CN204056298U - Low latitude assistant sliding delta wing device - Google Patents
Low latitude assistant sliding delta wing device Download PDFInfo
- Publication number
- CN204056298U CN204056298U CN201420375315.XU CN201420375315U CN204056298U CN 204056298 U CN204056298 U CN 204056298U CN 201420375315 U CN201420375315 U CN 201420375315U CN 204056298 U CN204056298 U CN 204056298U
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- CN
- China
- Prior art keywords
- delta wing
- pole
- clubfoot
- bungee
- sleeve
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Abstract
The utility model provides a kind of low latitude assistant sliding delta wing device, comprise delta wing, spring beam, pole, bungee, pulley, steel wire and foot pad, spring beam comprises becoming with delta wing center shaft and is connected to a fixed abreast and withstands on the crossbeam portion foremost of delta wing and be formed in one with crossbeam portion and on termination, be also connected with the camber beam portion of a sleeve, the clubfoot beam be connected with the two is had additional between sleeve and bungee, also be provided with by connecting rod in the dead ahead of clubfoot beam, the auxiliary damping portion of bungee and foot pad composition, auxiliary damping portion is with mutually concordant between clubfoot beam and camber beam portion, pole is set in sleeve and its one end is vertically connected at crossbeam portion, the other end of pole connects a bungee, pulley is fixedly arranged on the junction in pole and crossbeam portion, steel wire is positioned over pole inside and its one end is connected to sleeve, its other end connects leader after walking around pulley, foot pad is connected to the bottom of bungee.The utility model provides a kind of low latitude and to circle in the air product, has higher recreational.
Description
Technical field
The utility model relates to aircraft field, mainly refers to low-latitude flying apparatus field, more specifically, particularly relates to a kind of low latitude assistant sliding delta wing device.
Background technology
In extreme sport, delta wing is one of most popular project tool, its dynamic and unpowered point.The height point in the mountain valley that unpowered delta wing is releived at some up currents under needing participant oneself to be suspended on a delta wing and continued is as launching platform, through one section of run-up, participant takes in the air by the lift that delta wing produces and up current, the motion that a challenge of then aloft gliding is extremely strong.
But above-mentioned project is appointed and is so had certain danger, and needs participant to have good fitness.So make many airhogs hang back, but people are endless for the curiosity of flight, wherein, and can when reducing dangerous for airhog provides a kind of experience of flight, this is the direction that the art is studied, and is also a difficult problem urgently to be resolved hurrily.
Utility model content
In view of the above, the purpose of this utility model is to provide a kind of low latitude assistant sliding delta wing device, for solving the problem how providing flying instrument that a kind of danger is lower.
For achieving the above object and other relevant objects, the utility model provides following technical scheme:
The structural representation of a kind of low latitude assistant sliding delta wing device, from figure, this low latitude assistant sliding delta wing device comprises delta wing, spring beam, pole, bungee, pulley, steel wire and foot pad, wherein, delta wing to be spliced mutually with the second wing plate by the first wing plate and centered by phase stitching portion axle, spring beam comprises crossbeam portion and camber beam portion, crossbeam portion becomes with delta wing center shaft to be connected to a fixed abreast and the termination in crossbeam portion withstands on delta wing foremost, and camber beam portion and crossbeam portion are formed in one and are connected and the termination in camber beam portion are also connected with a sleeve, a clubfoot beam has been set up between sleeve and bungee, two ends coupling bush and the bungee respectively of clubfoot beam, and clubfoot beam is mutually concordant with camber beam portion, clubfoot beam is provided with the first damping spring and the second damping spring that vertically connect camber beam portion successively near sleeve place, also be provided with by connecting rod in the dead ahead of clubfoot beam, the auxiliary damping portion of bungee and foot pad composition, auxiliary damping portion is with mutually concordant between clubfoot beam and camber beam portion, pole is set in sleeve and its one end is vertically connected at crossbeam portion, the other end of pole connects a bungee, pulley is fixedly arranged on the junction in pole and crossbeam portion, steel wire is positioned over pole inside and its one end is connected to sleeve, its other end connects leader after walking around pulley, foot pad is connected to the bottom of bungee.
