CN207157569U - Emission system that flapping-wing aircraft takes off launcher and flapping-wing aircraft takes off - Google Patents
Emission system that flapping-wing aircraft takes off launcher and flapping-wing aircraft takes off Download PDFInfo
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- CN207157569U CN207157569U CN201721071956.6U CN201721071956U CN207157569U CN 207157569 U CN207157569 U CN 207157569U CN 201721071956 U CN201721071956 U CN 201721071956U CN 207157569 U CN207157569 U CN 207157569U
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- flapping
- wing aircraft
- launcher
- takes
- trusses
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Abstract
Vehicle technology field is the utility model is related to, launcher is taken off more particularly, to a kind of flapping-wing aircraft and flapping-wing aircraft takes off emission system.The flapping-wing aircraft takes off launcher, including travel mechanism, rail mechanism and haulage gear；Travel mechanism is arranged on rail mechanism, and haulage gear is used to make travel mechanism slide on rail mechanism；Travel mechanism is used to carry flapping-wing aircraft, wherein, travel mechanism includes mobile base and the lifting support being installed in mobile base, and lifting support is used to support flapping-wing aircraft, and lifting support can adjust the angle of pitch of flapping-wing aircraft.The flapping-wing aircraft takes off emission system, including described flapping-wing aircraft takes off launcher.The utility model can reduce appropriation of land, reduce construction cost.
Description
Technical field
Vehicle technology field is the utility model is related to, is risen more particularly, to a kind of take off launcher and flapping-wing aircraft of flapping-wing aircraft
Fly emission system.
Background technology
Flapping-wing aircraft is also known as ornithopter, refers to the aviation for overweighting air that wing can flutter up and down as bird and insect wing
Device, the wing fluttered (also referred to as flapping wing) not only produce lift, also produce motive force forward.Existing flapping-wing aircraft when taking off,
Longer runway is needed, to make flapping-wing aircraft disclosure satisfy that takeoff speed, and longer runway means that needs take more
More soils, and also add the construction cost of runway.
Utility model content
The purpose of this utility model is to provide a kind of flapping-wing aircraft and taken off launcher, to solve to flutter present in prior art
The runway occupation of land of wing machine is more, and also add the technical problem of the construction cost of runway.
The utility model provides a kind of flapping-wing aircraft and taken off launcher, including travel mechanism, rail mechanism and haulage gear；
The travel mechanism is arranged on the rail mechanism, and the haulage gear is used to make the travel mechanism in the rail mechanism
On slide；The travel mechanism is used to carry flapping-wing aircraft,
Wherein, the travel mechanism includes mobile base and the lifting support being installed in the mobile base, the liter
Descending branch frame is used to support the flapping-wing aircraft, and the lifting support can adjust the angle of pitch of the flapping-wing aircraft.
Further, the mobile base includes main chassis；The main chassis includes first that two parallel intervals are set
Trusses, and the second trusses that two parallel intervals are set；One end of second trusses and wherein first trusses
It is fixedly connected, the other end of second trusses is fixedly connected with another first trusses；On two first trusses
It is respectively and fixedly provided with multiple first rollers.
Further, the mobile base also includes stable frame, and the stable frame is fixedly connected with the main chassis,
And the second roller and the 3rd roller are provided with the stable frame, second roller is located at the length direction of the main chassis
Side, the 3rd roller is located at the opposite side of the length direction of the main chassis；The length direction of first trusses with
The length direction of the main chassis is parallel.
Further, the lifting support includes the support component that two parallel intervals are set；The support component includes
Support vertical pole and Extensible upright rod；The support vertical pole is connected with the Extensible upright rod, and the flexible of the Extensible upright rod can be adjusted
Save the angle of pitch of the support vertical pole.
Further, the rail mechanism includes the dragging track that more parallel intervals are set, and described for supporting
The track chassis of dragging track.
Further, the haulage gear includes hoist engine；One end of the rope of the hoist engine and the mobile base
It is fixedly connected.
Further, the rail mechanism also includes Stairs, and the Stairs are arranged at the length of the track chassis
The one end in direction.
Further, stop mechanism is provided with the track chassis, for carrying out locking or solution to the travel mechanism
Lock.
