CN106394900A - Leg control type one-man flight device - Google Patents
Leg control type one-man flight device Download PDFInfo
- Publication number
- CN106394900A CN106394900A CN201610909844.7A CN201610909844A CN106394900A CN 106394900 A CN106394900 A CN 106394900A CN 201610909844 A CN201610909844 A CN 201610909844A CN 106394900 A CN106394900 A CN 106394900A
- Authority
- CN
- China
- Prior art keywords
- flight device
- lower limb
- control type
- leg control
- pilot
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/026—Aircraft not otherwise provided for characterised by special use for use as personal propulsion unit
Abstract
The invention discloses a leg control type one-man flight device. A main mechanism comprises two propellers, a supporting frame, pedals, a waist rod and a spring yawing force offset mechanism. The two propellers are arranged on the left side and the right side of a pilot correspondingly and connected with limbs of the pilot through the supporting frame and the pedals, and meanwhile a spring force saving mechanism and the waist rod are connected to achieve the yawing force offset function. The flight device is small and exquisite and light, easy to drive, simple in structure, capable of vertically taking off and landing, flexible and reliable. The leg control type one-man flight device can be used for investigation, accident emergency escape, aerial photography, forest fire prevention and other any occasions where the flight device can fly.
Description
Technical field
The present invention relates to vehicle technology field, belong to individual lift device.
Background technology
At present in the world, the most propeller by aircraft of individual lift device is placed overhead, and only a few design will advance
Device is placed under sole, even if having a few money designs to be that propeller is placed under sole, also because cannot accomplish perfectly to fly very much
Row controls, and does not reach the effect of practicality.Occur in the world in the recent period very large-scale can manned four-axle aircraft, also because of power consumption
Height, needs Electronic Control, the shortcomings of technical sophistication degree is high.Cost is led to remain high.Lower limb control formula flight designed by the present invention
Device, because that eliminating flight control system, is controlled using the both legs of people so that pilot can obtain the manipulation spirit of maximum
Activity.The far super existing aircraft of mobility, and cost is lower.Due to propeller be divide into left and right two, add lower limb control
Motility.The danger of flame-out in flight can be reduced to a certain extent.
Content of the invention
It is an object of the invention to provide a kind of small volume and less weight, simply, driving is easily and the single of flexibility and reliability flies for structure
Row device, i.e. a kind of lower limb control formula individual lift device.
Its outstanding feature of the present invention is that pilot can pass through the freely activity of lower limb, controls angle of rake direction of propulsion.
And then control heading.Implementation is to place two propellers respectively in human pilot left and right sides lower extremity.Pass through
Bracing frame and the foot-operated left and right sides lower extremity that two propellers are fixed on driver.
Again because by impeller design in the both sides of pilot. the thrust that propeller produces will necessarily be because of the thick stick of bracing frame
Bar effect produces the side force pointing to pilot's waist. and this side force necessarily leads to driver's both legs in long-term flight course
Separate problem.For solve the problems, such as the separate present invention of this both legs waist hipbone position increased waist bar utilize waist bar rigidity
Synergy with spring makes the angle of rake side force in both sides cancel out each other.
Brief description
Fig. 1 is present configuration master map
It is embodied as explanation
Below in conjunction with the accompanying drawings the technical scheme of invention is described in detail：
Referring to accompanying drawing 1, the present invention includes propeller 1, bracing frame 2, rides 3, waist bar 4, spherical hinge 5, spring
6, elastic force set screw 7, belt 8.
Wherein propeller 1 provides flying power, produces thrust F upwards, and thrust F passes through bracing frame 2, and foot-operated 3 biographies
Pass pilot, and then drive flight.Pilot controls the direction of bracing frame 2 by leg, and then indirectly controls propulsion
The direction of propulsion of device 1.The purpose of arbitrarily angled flight can be reached.The present invention is in the premise of few loss manipulation degree of freedom as far as possible
Lower bracing frame 2 and waist bar 4 are connected using spherical hinge 5 mechanism.
Because bracing frame 2 the strong point in foot-operated 3 position, and thrust F is in the connection of bracing frame 2 and propeller 1
Place.2 points in same place.The inevitable effect because of lever produces certain component f, is applied to driver by bracing frame 2
Waist.For solving this problem, invention increases mechanism's spring 6, it is applied on waist bar 4 by spring handle power f, because of two
Side has same power f in opposite direction.Cancelled out each other by the rigidity of waist bar 4.So having necessarily to the mechanical rigid of waist bar 4
Requirement.
Claims (3)
1. a kind of lower limb control formula individual lift device, including propeller 1, supporting mechanism 2, rides 3, waist bar 4, spherical hinge 5, spring 6, adjusts
Section screw 7, belt 8.
2. the lower limb control formula individual lift device according to claims 1 it is characterised in that：Propeller 1 is the two of driver
The lower limb binding that side is passed through supporting mechanism 2 and ridden 3 and driver. allow driver to pass through lower limb controlling propeller 1
Direction.
3. the lower limb control formula individual lift device according to claims 1 it is characterised in that：Described waist bar 4 passes through spherical hinge
5 are connected with supporting mechanism 2, balance out side force produced by two side propellers 1 by waist bar 4 and spring 6.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610909844.7A CN106394900A (en) | 2016-10-19 | 2016-10-19 | Leg control type one-man flight device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610909844.7A CN106394900A (en) | 2016-10-19 | 2016-10-19 | Leg control type one-man flight device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106394900A true CN106394900A (en) | 2017-02-15 |
Family
ID=58013205
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610909844.7A Pending CN106394900A (en) | 2016-10-19 | 2016-10-19 | Leg control type one-man flight device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106394900A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110536835A (en) * | 2017-02-22 | 2019-12-03 | 重力工业有限公司 | Flight system |
-
2016
- 2016-10-19 CN CN201610909844.7A patent/CN106394900A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110536835A (en) * | 2017-02-22 | 2019-12-03 | 重力工业有限公司 | Flight system |
| CN110536835B (en) * | 2017-02-22 | 2021-09-17 | 重力工业有限公司 | Wearable flight system with propulsion assembly worn on body of user |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170215 |