Technique scheme provides the detailed process of low-latitude flying to be: first, on the pedal that people stands in camber beam portion and hand steered handle (this is people is the state of squatting), pull at handle downwards to be moved along pole top by sleeve simultaneously, camber beam portion is made to become to be squeezed state, then stand fast and to slide by sleeve with loosening steel wire, camber beam portion can be restored to the original state, a power backward and downward power can be produced in the restorable process in camber beam portion, power backward makes whole delta wing travel forward, simultaneously downward power extruding bungee, make to one, delta wing power upwards, under the effect of two power, delta wing will be upspring and under the effect of air to delta wing, be kept the flight of certain hour aloft like this, when delta wing is starting in the process declined, the people be positioned at above should continue to be cycled to repeat the process of drawing steel wire and release steel wire, before landing, flight forward can be continued by the power in camber beam portion to make delta wing.Be to be understood that, the flying height of the low latitude assistant sliding delta wing device in the utility model is very limited, general about 5 meters, only be applicable to the flight entertainment doing low latitude, this is for safety factor on the one hand, on the other hand also relevant with its know-why, because it does not move by machine, so it can not maintain a higher height for a long time.
As mentioned above, the utility model is by utilizing the elastic force of jumping beam below the distortion in camber beam portion and pole as propulsion source, what delta wing can be able to be kept certain height under artificial manipulation slides, thus gives the experience of circling in the air of a kind of low latitude of people, has higher recreational.
Accompanying drawing explanation
In order to be illustrated more clearly in the scheme in the utility model embodiment, be briefly described to describing the required accompanying drawing used in specific embodiment below, apparently, accompanying drawing in the following describes is only embodiments more of the present utility model, for those skilled in the art, under the prerequisite not paying creative work, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 shows the structural representation of a kind of low latitude assistant sliding delta wing device.
Fig. 2 shows pole and the connection diagram between camber beam portion, pulley, steel wire and bungee.
Fig. 3 shows the schematic diagram of pole along Fig. 2 arrow A direction.
Fig. 4 is the structural representation of low latitude assistant sliding delta wing device in an other embodiment.
Drawing reference numeral explanation
1 delta wing
11 first wing plates
12 second wing plates
2 spring beams
21 crossbeam portions
22 camber beam portions
23 sleeves
24 pedals
25 clubfoot beams
26 first damping springs
27 second damping springs
3 poles
31 symmetry slot
4 pulleys
5 bungees
6 steel wires
61 handles
7 foots pad
8 horizontal stripes
9 auxiliary damping portion
91 connecting rods
Detailed description of the invention
Below in conjunction with the accompanying drawing in the utility model embodiment, be clearly and completely described the technical scheme in the utility model embodiment, obviously, described embodiment is only a part of embodiment of the present utility model, instead of whole embodiments.Based on embodiment of the present utility model, other embodiments all that those of ordinary skill in the art obtain under the prerequisite not making creative work, all belong to the scope of the utility model protection.
Embodiment one
Please refer to Fig. 1, show the structural representation of a kind of low latitude assistant sliding delta wing device, from figure, this low latitude assistant sliding delta wing device comprises delta wing 1, spring beam 2, pole 3, bungee 5, pulley 4, steel wire 6 and foot pad 7, wherein, delta wing 1 to be spliced mutually with the second wing plate 12 by the first wing plate 11 and centered by phase stitching portion axle (the first wing plate 11 and the second wing plate 12 are that axis of symmetry tilts to both sides with center shaft, namely the first wing plate 11 and the second wing plate 12 phase stitching portion are top), spring beam 2 comprises crossbeam portion 21 and camber beam portion 22, crossbeam portion 21 becomes with delta wing 1 center shaft to be connected to a fixed abreast and the termination in crossbeam portion 21 withstands on delta wing 1 foremost, and camber beam portion 22 and crossbeam portion 21 are formed in one and are connected and the termination in camber beam portion 22 are also connected with a sleeve 23, pole 3 is set in sleeve 23 and its one end is vertically connected at crossbeam portion 21, the other end of pole 3 connects a bungee 5, pulley 4 is fixedly arranged on the junction in pole 3 and crossbeam portion 21, steel wire 6 is positioned over pole 3 inside and its one end is connected to sleeve 23, its other end connects leader 61 after walking around pulley 4, foot pad 7 is connected to the bottom of bungee 5.
Particularly, in order to clearly set forth technique scheme, see Fig. 2, show pole 3 and the connection diagram between camber beam portion 22, pulley 4, steel wire 6 and bungee 5, the top of pole 3 is connected to crossbeam portion 21 and the pulley 4 of spring beam 2 simultaneously, and the bottom of pole 3 is connected to bungee 5, the sleeve 23 in the camber beam portion 22 of simultaneously spring beam 2 to be socketed on pole 3 and between pulley 4 and bungee 5.See Fig. 3, show the schematic diagram of pole 3 along Fig. 2 arrow A direction, known according to figure, why sleeve 23 can move up and down along pole 3, is because pole 3 offers symmetry slot 31, and is provided with a horizontal stripe 8 in sleeve 23, horizontal stripe 8 passes the symmetry slot 31 on pole 3 and is connected and fixed in sleeve 23, and one end of steel wire 6 to be connected on horizontal stripe 8 and to stretch out outside pole 3 after walking around pulley 4 along pole 3 inside, and the other end of steel wire 6 then connects leader 61.