The utility model additionally provides a kind of flapping-wing aircraft and taken off emission system, including described flapping-wing aircraft takes off launcher.
Further, in addition to power transport vehicle.
Compared with prior art, the beneficial effects of the utility model are：
Flapping-wing aircraft provided by the utility model takes off launcher, including travel mechanism, rail mechanism and haulage gear；It is mobile
Mechanism is arranged on rail mechanism, and haulage gear is used to make travel mechanism slide on rail mechanism；Travel mechanism is used to carry
Flapping-wing aircraft, wherein, travel mechanism includes mobile base and the lifting support being installed in mobile base, and lifting support is used to support
Flapping-wing aircraft, and lifting support can adjust the angle of pitch of flapping-wing aircraft.Travel mechanism is set to be slided on rail mechanism by haulage gear
OK, just flapping-wing aircraft can so be accelerated when flapping-wing aircraft is installed in travel mechanism, makes flapping-wing aircraft in the mechanism that de-orbits
When speed, disclosure satisfy that takeoff speed, can so shorten distance of taking off, and appropriation of land can be reduced, reduce
Construction cost, but also possibility is provided for the take off mobility of launcher of flapping-wing aircraft, the optimization for being advantageous to land resource is matched somebody with somebody
Put.
The flapping-wing aircraft that the utility model also provides takes off emission system, including described flapping-wing aircraft takes off launcher.It is based on
Above-mentioned analysis understands that flapping-wing aircraft emission system of taking off can reduce appropriation of land, reduces construction cost, but also to flutter
The take off mobility of launcher of wing machine provides possibility, is advantageous to distributing rationally for land resource.
Brief description of the drawings
, below will be right in order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art
The required accompanying drawing used is briefly described in embodiment or description of the prior art, it should be apparent that, describe below
In accompanying drawing be some embodiments of the present utility model, for those of ordinary skill in the art, do not paying creativeness
On the premise of work, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is the structural representation for the flapping-wing aircraft launcher that the utility model embodiment one provides；
Fig. 2 is the close-up schematic view at A in Fig. 1；
Fig. 3 is the close-up schematic view at B in Fig. 1；
Fig. 4 is the close-up schematic view at C in Fig. 1；
Fig. 5 is the structural representation of travel mechanism in the utility model embodiment one.
In figure：
The trusses of 501- first；The trusses of 502- second；The rollers of 503- first；
The rollers of 504- second；The rollers of 505- the 3rd；506- auxiliary girders；
507- diagonal beams；508- supports vertical pole；509- Extensible upright rods；
510- dragging tracks；511- Stairs；512- inclined ramps；
513- protective buffering pads；514- hoist engines；515- ropes；
516- fixed pulleys；517- track chassis；518- flapping-wing aircrafts.
Embodiment
The technical solution of the utility model is clearly and completely described below in conjunction with accompanying drawing, it is clear that described
Embodiment is the utility model part of the embodiment, rather than whole embodiments.
Component generally here described in accompanying drawing with the utility model embodiment shown can be with a variety of
Configure to arrange and design.Therefore, the detailed description of the embodiment of the present utility model to providing in the accompanying drawings is not purport below
In the claimed the scope of the utility model of limitation, but it is merely representative of selected embodiment of the present utility model.
Based on the embodiment in the utility model, those of ordinary skill in the art are not under the premise of creative work is made
The every other embodiment obtained, belong to the scope of the utility model protection.
, it is necessary to explanation in description of the present utility model, term " " center ", " on ", " under ", it is "left", "right", " perpendicular
Directly ", the orientation of the instruction such as " level ", " interior ", " outer " or position relationship are based on orientation shown in the drawings or position relationship, are only
For the ease of description the utility model and simplified description, rather than indicate or imply that signified device or element must be with special
Fixed orientation, with specific azimuth configuration and operation, therefore it is not intended that to limitation of the present utility model.In addition, term " the
One ", " second ", " the 3rd " are only used for describing purpose, and it is not intended that instruction or hint relative importance.
