CN104908943B - Take turns rope flapping wing mechanism - Google Patents
Take turns rope flapping wing mechanism Download PDFInfo
- Publication number
- CN104908943B CN104908943B CN201410276203.3A CN201410276203A CN104908943B CN 104908943 B CN104908943 B CN 104908943B CN 201410276203 A CN201410276203 A CN 201410276203A CN 104908943 B CN104908943 B CN 104908943B
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- CN
- China
- Prior art keywords
- wheel
- flapping wing
- flexible cable
- wing
- wing wheel
- Prior art date
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Abstract
The present invention provides a kind of wheel rope flapping wing mechanism, it is therefore an objective to solves to flop wing by manpower, realizes that most basic raising is landed.To achieve the above object, the present invention is using the combined method taken turns with rope, wherein having used two flapping wing wheels, five directive wheels, four flexible cables, two support force rings.Flapping wing wheel and wing root are affixed, and flapping wing wheel plane is vertical with wing plane, flapping wing wheel axle center and the axis coinciding of wing swinging axle.Four end points of four flexible cables separate two-by-two, it is separately fixed on two flapping wing wheels, then a point inboard outside extraction converges after reverse wound flapping wing wheel two-by-two, left and right pile warp directive wheel two-by-two again, by the another end of four flexible cables, left and right is connected on support force ring two-by-two, the tangential force of flapping wing wheel torsional moment is thus changed into the active force that support force ring vertically moves, operated for people's legs and feet.So by the support force of the human body shoulder back of the body and legs and feet come wing of flopping, achievable most basic raising landing.
Description
Technical field
The invention belongs to flapping wing aircraft field.
Background technology
Since ancient times I to fly be the mankind lean on itself strength flight a hope, mankind's flapping flight as bird, mesh
It is preceding not realize.
The content of the invention
The present invention provides a kind of wheel rope flapping wing mechanism, it is therefore an objective to solves to flop wing by manpower, realizes most basic
Lifting falls.
To achieve the above object, present invention employs wheel and Suo Zuhe method, wherein with two, flapping wing wheel, directive wheel five
Individual, four and two support force rings of flexible cable.
Flapping wing wheel and wing root are affixed, and flapping wing wheel plane is vertical with wing plane, flapping wing wheel axle center and wing swinging axle
Axis coinciding, two flapping wing wheel planes in the same plane, get married depending on build by size, distance.Flapping wing wheel shaft (that is, wing is put
Moving axis) and each guide wheel shaft be all fixed on by bearing on backrest relevant position, backrest and human body shoulder are carried on the back, waist hip is fixed.
It is parallel with flapping wing wheel plane that the back of the body flutters flexible cable directive wheel plane, carries on the back and flutters on the outside of flexible cable directive wheel outside tangent line and right flapping wing wheel
Lateral incision line overlaps, and the back of the body flutters flexible cable directive wheel with flapping wing wheel apart from the compact action for not interfering rope and wheel.
Left and right shoulder wheel plane is vertical with left and right flapping wing wheel plane respectively, on left and right shoulder wheel tangent line respectively with left and right flapping wing
Wheel outside tangent line overlaps.
Left and right waist wheel plane is parallel with left and right shoulder wheel plane respectively, on rear side of left and right waist wheel tangent line respectively with left and right shoulder wheel
Front side tangent line overlaps.
Four end points of four flexible cables are fixed on two flapping wing wheels two-by-two respectively, then reverse wound flapping wing wheel two-by-two, are twined
It is more than the distance of support force ring movement around length, the abdomen drawn on the outside of flapping wing wheel is flutterred traction flexible cable and drawn on the inside of left shoulder wheel, flapping wing wheel
Go out the back of the body and flutter traction flexible cable around right shoulder wheel, then left and right is connected to support force two-by-two by the another end of four flexible cables by corresponding waist wheel respectively
On ring, the tangential force of flapping wing wheel torsional moment is thus changed into the active force that support force ring vertically moves, operated for people's legs and feet.
Person upright, two legs and feet alternately apply active force on support force ring, flapping wing wheel is carried out back rotation.Legs and feet displacement
Corresponding flapping wing wheel swing angle, swing angle is within 180 °.Size, speed, the distance of control action power, which are equal to, controls wing
Wing is flopped dynamics, frequency, amplitude.So by the support force of the human body shoulder back of the body and legs and feet come wing of flopping, achievable most basic raising
Landing.
