CN208360475U - Connection component and vertically taking off and landing flyer with the connection component - Google Patents

Abstract

The utility model discloses a kind of connection component and the vertically taking off and landing flyer with the connection component comprising cushion block, gasket and fixing seat.Cushion block is set in inner cavity and pad is set between top airfoil and lower aerofoil, and cushion block has the both ends for corresponding respectively to top airfoil and lower aerofoil.Gasket is set to the outer surface of one of top airfoil and lower aerofoil, and the wherein one end of cushion block is removably connected to by the first fixing piece.Fixing seat is set to wherein another outer surface of top airfoil and lower aerofoil, and wherein the other end of cushion block is removably connected to by the second fixing piece.Wherein, VTOL horn is removably mountable to fixing seat.The utility model, which can be realized, to be consolidated VTOL horn, is securely attached on wing.Meanwhile the utility model can be realized and connect to fast demountable between VTOL horn and wing, replacement easy to repair.

Description

Connection component and vertically taking off and landing flyer with the connection component

Technical field

The utility model relates to aircraft and its accessory technical fields, in particular to a kind of connection component and have The vertically taking off and landing flyer of the connection component.

Background technique

With the extensive use of various types of aircraft, requirement of the people to aircraft is also higher and higher.It is wherein compound Formula unmanned plane application is also more and more extensive.Existing combined type unmanned plane generally comprises the keys such as fuselage, wing, empennage, horn Component.Wherein, the main effect of horn is upward lift to be born when aircraft vertical takes off, and be transmitted to wing, fuselage On.As one of the essential important component that takes off vertically, the structure design and installation mode for the horn that hung down becomes flight The most important thing of device design.

In the prior art, it is difficult to which to having hung down, horn is accurately positioned, and constantly debugging is needed just to can guarantee wing Installation site, so that installation effectiveness is lower.And in the removable horn structure in part, most of structure is complicated or is difficult to protect Demonstrate,prove structural strength or structure is complicated redundancy.Meanwhile the horn of existing aircraft generallys use non-removable mode and fuselage It is fixedly connected, is unfavorable for maintenance replacement.

Utility model content

One main purpose of the utility model is to overcome at least one defect of the above-mentioned prior art, provides a kind of tool There are removable unloading functions and connects reliable and stable connection component.

Another main purpose of the utility model is to overcome at least one defect of the above-mentioned prior art, provides one kind Using the vertically taking off and landing flyer of above-mentioned connection component connection wing and VTOL horn.

To achieve the above objectives, the present invention adopts the following technical solutions:

One aspect according to the present utility model provides a kind of connection component, for connecting wing and VTOL horn, The wing has top airfoil, lower aerofoil and inner cavity.Wherein, the connection component includes cushion block, gasket and fixing seat.It is described Cushion block is set in the inner cavity and pad is set between the top airfoil and the lower aerofoil, and the cushion block, which has, corresponds respectively to institute State the both ends of top airfoil Yu the lower aerofoil.The gasket is set to the outer of one of the top airfoil and described lower aerofoil Surface, and it is removably connected to by the first fixing piece the wherein one end of the cushion block.The fixing seat is set on described Wherein another outer surface of aerofoil and the lower aerofoil, and its of the cushion block is removably connected to by the second fixing piece Middle the other end.Wherein, the VTOL horn is removably mountable to the fixing seat.

One of embodiment according to the present utility model, the cushion block both ends are respectively upper and lower end, The upper end corresponds to the top airfoil, and the lower end corresponds to the lower aerofoil；Wherein, the gasket is set on described The outer surface of aerofoil, and the upper end is removably connected to by first fixing piece, the fixing seat is set to described The outer surface of lower aerofoil, and the lower end is removably connected to by second fixing piece.

One of embodiment according to the present utility model, first fixing piece are bolt；Wherein, the cushion block Upper end offers the first screw hole, and the gasket offers first positioning hole, and the top airfoil offers first through hole, the spiral shell Bolt is arranged in the first positioning hole, the first through hole and is bolted in first screw hole, removably by the gasket It is connected to the upper end of the cushion block.

One of embodiment according to the present utility model, first screw hole, the first positioning hole and described One through-hole is that quantity is identical multiple, and multiple first positioning holes and multiple first screw holes correspond, and multiple institutes It states first through hole and multiple first screw holes corresponds.

