CN204428797U - A kind of rotary triangle wing - Google Patents
A kind of rotary triangle wing Download PDFInfo
- Publication number
- CN204428797U CN204428797U CN201420377190.4U CN201420377190U CN204428797U CN 204428797 U CN204428797 U CN 204428797U CN 201420377190 U CN201420377190 U CN 201420377190U CN 204428797 U CN204428797 U CN 204428797U
- Authority
- CN
- China
- Prior art keywords
- crossbeam
- ballast box
- dalta wing
- wing
- cylinder
- 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.)
- Expired - Fee Related
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Abstract
A kind of rotary triangle wing, it relates to recreation facility technical field, the outside of counterweight pillar is provided with ballast box cover, the upper end of counterweight pillar is provided with axis of a cylinder, rotate crossbeam to be connected with axis of a cylinder by the axle sleeve on it, rotate crossbeam upper end and be connected with ballast box lift control system, reducing motor on axis of a cylinder is connected with rotation crossbeam by the gear ring rotated on crossbeam, counterweight pillar both sides are provided with ballast box, one end of steel wire rope is connected with ballast box, the other end of steel wire rope is connected with dalta wing with reel by the pulley rotated on crossbeam, the two ends rotating crossbeam are provided with centrifugally regulated device, the side of centrifugally regulated device is provided with angle axle, the side of angle axle is provided with spring, the face support of dalta wing is connected with manned support, and described manned support bottom is provided with pedal.Its structure is simple, easy to operate, and it has the ability that human body controls lifting flight, and does not need dalta wing professional operation technology just can realize the lifting flight of dalta wing.
Description
Technical field
The utility model relates to recreation facility technical field, is specifically related to a kind of rotary triangle wing.
Background technology
Recreation facility is of all kinds, and wherein rotation and lifting flight class recreation facility kind is also many, and this kind of recreation facility adopts equipment autonomously to rotate and lifting, and its dalta wing can not operate flight near-earth layman.
Summary of the invention
The purpose of this utility model is to provide a kind of rotary triangle wing, and its structure is simple, easy to operate, and it has the ability that human body controls lifting flight, and does not need dalta wing professional operation technology just can realize the lifting flight of dalta wing.
In order to solve the problem existing for background technology, the utility model is by the following technical solutions: it comprises counter-balanced carriage, the manned support of dalta wing, described counter-balanced carriage comprises ballast box, ballast box lift control system, counterweight pillar, ballast box cover, axis of a cylinder, reducing motor, rotate crossbeam, centrifugally regulated device, angle axle, spring, steel wire rope, counterweight pillar is connected with ground by fastening bolt with the lower end of ballast box cover, the outside of counterweight pillar is provided with ballast box cover, the upper end of counterweight pillar is provided with axis of a cylinder, rotate crossbeam to be connected with axis of a cylinder by the axle sleeve on it, and rotation crossbeam upper end is connected with ballast box lift control system, reducing motor on axis of a cylinder is connected with rotation crossbeam by the gear ring rotated on crossbeam, counterweight pillar both sides are provided with ballast box, one end of steel wire rope is connected with ballast box, the other end of steel wire rope is connected with dalta wing with reel by the pulley rotated on crossbeam, the two ends rotating crossbeam are provided with centrifugally regulated device, the side of centrifugally regulated device is provided with angle axle, and the side of angle axle is provided with spring, the manned support of described dalta wing comprises dalta wing, manned support, and the face support of dalta wing is connected with manned support, and described manned support bottom is provided with pedal.