Human body is bent over, and considers that people's is physical limited, and increase auxiliary power necessitates.Can be in above-mentioned wheel rope flapping wing mechanism
Increase an Aided Machine power wheel.Reverse wound four two-by-two are distinguished again on two flapping wing wheels (corresponding adjustment flapping wing wheel thickness)
Its end points of bar flexible cable is fixed, and the another end of four flexible cables of extraction two-by-two in auxiliary power wheel upper extreme point fix by reverse wound.Control is dynamic
The positive and negative rotation of wheels must make power wheel drive the angle that flapping wing wheel rotates within 180 ° of degree, it is necessary to same with the motion of people's legs and feet
Walk wing of flopping.
Epicycle rope flapping wing mechanism removes the component of manual operation part, only with flapping wing wheel, power wheel combines with flexible cable can be single
Solely used on flapping-wing aircraft.
Brief description of the drawings
Fig. 1 person upright's status wheel rope flapping wing mechanism front views
Fig. 2 person upright's status wheel rope flapping wing mechanism right views
Fig. 3 person upright's status wheel rope flapping wing mechanism top views
Fig. 4 human body stooped over position wheel rope flapping wing mechanism front views
Fig. 5 human body stooped over position wheel rope flapping wing mechanism right views
Fig. 6 human body stooped over position wheel rope flapping wing mechanism top views
In figure：The left flapping wing wheels of 1-；The right flapping wing wheels of 2-；The 3- back ofs the body flutter flexible cable directive wheel；The left shoulder directive wheels of 4-；The right shoulders of 5- are oriented to
Wheel；The left waist directive wheels of 6-；7- bends on the right side directive wheel；8th, 9- abdomens flutter flexible cable；10th, the 11- back ofs the body flutter flexible cable；The left support force rings of 12-；13- is right
Support force ring；14- machine power wheels；15th, 16- abdomens flutter power traction flexible cable；17th, the 18- back ofs the body flutter power traction flexible cable.
Embodiment
Present invention wheel rope flapping wing mechanism (Fig. 1, Fig. 2, Fig. 3) embodiment：
Flapping wing wheel 1,2 is separately fixed at left and right wing root, and flapping wing wheel plane is mutually perpendicular to wing plane, flapping wing wheel shaft
The axis coinciding of the heart and wing swinging axle, distance between coplanar upper two flapping wings wheel is compact, which not to interfere flexible cable to move, is advisable, flapping wing
Wheel shaft (that is, wing swinging axle) is fixed in backrest by bearing.
The plane of directive wheel 3 is parallel with the plane of flapping wing wheel 2, the tangent line and the outside tangent line of flapping wing wheel 2 in the outside of directive wheel 3 with
Flexible cable 10,11 overlaps, and the distance of directive wheel 3 and flapping wing wheel 2 answers compact non-interference flexible cable and the action of wheel, and directive wheel 3 passes through
Bearing is fixed in the backrest between human body and flapping wing wheel 2.
The plane of directive wheel 4 is vertical with the plane of flapping wing wheel 1, the top tangent line of directive wheel 4 and the outside tangent line of flapping wing wheel 1 with it is soft
Rope 8,9 is overlapped, and the distance of directive wheel 4 and flapping wing wheel 1 is answered compact and is more than directive wheel 3 with flapping wing wheel 2 apart from sum, directive wheel 4
It is fixed on by bearing in the backrest of human body left shoulder position.
The plane of directive wheel 5 is vertical with the plane of flapping wing wheel 2, the top tangent line of directive wheel 5 and the outside tangent line of flapping wing wheel 2 with it is soft
Rope 10,11 is overlapped, and the distance of directive wheel 5 and flapping wing wheel 2 is answered compact and is more than directive wheel 3 with flapping wing wheel 2 apart from sum, directive wheel
5 are fixed on by bearing in the backrest of human body right shoulder.
Directive wheel 6,7 planes overlap with directive wheel 4,5 planes respectively, directive wheel 6,7 rear side tangent lines respectively with directive wheel 4,5
Front side tangent line is overlapped, and directive wheel 6,7 is separately fixed at by bearing in the backrest of left and right waist crotch position.