One of embodiment according to the present utility model, second fixing piece are bolt；Wherein, the cushion block Lower end offers the second screw hole, and the fixing seat offers second location hole, and the lower aerofoil offers the second through-hole, described Bolt is arranged in the second location hole, second through-hole and is bolted in second screw hole, and the fixing seat is removable Dress it is connected to the lower end of the cushion block.

One of embodiment according to the present utility model, second screw hole, the second location hole and described Two through-holes are that quantity is identical multiple, and multiple second location holes and multiple second screw holes correspond, and multiple institutes It states the second through-hole and multiple second screw holes corresponds.

One of embodiment according to the present utility model, the fixing seat include pedestal and buckle.The pedestal It is removably connected set on wherein another outer surface of the top airfoil and the lower aerofoil, and by second fixing piece In wherein the other end of the cushion block.The third fixing piece that snaps through is removably connected to the pedestal, and with institute It states pedestal and defines clip space jointly, so that the VTOL horn is arranged in the clip space.

Other side according to the present utility model, provides a kind of vertically taking off and landing flyer, including fuselage, wing, vertical Landing horn and VTOL power mechanism, the wing is set to the fuselage and has top airfoil, lower aerofoil and inner cavity, described VTOL power mechanism is set to the VTOL horn.Wherein, the VTOL horn passes through above embodiment institute The connection component stated is removably connected to the wing.

One of embodiment according to the present utility model is equipped with rib, the cushion block patch in the inner cavity of the wing Conjunction is connected to the rib.

One of embodiment according to the present utility model, the VTOL horn pass through connection component described in multiple groups It is removably connected to the wing, connection component described in multiple groups is spaced cloth on the direction that the VTOL horn extends It sets.

One of embodiment according to the present utility model, the vertically taking off and landing flyer further include electric connector, institute Stating electric connector includes two connectors matched；One of them described connector be set to the wing lower aerofoil, and with Cable connection in the inner cavity of the wing；Connector described in another one be set to the VTOL horn, and with it is described Cable connection in VTOL horn, the position of two connectors are corresponding.

As shown from the above technical solution, the utility model proposes connection component and with the VTOL of the connection component It the advantages of aircraft and has the active effect that

The utility model proposes connection component and with the vertically taking off and landing flyer of the connection component, by the way that cushion block is set The design in wing inner cavity, and the design by the way that cushion block and gasket and fixing seat are cooperatively connected are set, can be realized and risen vertical Drop horn is consolidated, is securely attached on wing.Meanwhile the utility model is removably mountable to admittedly by VTOL horn The design of reservation can be realized and connect to fast demountable between VTOL horn and wing, replacement easy to repair.

Further, in one of embodiment of the utility model, when using it is multiple the utility model proposes Connection component matches, and when being connected to wing for VTOL horn, can make being connected to for wing and VTOL horn Have it is quick, removable simultaneously, easily facilitate operator according to the correct direction between wing and VTOL horn for two Person quickly connects, and provides foolproof function.

Detailed description of the invention

The following detailed description to preferred embodiments of the present invention is considered in conjunction with the accompanying drawings, the utility model Various targets, feature and advantage will become apparent.Attached drawing is only the exemplary diagram of the utility model, not necessarily It is drawn to scale.In the accompanying drawings, same appended drawing reference always shows same or similar component.Wherein:

Fig. 1 is solid when a kind of connection component shown according to an illustrative embodiments is connect with VTOL horn Structural schematic diagram；

Fig. 2 is another angular views of Fig. 1；

Fig. 3 is a kind of sectional perspective structural representation of vertically taking off and landing flyer shown according to an illustrative embodiments Figure；

Fig. 4 is the cross-sectional view of the vertically taking off and landing flyer shown in Fig. 3；

Fig. 5 is the part isometric structural schematic diagram of the vertically taking off and landing flyer shown in Fig. 3.

Wherein, the reference numerals are as follows:

100. connection component；

110. cushion block；

111. upper end；

112. lower end；

120. gasket；

121. first positioning hole；

130. pedestal；

131. second location hole；

132. third location hole；

140. buckle；

141. the 4th location holes；

142. the 5th location holes；

200. wing；

210. top airfoil；

220. lower aerofoil；

230. inner cavity；

240. rib；

300. VTOL horns；

400. VTOL power mechanisms；

500. high current connector；

510. first connectors；

520. second connectors.

Specific embodiment

The exemplary embodiments for embodying the utility model features and advantages will describe in detail in the following description.It should be understood that It is that the utility model there can be various variations in different embodiments, does not all depart from the scope of the utility model, and Explanation therein and attached drawing are inherently illustrative, rather than to limit the utility model.