More specifically, in order to realize above technical scheme better, the camber beam portion 22 of spring beam 2 should select has elastomeric arc steel bar, and the center of gravity of whole pole 3 and spring beam 2 also should should be no more than 1/2 of whole center shaft apart from delta wing 1 distance foremost below the center shaft of delta wing 1, in addition, the camber beam portion 22 of spring beam 2 goes out also to be provided with pedal 24 near sleeve 23.
Embodiment two
See Fig. 4, show the structural representation of another low latitude assistant sliding delta wing device of the utility model, the present embodiment two and embodiment one difference place are: set up a clubfoot beam 25 between sleeve 23 and bungee 5, two ends coupling bush 23 and the bungee 5 respectively of clubfoot beam 25, and clubfoot beam 25 is mutually concordant with camber beam portion 22, in addition, clubfoot beam 25 is provided with the first damping spring 26 and the second damping spring 27 vertically connecting camber beam portion 22 successively near sleeve 23 place; In addition, the auxiliary damping portion 9 be made up of connecting rod 91, bungee 5 and foot pad 7 is also provided with in the dead ahead of clubfoot beam 25, auxiliary damping portion 9 is with mutually concordant between clubfoot beam 25 and camber beam portion 22, and these all the other structures implementing two low-to-medium altitude assistant sliding delta wing devices are all identical with embodiment one.Low latitude assistant sliding delta wing device in the present embodiment two increases damping effect further by arranging clubfoot beam 25, makes the comfort of low latitude assistant sliding delta wing device when landing, and also can increase can jump degree simultaneously.
In addition, in order to make the low latitude assistant sliding delta wing device in this enforcement two have better result of use, this sleeve 23 can be chosen as a bearing, wherein the center of camber beam portion 22 connection bearing, the outer place of clubfoot beam 25 connection bearing, namely clubfoot beam 25 and camber beam portion 22 are for being flexibly connected.
Further, in the first damping spring 26 be connected between camber beam portion 22 and clubfoot beam 25 and the second damping spring 27, the size of the first damping spring 26 is greater than the second damping spring 27, namely the tension force of the first damping spring 26 is less than the second damping spring 27, thus makes the junction between camber beam portion 22 and clubfoot beam 25 have better damping effect.
In addition, as the further optimization of this enforcement, auxiliary angle angle between damping portion 9 and clubfoot beam 25 is set to 40 ° to 45 °, the object arranging angle is like this in order to ensure that low latitude assistant sliding delta wing device is when unbalanced landing, and affiliated auxiliary damping portion 9 can have certain correcting bullet role.If angle angle is greater than 45 ° of situations of toppling over before there will be, the due effect of out of reach, in addition, if angle too small will not have the effect of correcting, it can tilt together along with clubfoot beam 25.
In order to make to understand above technical scheme with those skilled in the art know that further, be further described to the principle of work of the utility model low latitude assistant sliding delta wing device 1 and using method below.First, on the pedal 24 that people stands in camber beam portion 22 and hand steered handle 61(this be people be the state of squatting), pull at handle 61 downwards to be moved along pole 3 top by sleeve 23 simultaneously, make camber beam portion 22 in the state of being squeezed, then stand fast and allow sleeve 23 slide with loosening steel wire 6, camber beam portion 22 can be restored to the original state, a power backward and downward power can be produced in the restorable process in camber beam portion 22, power backward makes whole delta wing 1 travel forward, simultaneously downward power extruding bungee 5, make to 1 one, delta wing power upwards, under the effect of two power, delta wing 1 will be upspring and under air is to the effect of delta wing 1, is kept the flight of certain hour aloft like this, when delta wing 1 is starting in the process declined, the people be positioned at above should continue to be cycled to repeat the process of drawing steel wire 6 and release steel wire 6, before landing, flight forward can be continued by the power in camber beam portion 22 to make delta wing 1.Be to be understood that, the flying height of the low latitude assistant sliding delta wing device 1 in the utility model is very limited, general about 5 meters, only be applicable to the flight entertainment doing low latitude, this is for safety factor on the one hand, on the other hand also relevant with its know-why, because it does not move by machine, so it can not maintain a higher height for a long time.
In sum, the utility model jumps the elastic force of beam as propulsion source by utilizing below the distortion in camber beam portion 22 and pole 3, what delta wing 1 can be able to be kept certain height under artificial manipulation slides, thus experiences to a kind of low latitude of circling in the air of people, has higher recreational.