Flexible cable 8,9 end points are separately fixed on flapping wing wheel 1,2 and wound, and what coiling length was more than pin scrunches distance, and another two
End is drawn along on the outside of two flapping wing wheels towards human body direction, flexible cable 9 further around flapping wing wheel 2 backwards to human body draw further around through flapping wing wheel 1 with it is soft
Rope 8 converges, and around directive wheel 4, by directive wheel 6, connects with left support force ring 12.
Flexible cable 10,11 end points are separately fixed on flapping wing wheel 1,2 and wound, and coiling length scrunches distance more than pin, separately
Both ends are drawn along among two flapping wing wheels towards human body direction, after converging, around directive wheel 3, around directive wheel 5, by directive wheel 7
Connect with right support force ring 13.
Present invention wheel rope flapping wing mechanism operation is to be completed by the shoulder back of the body of people with the support force of legs and feet.
Left support force ring 12 is pedaled, the traction flapping wing of flexible cable 8,9 wheel 1 rotates clockwise traction flapping wing wheel 2 and rotated counterclockwise, and makes two wings
Flapwise belly is flopped, while two flapping wing wheels roll right support force ring 13.
Right support force ring 13 is pedaled, the traction flapping wing of flexible cable 10,11 wheel 1 rotates counterclockwise flapping wing wheel 2 and rotated clockwise, and makes two wings
Flopped to back, while two flapping wing wheels roll left support force ring 12.
Two legs and feet alternately apply active force on support force ring and flopped wing, and control size of exerting oneself can realize most basic raising
Landing.
Consider that people's is physical limited, can increase a He of Aided Machine power wheel 14 in the present invention takes turns rope flapping wing mechanism
Four flexible cables 15,16,17,18.(Fig. 4, Fig. 5, Fig. 6).
Machine power wheel 14 depends on the side of human body back one between being placed in two flapping wing wheels, and machine power wheel [14] plane is flutterred with two
Wing wheel plane is parallel, and the distance between two flapping wing wheels is answered compact non-interference with flexible cable.
Flexible cable 15,16 end points are separately fixed on flapping wing wheel, clockwise again by guiding to power wheel on the outside of flapping wing wheel after winding
Fixed around upper extreme point.
Flexible cable 17,18 end points are separately fixed on flapping wing wheel, counterclockwise again by guiding to power wheel on the inside of flapping wing wheel after winding
Fixed around upper extreme point.
Control the motion of power wheel forward and reverse rotation synchronous with left and right support force ring linear motion, realize the muscle power of supplement people not
Foot.
Present invention wheel rope flapping wing mechanism removes manual operation component, only with flapping wing wheel 1,2 and power wheel 14 and flexible cable 15,
16th, 17,18 combinations can be individually mounted on flapping-wing aircraft of different sizes and use.
Claims (1)
1. one kind wheel rope flapping wing mechanism, it is characterised in that including：Left flapping wing wheel (1), right flapping wing wheel (2), the back of the body flutter flexible cable directive wheel
(3), left shoulder directive wheel (4), right shoulder directive wheel (5), left waist directive wheel (6), right waist directive wheel (7), left abdomen flutter flexible cable (8), the right side
Abdomen flutters flexible cable (9), the left back of the body flutters flexible cable (10), the right back of the body flutters flexible cable (11), left support force ring (12), right support force ring (13), left wing, the right side
Wing, backrest；The left flapping wing wheel (1), the right flapping wing wheel (2) are separately fixed at the left wing, the root of the right wing
Portion, and where the plane where the left flapping wing wheel (1), the right flapping wing wheel (2) and the left wing, the right wing
Plane is vertical, and the left flapping wing wheel (1), the axle center of the right flapping wing wheel (2) are swung with the left wing, the right wing respectively
The axis coinciding of axle；The back of the body flutters flexible cable directive wheel (3), the left shoulder directive wheel (4), the right shoulder directive wheel (5), the left side
Waist directive wheel (6), the right waist directive wheel (7) are fixed in the backrest by bearing；The left abdomen flutters flexible cable (8), institute
State right abdomen flutter flexible cable (9) end points be separately fixed at the left flapping wing wheel (1), the winding of on the right flapping wing wheel (2) and left and right, separately