, it is necessary to which explanation, unless otherwise clearly defined and limited, term " are pacified in description of the present utility model
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected or be detachably connected, or integratedly
Connection；Can be mechanical connection or electrical connection；Can be joined directly together, can also be indirectly connected by intermediary,
It can be the connection of two element internals.For the ordinary skill in the art, above-mentioned art can be understood with concrete condition
Concrete meaning of the language in the utility model.
Embodiment one
Fig. 1 is the structural representation for the flapping-wing aircraft launcher that the utility model embodiment one provides；Fig. 2 is in Fig. 1 at A
Close-up schematic view；Fig. 3 is the close-up schematic view at B in Fig. 1；Fig. 4 is the close-up schematic view at C in Fig. 1；Figure
5 be the structural representation of travel mechanism in the utility model embodiment one, referring to shown in Fig. 1 to Fig. 5, the utility model embodiment
One, which provides a kind of flapping-wing aircraft, takes off launcher, including travel mechanism, rail mechanism and haulage gear；Travel mechanism is arranged at rail
In road mechanism, haulage gear is used to make travel mechanism slide on rail mechanism；Travel mechanism is used to carry flapping-wing aircraft 518, its
In, travel mechanism includes mobile base and the lifting support being installed in mobile base, and lifting support is used to support flapping-wing aircraft, and
Lifting support can adjust the angle of pitch of flapping-wing aircraft, that is to say, that change fuselage axial direction and the folder of horizontal direction of flapping-wing aircraft
The size of angle.
Specifically, flapping-wing aircraft is positioned in travel mechanism, mobile after travel mechanism is slided to the end of rail mechanism
Mechanism is positioned over the flapping-wing aircraft in travel mechanism and possesses takeoff speed because inertia de-orbits mechanism, and starts to vibrate
Flapping wing, so as to realize lift-off.
The flapping-wing aircraft that the embodiment provides takes off launcher, by haulage gear make travel mechanism on rail mechanism it is sliding
OK, just flapping-wing aircraft can so be accelerated when flapping-wing aircraft is installed in travel mechanism, makes flapping-wing aircraft in the mechanism that de-orbits
When speed, disclosure satisfy that takeoff speed, can so shorten distance of taking off, and appropriation of land can be reduced, reduce
Construction cost, but also possibility is provided for the take off mobility of launcher of flapping-wing aircraft, the optimization for being advantageous to land resource is matched somebody with somebody
Put.
In the optional scheme of the embodiment, mobile base includes main chassis；Main chassis includes what two parallel intervals were set
First trusses 501, and the second trusses 502 that two parallel intervals are set, two first trusses 501 and two second trusses
502 form rectangular frame structure；One end of second trusses 502 is fixedly connected with wherein first trusses 501, the second trusses 502
The other end be fixedly connected with another first trusses 501；Multiple first rollers 503 are respectively and fixedly provided with two first trusses 501,
Travel mechanism is set to be slided along the length direction of rail mechanism by the first rolling rolled.
Specifically, the length direction of the first trusses 501 is parallel with the length direction of rail mechanism；Second trusses 502
Length direction and rail mechanism length direction it is perpendicular.
In the optional scheme of the embodiment, mobile base also includes stable frame, and stable frame is fixedly connected with main chassis,
And the second roller 504 and the 3rd roller 505 are provided with stable frame, the second roller 504 is located at the length direction of main chassis
Side, the 3rd roller 505 are located at the opposite side of the length direction of main chassis；The length direction of first trusses 501 and main chassis
Length direction is parallel.
Specifically, stable frame includes four auxiliary girders 506 and diagonal beam 507；Diagonal beam 507 and rail mechanism
Length direction it is perpendicular, and diagonal beam 507 is fixedly connected with the first trusses 501；One end of wherein two auxiliary girders 506 with
One end of diagonal beam 507 is fixedly connected, and one end of two auxiliary girders 506 is fixed with the other end of diagonal beam 507 and connected in addition
Connect.The middle part of diagonal beam 507 offers jack.
In the optional scheme of the embodiment, lifting support includes the support component that two parallel intervals are set；Support component
Including support vertical pole 508 and Extensible upright rod 509；Support vertical pole 508 is connected with Extensible upright rod 509, and Extensible upright rod 509 is stretched
The angle of pitch of support vertical pole 508 can be adjusted, that is, realizes the angle of pitch of regulation flapping-wing aircraft.
