accompanying drawing embodiment of the present utility model is described in further detail.
By Fig. 1-Fig. 7 as can be known, the utility model lift device closes button by lift device loam cake 1 and lift device base 2 and forms, its body shape is a cylinder, the outstanding forward formation of front end is pointed, on the afterbody, respectively open a valve 3 down, and be fitted with valve plug 4,2 folders of lift device loam cake 1 and base, one trapping capsule 5, the outside centre of lift device base plate is established a boss 6, is evenly equipped with gusset 7 every 90 ° on every side, mainly gains in strength, boss 6 is provided with three annulus 8, link to each other with people's waist belt by three ropes 14, earlier valve is opened during use, following valve charges into air and is close to lift device loam cake 1 inwall fully until trapping capsule 5, again hydrogen is charged into by last valve, be close to lift device base 2 inwalls fully until trapping capsule 5, fully be full of hydrogen in the lift device this moment, fills in, following valve gets final product.
Dynamic equipment 9 is a curved thin plate, the base central part is provided with moccasin band 13, large and smallly be as the criterion with forearm by the people, upwards 1/3 place is provided with boss 11 apart from the base, and boss 11 is provided with handle 12, is furnished with divergent shape gusset 10 around the boss 11, it shown in the figure right hand dynamic equipment, the right side gusset distributes closeer and long, and the left side is dredged and lacked, and the left hand dynamic equipment is just in time opposite with it.
When this aircraft work, with three ropes people's waist belt is coupled together with three annulus 8 on the lift device lower end boss 6, to be full of hydrogen in the lift device as stated above, people's both arms extend through the moccasin band 13 of dynamic equipment lower end, and the handle 12 of holding with a firm grip, power and the combined action of people's double-arm dynamic equipment that provided by the lift device this moment, the people can finish automatic control, free flight.Can shake dynamic equipment soon when full of physical strength, slow shake or do not shake dynamic equipment and can fall.
Claims (2)
1. capsula interna inflatable free flight device, comprise, it is characterized in that: the lift device closes button by lift device loam cake (1) and lift device base (2) and forms, base portion is a cylinder, the outstanding forward formation of front end is pointed, on the afterbody, respectively open a valve (3) down, and be fitted with valve plug (4), folder one trapping capsule (5) between lift device loam cake (1) and base (2), the outside centre of lift device base plate is established a boss (6), be evenly equipped with gusset (7) every 90 ° on every side, boss (6) is provided with three annulus (8), link to each other with people's waist belt by three ropes (14), dynamic equipment (9) is a curved thin plate, and the base central part is provided with moccasin band (13), upwards 1/3 place is provided with boss (11) apart from the base, boss (11) is provided with handle (12), and boss (11) is furnished with divergent shape gusset (10) all around, and handle (12) and moccasin band (13) join with people's palm and arm respectively.
2. capsula interna inflatable free flight device according to claim 1 is characterized in that: have a rope (15) to link to each other with people's waist belt on the dynamic equipment (9).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620022095 CN200974614Y (en) | 2006-11-28 | 2006-11-28 | Internal capsule inflatable free aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200620022095 CN200974614Y (en) | 2006-11-28 | 2006-11-28 | Internal capsule inflatable free aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN200974614Y true CN200974614Y (en) | 2007-11-14 |
Family
ID=38900906
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200620022095 Expired - Fee Related CN200974614Y (en) | 2006-11-28 | 2006-11-28 | Internal capsule inflatable free aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN200974614Y (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106174781A (en) * | 2016-09-09 | 2016-12-07 | 张俊明 | A kind of flight equipment |
-
2006
- 2006-11-28 CN CN 200620022095 patent/CN200974614Y/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106174781A (en) * | 2016-09-09 | 2016-12-07 | 张俊明 | A kind of flight equipment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20071114 Termination date: 20151128 |