CN204726670U - A kind of flight instruments - Google Patents
A kind of flight instruments Download PDFInfo
- Publication number
- CN204726670U CN204726670U CN201520051056.XU CN201520051056U CN204726670U CN 204726670 U CN204726670 U CN 204726670U CN 201520051056 U CN201520051056 U CN 201520051056U CN 204726670 U CN204726670 U CN 204726670U
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- Prior art keywords
- air bag
- adapter sleeve
- hawser
- aviator
- flight instruments
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- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 claims abstract description 59
- 239000000463 material Substances 0.000 claims description 8
- 208000002925 dental caries Diseases 0.000 claims description 4
- 239000000203 mixture Substances 0.000 claims description 2
- 238000000034 method Methods 0.000 description 15
- 230000008569 process Effects 0.000 description 15
- 238000010586 diagram Methods 0.000 description 5
- 230000036541 health Effects 0.000 description 4
- 230000005484 gravity Effects 0.000 description 3
- 239000002775 capsule Substances 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008901 benefit Effects 0.000 description 1
- 210000000988 bone and bone Anatomy 0.000 description 1
- 230000006872 improvement Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
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Abstract
The utility model provides a kind of flight instruments, comprise air bag, a pair flapping wing, self-locking lock catch, for a pair control lever that aviator grips, controller, attaching parts, hawser, hawser draw off gear and adapter sleeve, air bag and adapter sleeve are tightly locked by self-locking lock catch and are connected, hawser draw off gear is located at air bag, controller is for controlling hawser folding and unfolding, hawser is used for the leg of air bag with aviator to bind mutually, air bag is rotationally connected by attaching parts and adapter sleeve, adapter sleeve is flexibly connected with flapping wing, one end of control lever is connected with flapping wing, a control lever in a pair control lever is located at by controller.The utility model adopts self-locking lock catch and hawser draw off gear control taking off of aviator and land, and makes aviator take off and more be conducive to operation and controlling when landing.
Description
Technical field
The utility model relates to extreme sport clothing arts, in particular to a kind of flight instruments.
Background technology
Can fly on high as small bird is the dream of the mankind for a long time, various aircraft is out manufactured based on this dream, the kind of aircraft has a lot, such as hot gas capsule, bionical flight instruments, some aircraft may be used for sports, the object can reach entertainment life, improving the health, and be one of most challenge and irritating sports instantly with flight instruments flight.
In the prior art, aviator commonly uses hawser and health and air bag is bound, and instigates flapping wing, thus realize flight, because the volume of air bag is excessive, aviator is when using flight instruments to do extreme flight motion, all more difficult when taking off and land, and be unfavorable for controlling in the process of flight.
Utility model content
In view of this, the utility model provides a kind of flight instruments, with improve aviator use flight instruments do extreme flight motion time, take off landing time difficulty and flight course in be unfavorable for control problem.For achieving the above object, the utility model provides following technical scheme:
A kind of flight instruments, comprise air bag, a pair flapping wing, self-locking lock catch, for a pair control lever that aviator grips, controller, hawser, attaching parts, hawser draw off gear and adapter sleeve, described self-locking lock catch comprises lug boss and concave part, described lug boss is located at described adapter sleeve, described concave part is located at described air bag, described air bag and described adapter sleeve are tightly locked by described self-locking lock catch and are connected, described hawser draw off gear is located at described air bag, described controller is for controlling the folding and unfolding of described hawser, described hawser is used for the leg of described air bag with aviator to bind mutually, described air bag is rotationally connected by described attaching parts and described adapter sleeve, described adapter sleeve is flexibly connected with described flapping wing, one end of described control lever is connected with described flapping wing, a described control lever in a pair control lever is located at by described controller.
Preferably, described hawser draw off gear is remote control electric capstan winch, and described controller is the controller controlling described remote control electric capstan winch.Adopting remote control electric capstan winch, avoid tractive electric wire, reducing the obstruction of aviator when flying simultaneously.
Preferably, described attaching parts is rotating shaft, and one end of described rotating shaft is fixedly connected with described air bag, and the other end of described rotating shaft is fixedly connected with described adapter sleeve, the length of described rotating shaft, for when aviator is in standing state, makes described air bag higher than the length on the crown of aviator.Be arranged on this flight instruments like this when taking off and land, avoid because air bag volume is excessive, be unfavorable for that aviator takes off and landing.