Specifically, in each support component, the quantity of support vertical pole 508 is one, and the quantity of Extensible upright rod 509 is two
Root.Extensible upright rod 509 supports the length direction of vertical pole 508 flexible parallel to two perpendicular to the plane where rectangular frame structure
Plane where vertical rod 509.Extensible upright rod 509 includes two poles, and one of pole is plugged on another pole, and
It is locked between two poles are realized by adjusting tight screw, that is, adjusts the flexible of Extensible upright rod 509.Two support vertical poles 508
For supporting the fuselage of flapping-wing aircraft.
In the optional scheme of the embodiment, rail mechanism includes the dragging track 510, Yi Jiyong that more parallel intervals are set
In the track chassis 517 of support dragging track 510.
Specifically, the quantity of dragging track 510 is 4.The first roller 503 is wherein placed on two dragging tracks 510；
Another two dragging tracks 510 place the second roller 504 and the 3rd roller 505 respectively.Dragging track 510 is located at the top of track chassis
Portion, the height of track chassis are more than the height of flapping-wing aircraft.
In the optional scheme of the embodiment, rail mechanism also includes Stairs 511, and Stairs 511 are arranged at track chassis
Length direction one end, i.e. track chassis initiating terminal, by Stairs 511 so that personnel can arrive the top of track chassis
Portion.When flapping-wing aircraft takes off, flown from the end of track chassis.The initiating terminal of track chassis is additionally provided with inclined ramp 512, for making
Flapping-wing aircraft reaches the dragging track 510 at the top of track chassis along inclined ramp 512.Also set up in front of the end of track chassis
There is protective buffering pad 513.
In the optional scheme of the embodiment, stop mechanism is provided with track chassis, for carrying out locking to travel mechanism
Or unblock, stop mechanism is electric mortise lock, and electric mortise lock can be inserted in the jack at the middle part of diagonal beam 507, to realize to moving machine
Structure carries out locking.
In the optional scheme of the embodiment, haulage gear includes hoist engine；One end of the rope of hoist engine and mobile base
It is fixedly connected.Hoisting machine is located at the bottom of the end of track chassis.Fixed pulley, elevator are installed at the top of the end of track chassis
The rope 515 of machine 514 drives fixed pulley 516 to move, and installation fixed pulley can prevent the rope of hoist engine from being ground by track chassis
Damage.
Embodiment two
The utility model embodiment two additionally provides a kind of flapping-wing aircraft and taken off emission system, including the flutterring of providing of embodiment one
Wing machine takes off launcher.
Flapping-wing aircraft emission system of taking off also includes controlling switch, for controlling being turned on and off for hoist engine, and electric mortiser
Lock is turned on and off.It should be noted that electric mortise lock is mainly used in preventing travel mechanism from accident occurs in dragging track 510
Slide；Therefore when launching flapping-wing aircraft, it is necessary to first power off electric mortise lock, the dead bolt of electric mortise lock is retracted, so that travel mechanism can be certainly
By moving.
Embodiment three
Flapping-wing aircraft in the utility model embodiment three emission system of taking off is improvement on the basis of embodiment two, is implemented
Technology contents not repeated description disclosed in example two, the disclosure of embodiment two fall within the disclosure of the present embodiment two.
In the embodiment three, flapping-wing aircraft emission system of taking off also includes power transport vehicle；Flapping-wing aircraft take off launcher installation
Taken off the removable of launcher on power transport vehicle, being so easy to implement flapping-wing aircraft, the transmitting of such flapping-wing aircraft is not just by solid
Determine the restriction of runway.
Finally it should be noted that：Various embodiments above is only to illustrate the technical solution of the utility model, rather than it is limited
System；Although the utility model is described in detail with reference to foregoing embodiments, one of ordinary skill in the art should
Understand：It can still modify to the technical scheme described in foregoing embodiments, either to which part or whole
Technical characteristic carries out equivalent substitution；And these modifications or replacement, the essence of appropriate technical solution is departed from this practicality newly
The scope of each embodiment technical scheme of type.In addition, it will be appreciated by those of skill in the art that although some realities described herein
Applying example includes some features included in other embodiments rather than further feature, but the combination of the feature of different embodiments
Mean within the scope of the utility model and form different embodiments.For example, in the following claims,
The one of any of embodiment claimed mode can use in any combination.
