CN2573373Y - Human body controlled flying knapsack helicopter - Google Patents
Human body controlled flying knapsack helicopter Download PDFInfo
- Publication number
- CN2573373Y CN2573373Y CN 02252413 CN02252413U CN2573373Y CN 2573373 Y CN2573373 Y CN 2573373Y CN 02252413 CN02252413 CN 02252413 CN 02252413 U CN02252413 U CN 02252413U CN 2573373 Y CN2573373 Y CN 2573373Y
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- human body
- helicopter
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- measure
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Abstract
The utility model relates to a backpack-type helicopter which is controlled to fly by a human body. A metal frame is used for connecting and positioning a motor, a gearbox, a wing shaft and two pairs of rotary wings with the same size and opposite rotary directions and the utility model is bound and fixed on a human body through shoulder straps, forming a helicopter which combines a human body and a helicopter. The helicopter can control the flying by a human body and has not a traditional flight control system. The utility model has the advantages of simple structure and easy control.
Description
The utility model relates to a kind of Backpack type autogyro with human body control flight, belongs to the autogyro field.
At present, known autogyro is by auto-bank unit and the feathering system that matches and always controls flight apart from control system that its structure is very complicated, and handles difficulty.
The purpose of this utility model provides a kind of Backpack type autogyro of not establishing the man-machine integration of above-mentioned control system, and the people is the occupant of helicopter still not, is again the flight-control component of autogyro simultaneously.
The purpose of this utility model is achieved in that a framework that is made of metal, the conical gear case that top is installing and fixing a driving engine and matching, two output shafts of gear case straight up, axle head respectively is equipped with a secondary rotor, two secondary rotor rotation directions are measure-alike on the contrary, the upper half of human body size design is pressed in the framework bottom, by binding gallus on aviator's body, an autogyro with the flight of human body direct control is formed in man-machine unification, unique controller of helicopter is an engine throttle, and flicon is to change center-of-gravity position by human body conversion body gesture to cooperate suitable accelerator open degree to realize.Attention when aviator's health and to coil when vertical with the rotor slurry, the pulling force that rotor produces and action of gravity are on same vertical line, and the rotating speed of aviator by throttle change driving engine just can make the helicopter vertical takeoff and landing (VTOL) or hover.Center-of-gravity position reach when aviator's body forward is crooked, helicopter is with people's bench over, the pulling force of rotor and gravity shape at an angle, suitably open the throttle wide improves rotating speed, the synthetic level of pulling force two power when overcoming gravity making a concerted effort forward, fly before the helicopter.In like manner the aviator lean back or left, when crooked to the right helicopter will fly backward or left, flight to the right.The preceding topic of effectively controlling flight with human body is that the human body body weight must be occupied bigger ratio in helicopter, and the physical construction of helicopter should be directly simple in therefore implementing, and alleviates unnecessary weight.
Owing to adopt such scheme, helicopter simple in structure, handle easily.
Below in conjunction with drawings and Examples the utility model is further specified.
Fig. 1 is a schematic diagram of the present utility model.
Among the figure: the human body position that the human body position d. that the human body position c. that the human body position b. that a. flies forward flies backward flies left flies to the right
Fig. 2 is the structural representation of the utility model first embodiment
Fig. 3 is the structural representation of the utility model second embodiment
Fig. 4 is the structural representation of the utility model the 3rd embodiment
Among the figure: 1. rotor 2. wing axles 3. driving engines 4. wing shaft gears 5. driving gears 6. frameworks 7. braces 8. throttle wire drawings
In Fig. 1, braces on the metal framework is bundled in mechanics on aviator's the body, man-machine uniting two into one, human body is to front curve as shown in Figure 1a, the center of gravity reach, helicopter turns forward with human body top, and the direction of pull of rotor and gravity direction shape synthetic at an angle making a concerted effort forward, helicopter flies forward when overcoming gravity.Helicopter will fly backward when in like manner human body was crooked backward, and helicopter will fly left when human body was crooked left, and helicopter will fly to the right shown in Fig. 1 b, Fig. 1 c, Fig. 1 d when human body was crooked to the right.