Claims (6)
1. a low latitude assistant sliding delta wing device, it is characterized in that: comprise delta wing (1), spring beam (2), pole (3), bungee (5), pulley (4), steel wire (6) and foot pad (7), wherein, delta wing (1) to be spliced mutually with the second wing plate (12) by the first wing plate (11) and centered by phase stitching portion axle, spring beam (2) comprises crossbeam portion (21) and camber beam portion (22), crossbeam portion (21) becomes with delta wing (1) center shaft to be connected to a fixed abreast and the termination of crossbeam portion (21) withstands on delta wing (1) foremost, and camber beam portion (22) and crossbeam portion (21) are formed in one and are connected and the termination of camber beam portion (22) are also connected with a sleeve (23), a clubfoot beam (25) has been set up between sleeve (23) and bungee (5), two ends coupling bush (23) and the bungee (5) respectively of clubfoot beam (25), and clubfoot beam (25) is mutually concordant with camber beam portion (22), in addition, clubfoot beam (25) is provided with the first damping spring (26) and the second damping spring (27) that vertically connect camber beam portion (22) successively near sleeve (23) place, wherein, also be provided with in the dead ahead of clubfoot beam (25) by connecting rod (91), the auxiliary damping portion (9) that bungee (5) and foot pad (7) form, auxiliary damping portion (9) is with mutually concordant between clubfoot beam (25) and camber beam portion (22), pole (3) is set in sleeve (23) and its one end is vertically connected at crossbeam portion (21), the other end of pole (3) connects a bungee (5), pulley (4) is fixedly arranged on the junction in pole (3) and crossbeam portion (21), steel wire (6) is positioned over pole (3) inside and its one end is connected to sleeve (23), its other end is walked around pulley (4) and is connected leader (61) afterwards, foot pad (7) is connected to the bottom of bungee (5).
2. low latitude according to claim 1 assistant sliding delta wing device, is characterized in that: the size of the first damping spring (26) is greater than the second damping spring (27).
3. low latitude according to claim 1 assistant sliding delta wing device, it is characterized in that: sleeve (23) is a bearing, the center of camber beam portion (22) connection bearing, the outer place of clubfoot beam (25) connection bearing, clubfoot beam (25) and camber beam portion (22) are for being flexibly connected.
4. low latitude according to claim 1 assistant sliding delta wing device, is characterized in that: the camber beam portion (22) of spring beam (2) is for having elastomeric arc steel bar.
5. low latitude according to claim 1 assistant sliding delta wing device, is characterized in that: the center of gravity of whole pole (3) and spring beam (2) also should should be no more than 1/2 of whole center shaft apart from delta wing (1) distance foremost below the center shaft of delta wing (1).
6. low latitude according to claim 1 assistant sliding delta wing device, is characterized in that: in the camber beam portion (22) of spring beam (2), upper close sleeve (23) goes out also to be provided with pedal (24).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420375315.XU CN204056298U (en) | 2014-07-08 | 2014-07-08 | Low latitude assistant sliding delta wing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420375315.XU CN204056298U (en) | 2014-07-08 | 2014-07-08 | Low latitude assistant sliding delta wing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204056298U true CN204056298U (en) | 2014-12-31 |
Family
ID=52197861
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420375315.XU Expired - Fee Related CN204056298U (en) | 2014-07-08 | 2014-07-08 | Low latitude assistant sliding delta wing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204056298U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104890870A (en) * | 2015-05-28 | 2015-09-09 | 哈尔滨工程大学 | Hydroplaning delta wing with automatic flipping cover |
| CN104890869A (en) * | 2015-05-28 | 2015-09-09 | 哈尔滨工程大学 | Hydroplaning delta wing with automatic sliding cover |
| CN104890868B (en) * | 2015-05-28 | 2016-09-14 | 哈尔滨工程大学 | One enters water self-opening manpower plateau aircraft |
-
2014
- 2014-07-08 CN CN201420375315.XU patent/CN204056298U/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104890870A (en) * | 2015-05-28 | 2015-09-09 | 哈尔滨工程大学 | Hydroplaning delta wing with automatic flipping cover |
| CN104890869A (en) * | 2015-05-28 | 2015-09-09 | 哈尔滨工程大学 | Hydroplaning delta wing with automatic sliding cover |
| CN104890870B (en) * | 2015-05-28 | 2016-08-24 | 哈尔滨工程大学 | A kind of automatic cover-turning hydroplane dalta wing |
| CN104890868B (en) * | 2015-05-28 | 2016-09-14 | 哈尔滨工程大学 | One enters water self-opening manpower plateau aircraft |
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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: 20141231 Termination date: 20150708 |
|
| EXPY | Termination of patent right or utility model |