Preferably, described flight instruments also comprises fixed cover and support frame, and described fixed cover is located at described air bag, and described fixed cover is sheathed on outside described support frame, and described self-locking lock catch be used for by described fixed cover with described be connected to be locked lock.This flight instruments is loaded onto support frame, air bag can be prevented to be out of shape in the process of flight.
Preferably, described fixed cover is provided with two holes, and described rotating shaft is fixedly connected with described support frame by described hole, and described hawser draw off gear is located at described support frame, and described hawser is through described hole.Rotating shaft is connected with support frame and has more stability, and in the process of flight not fragile fixed cover.
Preferably, the shape of described adapter sleeve is vest shape, described adapter sleeve is primarily of two braces, two pieces of sternites and one piece of tergite composition, described sternite is hinged with described tergite respectively, between described sternite, snap close connects, and described braces is connected with described tergite and sternite snap close respectively, and described flapping wing is fixedly connected with described braces, and with the axis of adapter sleeve for axis of symmetry, the point of connection of described flapping wing and described braces is symmetric.The shape of adapter sleeve is set to vest shape, flapping wing is symmetrical, the outward appearance of this flight instruments can be beautified, and more convenient to operate.
Preferably, described air bag is spliced by least two cavitys.Be arranged so that like this air bag fly process in one of them cavity break time, air bag also has certain buoyancy, make aviator flight process in there is certain safety.
Preferably, described flapping wing adopts Universal connector to be connected with the connection mode of described adapter sleeve.Adopt Universal connector to be connected flapping wing and adapter sleeve, make flapping wing can be movable up and down in the process of flight, be conducive to the control of aviator to heading.
Preferably, the material that described support frame adopts is light material.Support frame adopts light material to make, and decreases total heavy burden of this flight instruments, and aviator can be made laborsaving in the process of flight.
Relative to prior art, the utility model comprises following beneficial effect: the utility model adopts self-locking lock catch and hawser draw off gear control taking off of aviator and land, and makes aviator take off and more be conducive to operation and controlling when landing.
Accompanying drawing explanation
For making the object of the utility model embodiment, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in the utility model embodiment, technical scheme in the utility model embodiment is clearly and completely described, obviously, described embodiment is the utility model part embodiment, instead of whole embodiments.The assembly of the utility model embodiment describing and illustrate in usual accompanying drawing herein can be arranged with various different configuration and design.Therefore, below to the detailed description of the embodiment of the present utility model provided in the accompanying drawings and the claimed scope of the present utility model of not intended to be limiting, but selected embodiment of the present utility model is only represented.Based on the embodiment in the utility model, those of ordinary skill in the art are not making the every other embodiment obtained under creative work prerequisite, all belong to the scope of the utility model protection.
Fig. 1 is the application schematic diagram of aviator that the utility model embodiment one provides flight instruments when being in state of flight;
Fig. 2 is that aviator that the utility model embodiment one provides is when being in standing state and the application schematic diagram of flight instruments;
Fig. 3 is the application schematic diagram of aviator that the utility model embodiment two provides flight instruments when being in state of flight;
Fig. 4 is the application schematic diagram of aviator that the utility model embodiment two provides flight instruments when being in standing state;
Fig. 5 be the utility model embodiment two provide fixed cover, support frame, rotating shaft, remote control electric capstan winch position relationship schematic diagram;
Fig. 6 is the structural representation of the self-locking lock catch that the utility model provides;
Fig. 7 is the structural representation of the adapter sleeve that the utility model provides;
Fig. 8 is the structural representation of the control lever that the utility model provides.
Wherein, the corresponding relation between Reference numeral and component names is as follows: air bag 101; Flapping wing 102; Self-locking lock catch 103; Control lever 104; Rotating shaft 105; Adapter sleeve 106; Hawser 107; Remote control electric capstan winch 108; Hole 109; Fixed cover 110; Support frame 111; Remote control electric capstan winch switch 112; Sternite 113; Tergite 114; Braces 115.