Operation principle of the present utility model: driven by power rotation crossbeam, dalta wing and ballast box rotation, ballast box makes dalta wing side weightlessness alleviate dalta wing heavy burden increases lift, and gravity center of human body's skew makes the generation of dalta wing change Windward angle be elevated.Electric speed reducer on axis of a cylinder connects driven rotary crossbeam by the gear ring rotated on crossbeam and rotates.When ballast box lift control system promotes ballast box, dalta wing and manned support decline, ballast box lift control system only start and at the end of on lower people time use, reel is identical with pulley action outside starting to terminate.When the electric speed reducer driven rotary crossbeam on axis of a cylinder after power supply is connected and dalta wing rotate.The weight of the weight fluctuations adjusting triangle wing side of ballast box, the weight of ballast box increases, the weight saving of dalta wing side, otherwise increases the weight of, and counterweight is the load in order to alleviate dalta wing, makes very little dalta wing just can produce enough lift.When dalta wing can produce lifting when rotated, when human body moves forward on the footrests, dalta wing is that the elevation angle drives human body to decline, when moving after human body, dalta wing drives human body to rise in raising angle, centrifugal force is produced when dalta wing rotates, the steel wire rope looseness in outside, at this moment the centrifugally regulated device rotated on crossbeam plays a part to tighten up steel wire rope.
The utility model has following beneficial effect: its structure is simple, easy to operate, and it has the ability that human body controls lifting flight, and does not need dalta wing professional operation technology just can realize the lifting flight of dalta wing.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model.
Detailed description of the invention
Referring to Fig. 1, this detailed description of the invention is by the following technical solutions: it comprises counter-balanced carriage 1, the manned support 2 of dalta wing, described counter-balanced carriage 1 comprises ballast box 3, ballast box lift control system 4, counterweight pillar 5, ballast box cover 6, axis of a cylinder 7, reducing motor 8, rotate crossbeam 9, centrifugally regulated device 10, angle axle 11, spring 12, steel wire rope 13, counterweight pillar 5 is connected with ground by fastening bolt with the lower end of ballast box cover 6, the outside of counterweight pillar 5 is provided with ballast box cover 6, the upper end of counterweight pillar 5 is provided with axis of a cylinder 7, rotate crossbeam 9 to be connected with axis of a cylinder 7 by the axle sleeve on it, and rotation crossbeam 9 upper end is connected with ballast box lift control system 4, reducing motor 8 on axis of a cylinder 7 is connected with rotation crossbeam 9 by the gear ring rotated on crossbeam 9, counterweight pillar 5 both sides are provided with ballast box 3, one end of steel wire rope 13 is connected with ballast box 3, the other end of steel wire rope 13 is connected with the manned support 2 of reel and dalta wing by the pulley rotated on crossbeam 9, the two ends rotating crossbeam 9 are provided with centrifugally regulated device 10, the side of centrifugally regulated device 10 is provided with angle axle 11, the side of angle axle 11 is provided with spring 12, the manned support of described dalta wing 2 comprises dalta wing 14, manned support 15, and the face support of the manned support of dalta wing 2 is connected with manned support 15, and the bottom of described manned support 15 is provided with pedal 16.
The operation principle of this detailed description of the invention: driven by power rotates crossbeam 9, dalta wing 14 and ballast box 3 and rotates, ballast box 3 makes dalta wing 14 side weightlessness alleviate dalta wing 14 heavy burden increases lift, and gravity center of human body's skew makes dalta wing 14 change Windward angle and produces lifting.Electric speed reducer on axis of a cylinder 7 connects driven rotary crossbeam 9 by the gear ring rotated on crossbeam 9 and rotates.When ballast box lift control system 4 promotes ballast box 3, dalta wing 14 and manned support 15 decline, ballast box lift control system 4 only start and at the end of on lower people time use, reel is identical with pulley action outside starting to terminate.When the electric speed reducer driven rotary crossbeam 9 on axis of a cylinder 7 after power supply is connected and dalta wing 14 rotate.The weight of the weight fluctuations adjusting triangle wing 14 side of ballast box 3, the weight of ballast box 3 increases, dalta wing 14 side weight saving, otherwise increases the weight of, and counterweight is the load in order to alleviate dalta wing 14, makes very little dalta wing 14 just can produce enough lift.When dalta wing 14 can produce lifting when rotated, when human body moves forward on pedal 16, dalta wing 14 drives human body to decline in the elevation angle, when moving after human body, dalta wing 14 drives human body to rise in raising angle, centrifugal force is produced when dalta wing 14 rotates, the steel wire rope 13 in outside relaxes, and at this moment the centrifugally regulated device 10 rotated on crossbeam 9 plays a part to tighten up steel wire rope 13.