In embodiment illustrated in fig. 2, the opposite two paddle rotors (1) of a secondary measure-alike rotation direction are respectively adorned in the two identical wing axle (2) parallel to each other straight up of length upper ends, two measure-alike conical wing shaft gears (4) in lower end and two of driving engine (3) axle head measure-alike conical driving gear (5) engagements, and by metal framework (6) connection location, bundle the helicopter of forming man-machine one on the body that is fixed on the aviator by the braces (7) on the framework (6), throttle wire drawing (8) one ends are positioned at aviator's both hands place, and the other end connects driving engine (3) throttle.The width between centers of two secondary two paddle rotors is the virtually any size greater than the rotor radius, and two secondary rotors are tangent less than diameter the time, and the setting angle of two secondary rotors should differ 90 degree.
In the embodiment shown in fig. 3, two measure-alike conical wing shaft gears (4) in opposite two paddle rotors (1) lower end of a secondary measure-alike rotation direction and two of driving engine (3) axle head measure-alike conical driving gear (5) oblique engagements are respectively adorned in the two identical bevelled laterally of length wing axles (2) upper end, and by metal framework (6) connection location, be fixed on by the braces (7) on the framework (6) binding on aviator's the body and form helicopter, throttle wire drawing (8) one ends are positioned at aviator's both hands place, and the other end connects driving engine (3) throttle.
In the embodiment shown in fig. 4, long outer short in two concentric wing axles (2) straight up, one high and one low conical driving gear (5) engagement of respectively adorning two measure-alike conical wing shaft gears (4) in opposite rotor (1) lower end of a secondary measure-alike rotation direction and driving engine (3) axle head in upper end, and by metal framework (6) connection location, be fixed on by the braces (7) on the framework (6) binding on aviator's the body and form helicopter, throttle wire drawing (8) one ends are positioned at aviator's both hands place, and the other end connects driving engine (3) throttle.
Claims (3)
1. Backpack type autogyro with human body control flight, it is by a metal framework, braces, driving engine, gear case, wing axle, rotor and people form, it is characterized in that: the opposite two blade rotors of a secondary measure-alike rotation direction are respectively adorned in the two identical wing axle parallel to each other straight up of length upper ends, two measure-alike conical driving gear engagements of two measure-alike conical wing shaft gears in lower end and driving engine axle head, and by metal framework connection location, be fixed on by the binding gallus on the framework on aviator's the body, throttle wire drawing one end is positioned at aviator's both hands place, and the other end connects engine throttle.
2. Backpack type autogyro as claimed in claim 1 is characterized in that: two wings axially tilt in the outside, wing shaft gear and the engagement of driving gear oblique.
3. Backpack type autogyro as claimed in claim 1 is characterized in that: long tiltedly outer in two concentric wing axles, and the one high and one low opposite rotor of a secondary measure-alike rotation direction of respectively adorning.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02252413 CN2573373Y (en) | 2002-09-01 | 2002-09-01 | Human body controlled flying knapsack helicopter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02252413 CN2573373Y (en) | 2002-09-01 | 2002-09-01 | Human body controlled flying knapsack helicopter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2573373Y true CN2573373Y (en) | 2003-09-17 |
Family
ID=33721913
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 02252413 Expired - Fee Related CN2573373Y (en) | 2002-09-01 | 2002-09-01 | Human body controlled flying knapsack helicopter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2573373Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102806994A (en) * | 2011-05-31 | 2012-12-05 | 王略 | Ultra-light single-person deceleration tilting type coaxial helicopter |
| CN106904277A (en) * | 2017-04-18 | 2017-06-30 | 佛山市神风航空科技有限公司 | A kind of run-up device |
| CN108783846A (en) * | 2018-06-13 | 2018-11-13 | 苏州若依玫信息技术有限公司 | A kind of intelligent knapsack control method with function of safety protection |
-
2002
- 2002-09-01 CN CN 02252413 patent/CN2573373Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102806994A (en) * | 2011-05-31 | 2012-12-05 | 王略 | Ultra-light single-person deceleration tilting type coaxial helicopter |
| CN106904277A (en) * | 2017-04-18 | 2017-06-30 | 佛山市神风航空科技有限公司 | A kind of run-up device |
| CN108783846A (en) * | 2018-06-13 | 2018-11-13 | 苏州若依玫信息技术有限公司 | A kind of intelligent knapsack control method with function of safety protection |
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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 |