Detailed description of the invention
Can fly on high as small bird is the dream of the mankind for a long time, various aircraft is out manufactured based on this dream, the kind of aircraft has a lot, such as hot gas capsule, bionical flight instruments, some aircraft may be used for sports, the object can reach entertainment life, improving the health, and to carry out sporting flying with flight instruments be one of most challenge and irritating sports instantly.
In the prior art, aviator commonly uses hawser and health and air bag is bound, and instigates flapping wing simultaneously thus realizes flight, because the volume of air bag is excessive, when aviator uses during flight instruments flight, all more difficult when taking off and land, be unfavorable for controlling in the process of flight.
In view of upper kind situation, contriver, through a large amount of research and practices, provides a kind of flight instruments.This flight instruments comprises air bag, a pair flapping wing, adapter sleeve, self-locking lock catch, a pair control lever, controller, hawser, the hawser draw off gear that grip for aviator, air bag and adapter sleeve are rotationally connected, self-locking lock catch is used for air bag to lock with being connected to be locked, hawser is used for the leg of air bag with aviator to bind mutually, controller is the device for controlling hawser folding and unfolding, described adapter sleeve is flexibly connected with described flapping wing, and one end of described control lever is connected with described flapping wing.
When using this flight instruments, adapter sleeve is placed on upper body by aviator, and bind with by hawser and leg, the both hands of aviator hold control lever, and press controller buttons, hawser draw off gear starts to shrink hawser and the leg of aviator and air bag is adjacent to, at this moment the waist of aviator upwards exerts a force, self-locking lock catch is locked, aviator instigates flapping wing to make this device produce buoyancy up and down simultaneously, and air bag itself can produce buoyancy, when the buoyancy that both produce is greater than the gravity that aviator and flight instruments produce, can fly.
Also by reference to the accompanying drawings the utility model is described in further detail below by specific embodiment.
Fig. 1, Fig. 2 shows a kind of flight instruments that the utility model embodiment one provides, this flight instruments comprises air bag 101, a pair flapping wing 102, self-locking lock catch 103, a pair control lever 104, hawser 107, hawser draw off gear, and adapter sleeve 106, described adapter sleeve 106 adopts Universal connector to be connected with described flapping wing 102, described self-locking lock catch 103 comprises lug boss and concave part, as Fig. 6, described lug boss is located at described adapter sleeve 106, described concave part is located at described air bag 102, described hawser draw off gear is remote control electric capstan winch 108, described remote control electric capstan winch comprises remote control electric capstan winch switch 112, natch, described hawser draw off gear is not limited only to remote control electric capstan winch 108, also can substitute with hand winch or the replacement of some other hawser draw off gear.Described air bag 101 is located at by described remote control electric capstan winch 108, as Fig. 1, one end of described hawser 107 is located in described remote control electric capstan winch 108, leg with aviator is bound by the other end of described hawser 107 mutually, described flight instruments comprises attaching parts, described attaching parts is rotating shaft 105, described air bag 101 is rotationally connected with described adapter sleeve 106 by described rotating shaft 105, the length of described rotating shaft 105 is for when aviator is in standing state, make described air bag 101 higher than the length on the crown of aviator, be arranged on this flight instruments like this when taking off and land, avoid because air bag 101 volume is excessive, be unfavorable for that aviator takes off and landing, natch, described attaching parts is not limited only to rotating shaft, also of a rotating shaft rotation wall hawser can be substituted or some other attaching parts that can realize that adapter sleeve 106 and air bag 101 are rotationally connected.Described control lever 104, as Fig. 8, one end be connected with described flapping wing 102, a described remote control electric capstan winch switch 112 described control lever 104 located therein.
When using this flight instruments, adapter sleeve 106 is through at upper body by aviator, and bind with by hawser 107 and leg, the both hands of aviator hold control lever 104, and press remote control electric capstan winch switch 112 button, remote control electric capstan winch 108 starts to shrink hawser 107 and the leg of aviator and air bag 101 is adjacent to, at this moment the waist of aviator upwards exerts a force, self-locking lock catch 103 is locked, aviator instigates flapping wing 102 to make this flight instruments produce buoyancy up and down simultaneously, and air bag 101 itself can produce buoyancy, when the buoyancy that both produce is greater than the gravity that aviator and flight instruments produce, can fly.