Claims (10)
- The launcher 1. a kind of flapping-wing aircraft takes off, it is characterised in that including travel mechanism, rail mechanism and haulage gear；The shifting Motivation structure is arranged on the rail mechanism, and the haulage gear is used to make the travel mechanism sliding on the rail mechanism OK；The travel mechanism is used to carry flapping-wing aircraft,Wherein, the travel mechanism includes mobile base and the lifting support being installed in the mobile base, the lifting branch Frame is used to support the flapping-wing aircraft, and the lifting support can adjust the angle of pitch of the flapping-wing aircraft.
- The launcher 2. flapping-wing aircraft according to claim 1 takes off, it is characterised in that the mobile base includes main chassis； The main chassis includes the first trusses that two parallel intervals are set, and the second trusses that two parallel intervals are set；It is described One end of second trusses is fixedly connected with wherein one first trusses, the other end of second trusses with another described in First trusses is fixedly connected；Multiple first rollers are respectively and fixedly provided with two first trusses.
- The launcher 3. flapping-wing aircraft according to claim 2 takes off, it is characterised in that the mobile base also includes shakeless deckle Frame, the stable frame is fixedly connected with the main chassis, and the second roller and the 3rd roller are provided with the stable frame, Second roller is located at the side of the length direction of the main chassis, and the 3rd roller is located at the length side of the main chassis To opposite side；The length direction of first trusses is parallel with the length direction of the main chassis.
- The launcher 4. flapping-wing aircraft according to any one of claim 1-3 takes off, it is characterised in that the lifting support bag Include the support component that two parallel intervals are set；The support component includes support vertical pole and Extensible upright rod；The support vertical pole It is connected with the Extensible upright rod, the flexible angle of pitch that can adjust the support vertical pole of the Extensible upright rod.
- The launcher 5. flapping-wing aircraft according to any one of claim 1-3 takes off, it is characterised in that the rail mechanism bag The dragging track that more parallel intervals are set is included, and for supporting the track chassis of the dragging track.
- The launcher 6. flapping-wing aircraft according to any one of claim 1-3 takes off, it is characterised in that the haulage gear bag Include hoist engine；One end of the rope of the hoist engine is fixedly connected with the mobile base.
- The launcher 7. flapping-wing aircraft according to claim 5 takes off, it is characterised in that the rail mechanism also includes walking Ladder, the Stairs are arranged at one end of the length direction of the track chassis.
- The launcher 8. flapping-wing aircraft according to claim 5 takes off, it is characterised in that be provided with stop on the track chassis Mechanism, for carrying out locking or unblock to the travel mechanism.
- The emission system 9. a kind of flapping-wing aircraft takes off, it is characterised in that including the flapping-wing aircraft as any one of claim 1-8 Take off launcher.
- The emission system 10. flapping-wing aircraft according to claim 9 takes off, it is characterised in that also including power transport vehicle.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721071956.6U CN207157569U (en) | 2017-08-23 | 2017-08-23 | Emission system that flapping-wing aircraft takes off launcher and flapping-wing aircraft takes off |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721071956.6U CN207157569U (en) | 2017-08-23 | 2017-08-23 | Emission system that flapping-wing aircraft takes off launcher and flapping-wing aircraft takes off |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207157569U true CN207157569U (en) | 2018-03-30 |
Family
ID=61718327
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721071956.6U Expired - Fee Related CN207157569U (en) | 2017-08-23 | 2017-08-23 | Emission system that flapping-wing aircraft takes off launcher and flapping-wing aircraft takes off |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207157569U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109896036A (en) * | 2019-04-18 | 2019-06-18 | 太原科技大学 | Flapping-wing aircraft launching apparatus |
-
2017
- 2017-08-23 CN CN201721071956.6U patent/CN207157569U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109896036A (en) * | 2019-04-18 | 2019-06-18 | 太原科技大学 | Flapping-wing aircraft launching apparatus |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20180330 |