Both ends are drawn along the left flapping wing wheel (1), right flapping wing wheel (2) lateral direction, and the right abdomen flutters flexible cable (9) further around the right side
Drawn on the inside of flapping wing wheel (2), flutter flexible cable (8) with the left abdomen to outside further around the left flapping wing wheel (1) and converge, around the left side
Shoulder directive wheel (4), by the left waist directive wheel (6), connect with the left support force ring (12)；It is described it is left the back of the body flutter flexible cable (10),
It is described it is right carry on the back flutter flexible cable (11) end points be separately fixed at the left flapping wing wheel (1), on the right flapping wing wheel (2) and right left side twines
Around another both ends are drawn after converging along the left flapping wing wheel (1), the middle direction of the right flapping wing wheel (2), are flutterred around the back of the body soft
Rope directive wheel (3), around the right shoulder directive wheel (5), by the right waist directive wheel (7) and right support force ring (13) phase
Connect；Also include：Machine power wheel (14) and the first flexible cable (15), the second flexible cable (16), the 3rd flexible cable (17), the 4th flexible cable
(18), the machine power wheel (14) is installed in the backrest, and is located at the left flapping wing wheel (1) and the right flapping wing wheel
(2) between, plane where the machine power wheel (14) and plane where the left flapping wing wheel (1) and the right flapping wing wheel (2)
Parallel, first flexible cable (15), the end points of second flexible cable (16) are separately fixed at the left flapping wing wheel (1), the right side
The winding of on flapping wing wheel (2) and left and right, then guide to the machine along the left flapping wing wheel (1), right flapping wing wheel (2) outside respectively
Tool power wheel (14) winding aft terminal is fixed, and the 3rd flexible cable (17), the end points of the 4th flexible cable (18) are also fixed respectively
On the left flapping wing wheel (1) and the right flapping wing wheel (2) and right left winding, then flutterred along the left flapping wing wheel (1), the right side
Guide to the machine power wheel (14) on the inside of wing wheel (2), and according to first flexible cable (15), second flexible cable (16) phase
Anti- direction is wrapped on power wheel (14), and end points is fixed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410276203.3A CN104908943B (en) | 2014-06-20 | 2014-06-20 | Take turns rope flapping wing mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410276203.3A CN104908943B (en) | 2014-06-20 | 2014-06-20 | Take turns rope flapping wing mechanism |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN104908943A CN104908943A (en) | 2015-09-16 |
| CN104908943B true CN104908943B (en) | 2018-01-16 |
Family
ID=54078479
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410276203.3A Expired - Fee Related CN104908943B (en) | 2014-06-20 | 2014-06-20 | Take turns rope flapping wing mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104908943B (en) |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN85108572A (en) * | 1985-11-09 | 1987-06-03 | 魏强 | Flapping wing aircraft |
| CN1508044A (en) * | 2002-12-18 | 2004-06-30 | 张志亮 | Manned flapping-wing craft |
| US7255305B2 (en) * | 2004-11-02 | 2007-08-14 | Milan Dennis Earl | Flying device utilizing natural principles |
| CN201052838Y (en) * | 2007-05-29 | 2008-04-30 | 吴思泉 | Manpower aircraft |
| KR101031869B1 (en) * | 2009-06-08 | 2011-05-02 | 건국대학교 산학협력단 | Flapping system for a large flapping angle generation |
| JP2014008867A (en) * | 2012-06-29 | 2014-01-20 | Yoshikata Rokusha | Body installation type flight tool and flight support device |
| CN203158229U (en) * | 2012-12-13 | 2013-08-28 | 王发身 | Bionic flapping-wing aircraft |
-
2014
- 2014-06-20 CN CN201410276203.3A patent/CN104908943B/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| CN104908943A (en) | 2015-09-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| DD01 | Delivery of document by public notice |
Addressee: Wang Jingchan Document name: Notification of Passing Preliminary Examination of the Application for Invention |
|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| DD01 | Delivery of document by public notice | ||
| DD01 | Delivery of document by public notice |
Addressee: Wang Jingchan Document name: Notification of an Office Action |
|
| GR01 | Patent grant | ||
| 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: 20180116 Termination date: 20210620 |