This detailed description of the invention has following beneficial effect: its structure is simple, easy to operate, and it has the ability that human body controls lifting flight, and does not need dalta wing professional operation technology just can realize the lifting flight of dalta wing.
Claims (1)
1. a rotary triangle wing, it is characterized in that it comprises counter-balanced carriage (1), the manned support of dalta wing (2), described counter-balanced carriage (1) comprises ballast box (3), ballast box lift control system (4), counterweight pillar (5), ballast box cover (6), axis of a cylinder (7), reducing motor (8), rotate crossbeam (9), centrifugally regulated device (10), angle axle (11), spring (12), steel wire rope (13), counterweight pillar (5) is connected with ground by fastening bolt with the lower end of ballast box cover (6), the outside of counterweight pillar (5) is provided with ballast box cover (6), the upper end of counterweight pillar (5) is provided with axis of a cylinder (7), and the upper end rotating crossbeam (9) is connected with ballast box lift control system (4), rotate crossbeam (9) to be connected with axis of a cylinder (7) by the axle sleeve on it, reducing motor (8) on axis of a cylinder (7) is connected with rotation crossbeam (9) by the gear ring rotated on crossbeam (9), counterweight pillar (5) both sides are provided with ballast box (3), one end of steel wire rope (13) is connected with ballast box (3), the other end of steel wire rope (13) is connected with the manned support of reel and dalta wing (2) by the pulley rotated on crossbeam (9), the two ends rotating crossbeam (9) are provided with centrifugally regulated device (10), the side of centrifugally regulated device (10) is provided with angle axle (11), the side of angle axle (11) is provided with spring (12), the manned support of described dalta wing (2) comprises dalta wing (14), manned support (15), the face support of the manned support of dalta wing (2) is connected with manned support (15), the bottom of described manned support (15) is provided with pedal (16).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420377190.4U CN204428797U (en) | 2014-07-09 | 2014-07-09 | A kind of rotary triangle wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420377190.4U CN204428797U (en) | 2014-07-09 | 2014-07-09 | A kind of rotary triangle wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204428797U true CN204428797U (en) | 2015-07-01 |
Family
ID=53596721
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420377190.4U Expired - Fee Related CN204428797U (en) | 2014-07-09 | 2014-07-09 | A kind of rotary triangle wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204428797U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105879394A (en) * | 2016-07-05 | 2016-08-24 | 王文杰 | Flight game device and rack thereof |
| CN107086526A (en) * | 2017-05-27 | 2017-08-22 | 中山市金马科技娱乐设备股份有限公司 | A kind of new flight tap cable tightening structure |
| CN112697642A (en) * | 2020-12-05 | 2021-04-23 | 合肥市公路桥梁工程有限责任公司 | Highway construction slurry proportion detection device and method convenient to adjust |
| CN114307101A (en) * | 2021-12-31 | 2022-04-12 | 武汉大学 | Simulated flight system |
-
2014
- 2014-07-09 CN CN201420377190.4U patent/CN204428797U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105879394A (en) * | 2016-07-05 | 2016-08-24 | 王文杰 | Flight game device and rack thereof |
| CN105879394B (en) * | 2016-07-05 | 2018-03-06 | 王文杰 | A kind of flight amusement device and its frame |
| CN107086526A (en) * | 2017-05-27 | 2017-08-22 | 中山市金马科技娱乐设备股份有限公司 | A kind of new flight tap cable tightening structure |
| CN112697642A (en) * | 2020-12-05 | 2021-04-23 | 合肥市公路桥梁工程有限责任公司 | Highway construction slurry proportion detection device and method convenient to adjust |
| CN114307101A (en) * | 2021-12-31 | 2022-04-12 | 武汉大学 | Simulated flight system |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150701 Termination date: 20170709 |