In the present embodiment, the shape of described adapter sleeve 106 is vest shape, described adapter sleeve 106 forms primarily of two braces, 115, two pieces of sternites 113 and one block of tergite 114, described sternite 113 is hinged with described tergite 114 respectively, between described sternite 113, snap close connects, as Fig. 7, described braces 115 is connected with described sternite 113 and tergite 114 snap close respectively, the point of connection of described flapping wing 102 and described braces 115 with the axis of adapter sleeve 106 for axis of symmetry is symmetric.By symmetrical for flapping wing 102, the outward appearance of this flight instruments can be beautified, and more convenient to operate.
Fig. 3, Fig. 4, Fig. 5 show a kind of flight instruments that the utility model embodiment two provides.This flight instruments comprises air bag 101, a pair flapping wing 102, self-locking lock catch 103, a pair control lever 104, hawser 107, remote control electric capstan winch, remote control electric capstan winch switch 112, fixed cover 110, support frame 111 and adapter sleeve 106, described fixed cover 110 is located at described air bag 101, described fixed cover 110 is sheathed on outside described support frame 111, this flight instruments is loaded onto support frame 111, air bag 101 can be prevented to be out of shape in the process of flight.Described flapping wing 102 adopts Universal connector to be connected with described adapter sleeve 106, described self-locking lock catch 103 comprises lug boss and concave part, as Fig. 6, described lug boss is located at described adapter sleeve 106, described concave part is located at described fixed cover 110, described flight instruments comprises rotating shaft 105, described fixed cover 110 is provided with two holes 109, one end of described rotating shaft 105 is fixedly connected with described support frame 111 by described hole 109, the other end of described rotating shaft 105 is fixedly connected with described adapter sleeve 106, rotating shaft 105 has more stability with the connection of support frame 111, not fragile fixed cover 110 in the process of flight, the length of described rotating shaft 105 is for when aviator is in standing state, make described air bag 101 higher than the length on the crown of aviator, be arranged on this flight instruments like this when taking off and land, avoid because air bag 101 volume is excessive, be unfavorable for that aviator takes off and landing.Described support frame 111 is located at by described remote control electric capstan winch 108, one end of described hawser 107 is located in described remote control electric capstan winch 108, the other end of described hawser 107 is bound with the leg of aviator mutually through described hole 109, one end of described control lever 104 is connected with described flapping wing 102, a described remote control electric capstan winch switch 112 described control lever 104 located therein.
When using this flight instruments, adapter sleeve 106 is through at upper body by aviator, and bind with by hawser 107 and leg, the both hands of aviator hold control lever 104, and press remote control electric capstan winch switch 112 button, remote control electric capstan winch 108 starts to shrink hawser 107 and the leg of aviator and air bag 101 is adjacent to, at this moment the waist of aviator upwards exerts a force, self-locking lock catch 103 is locked, aviator instigates flapping wing 102 to make this device produce buoyancy up and down simultaneously, and air bag 101 itself can produce buoyancy, when the buoyancy that both produce is greater than the gravity that aviator and flight instruments produce, can fly.
In the present embodiment, described air bag 101 is spliced by least two cavitys.Be arranged so that like this air bag 101 fly process in one of them cavity break time, air bag 101 also has certain buoyancy, make aviator flight process in there is certain safety.
In the present embodiment, the material that described support frame 111 adopts is light material.Support frame 111 adopts light material to make, and decreases total heavy burden of this flight instruments, and aviator can be made laborsaving in the process of flight.
In the present embodiment, the shape of described adapter sleeve 106 is vest shape, as Fig. 7, described adapter sleeve 106 forms primarily of two braces, 115, two pieces of sternites 113 and one block of tergite 114, described sternite 113 is hinged with described tergite 114 respectively, between described sternite 113, snap close connects, described braces 115 is connected with described sternite 113 and tergite 114 snap close respectively, described flapping wing 102 is fixedly connected with described braces 115, and with the axis of adapter sleeve 106 for axis of symmetry, described flapping wing 102 is symmetric with the point of connection of described braces 115.Flapping wing is symmetrical, the outward appearance of this flight instruments can be beautified, and more convenient to operate.
In the present embodiment, described air bag 101 is spliced by least two cavitys.Be arranged so that like this air bag 101 fly process in one of them cavity break time, air bag 101 also has certain buoyancy, ensure that aviator flight process in safety.
In the present embodiment, described support frame 111 is the intersecting parallels skeleton that four bone bar bolts are formed by connecting.Intersecting parallels skeleton has good fixation, and it is a kind of common mode that removably connects that bolt connects, practical.
The foregoing is only preferred embodiment of the present utility model, be not limited to the utility model, for a person skilled in the art, the utility model can have various modifications and variations.All within spirit of the present utility model and principle, any amendment done, equivalent replacement, improvement etc., all should be included within protection domain of the present utility model.
Claims (9)
1. a flight instruments, it is characterized in that, comprise air bag, a pair flapping wing, self-locking lock catch, for a pair control lever that aviator grips, controller, attaching parts, hawser, hawser draw off gear and adapter sleeve, described self-locking lock catch comprises lug boss and concave part, described lug boss is located at described adapter sleeve, described concave part is located at described air bag, described air bag and described adapter sleeve are tightly locked by described self-locking lock catch and are connected, described hawser draw off gear is located at described air bag, described controller is for controlling the folding and unfolding of described hawser, described hawser is used for the leg of described air bag with aviator to bind mutually, described air bag is rotationally connected by described attaching parts and described adapter sleeve, described adapter sleeve is flexibly connected with described flapping wing, one end of described control lever is connected with described flapping wing, a described control lever in a pair control lever is located at by described controller.
2. flight instruments according to claim 1, it is characterized in that, described hawser draw off gear is remote control electric capstan winch, and described controller is the controller controlling described remote control electric capstan winch.
3. flight instruments according to claim 1, it is characterized in that, described attaching parts is rotating shaft, one end of described rotating shaft is fixedly connected with described air bag, the other end of described rotating shaft is fixedly connected with described adapter sleeve, the length of described rotating shaft, for when aviator is in standing state, makes described air bag higher than the length on the crown of aviator.
4. flight instruments according to claim 3, it is characterized in that, described flight instruments also comprises fixed cover and support frame, described fixed cover is located at described air bag, described fixed cover is sheathed on outside described support frame, and described self-locking lock catch be used for by described fixed cover with described be connected to be locked lock.
5. flight instruments according to claim 4, is characterized in that, described fixed cover is provided with two holes, and described rotating shaft is fixedly connected with described support frame by described hole, and described hawser draw off gear is located at described support frame, and described hawser is through described hole.
6. flight instruments according to claim 1, it is characterized in that, the shape of described adapter sleeve is vest shape, described adapter sleeve is primarily of two braces, two pieces of sternites and one piece of tergite composition, and described sternite is hinged with described tergite respectively, and between described sternite, snap close connects, described braces is connected with described sternite and tergite snap close respectively, described flapping wing is fixedly connected with described braces, and with the axis of described adapter sleeve for axis of symmetry, the point of connection of described flapping wing and described braces is symmetric.
7. flight instruments according to claim 1, is characterized in that, described air bag is spliced by least two cavitys.
8. flight instruments according to claim 1, is characterized in that, described flapping wing and described adapter sleeve adopt Universal connector to be connected.
9. flight instruments according to claim 4, is characterized in that, the material that described support frame adopts is light material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520051056.XU CN204726670U (en) | 2015-01-26 | 2015-01-26 | A kind of flight instruments |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520051056.XU CN204726670U (en) | 2015-01-26 | 2015-01-26 | A kind of flight instruments |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204726670U true CN204726670U (en) | 2015-10-28 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520051056.XU Expired - Fee Related CN204726670U (en) | 2015-01-26 | 2015-01-26 | A kind of flight instruments |
Country Status (1)
| Country | Link |
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| CN (1) | CN204726670U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106945813A (en) * | 2017-04-02 | 2017-07-14 | 王庆翠 | A kind of manned method that balloon of utilization aerostatic buoyancy is combined with flapping-wing aircraft |
-
2015
- 2015-01-26 CN CN201520051056.XU patent/CN204726670U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106945813A (en) * | 2017-04-02 | 2017-07-14 | 王庆翠 | A kind of manned method that balloon of utilization aerostatic buoyancy is combined with flapping-wing 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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151028 |