In being described below the different illustrative embodiments to the utility model, carried out referring to attached drawing, the attached drawing A part of the utility model is formed, and wherein shows many aspects of achievable the utility model by way of example not Same exemplary structure, system and step.It should be understood that other of component, structure, exemplary means, system and step can be used Specified scheme, and structural and functional modification can be carried out without departing from the scope of the utility model.Although moreover, originally It can be used term " upper end ", " lower end ", " between ", " in " etc. exemplary come the difference for describing the utility model in specification Feature and element, but these terms are in this article merely for convenient, for example, with reference to the accompanying drawings described in exemplary direction.This Any content in specification is not necessarily to be construed that the specific three dimensional direction of Structure of need is just fallen into the scope of the utility model.

Connection component embodiment one

Refering to fig. 1, the connection component 100 that can embody the principles of the present invention is representatively illustrated in Fig. 1 and is hung down Schematic perspective view when straight landing horn 300 connects.In the illustrative embodiments, the utility model proposes connection Component 100 is illustrated by taking VTOL horn 300 and wing 200 for connecting vertically taking off and landing flyer as an example.This Field technical staff it is easily understood that for by the connection component 100 be used to connect the wing 200 of other kinds of aircraft with Similar to the other structures of VTOL horn 300, and to following specific embodiments make it is a variety of remodeling, addition, substitution, Delete or other variation, these variation still the utility model proposes connection component 100 principle in the range of.

As shown in Figure 1, in the present embodiment, wing 200 can refer to the structure design of existing wing 200, i.e. wing 200 Including top airfoil 210, lower aerofoil 220 and inner cavity 230.Specifically, so-called top airfoil 210 and lower aerofoil 220 are wing The upper and lower surfaces of mask, inner cavity 230 are the cavity that top airfoil 210 and lower aerofoil 220 (i.e. wing mask) define Structure.Wherein, every group of connection component 100 mainly includes cushion block 110, gasket 120 and fixing seat.Cooperate refering to Fig. 2 to Fig. 5, Fig. 2 representatively illustrates another angular views that can embody the connection component 100 of the utility model principle；Fig. 3 is representative Ground shows the sectional perspective structural schematic diagram that can embody the vertically taking off and landing flyer of the utility model principle；Fig. 4 is representative Ground shows the cross-sectional view that can embody the vertically taking off and landing flyer of the utility model principle；Fig. 5 is representatively illustrated can Embody the part isometric structural schematic diagram of the vertically taking off and landing flyer of the utility model principle.It is practical to this below in conjunction with attached drawing Structure, connection type and the functional relationship of each chief component of the connection component 100 of novel proposition are described in detail.

As depicted in figs. 1 and 2, in the present embodiment, cushion block 110 is arranged in the inner cavity 230 of wing 200.It is specific and Speech, cushion block 110 be pad be located between the top airfoil 210 of wing 200 and lower aerofoil 220, and cushion block 110 have correspond respectively to The both ends of aerofoil 210 and lower aerofoil 220, the both ends are respectively under corresponding to the upper end 111 of top airfoil 210 and corresponding to The lower end 112 of aerofoil 220.It accordingly, can will such as rotor by being embedded in cushion block 110 in the inner cavity 230 of wing 200 VTOL power mechanism 400 caused by lift be transferred to wing 200, and be further transferred to fuselage.

As depicted in figs. 1 and 2, in the present embodiment, the appearance of the top airfoil 210 of wing 200 is arranged in gasket 120 Face, and be removably connected by the first fixing piece in the upper end of cushion block 110 111.Accordingly, when gasket 120 and cushion block 110 When upper end 111 connects, then the whole top airfoil 210 with wing 200 of connection component 100 is connected and fixed.

Further, as depicted in figs. 1 and 2, in the present embodiment, the first fixing piece preferably uses bolt, that is, pads Piece 120 with cushion block 110 is removably connected by bolt.Correspondingly, the upper end 111 of cushion block 110 offers the first screw hole, Gasket 120 offers first positioning hole 121, and top airfoil 210 offers first through hole.Accordingly, bolt is arranged in first positioning hole 121, first through hole and it is bolted in the first screw hole, so that gasket 120 to be removably connected to the upper end 111 of cushion block 110.? In other embodiments, first of other fixed connecting elements substitution bolt as connection cushion block 110 with gasket 120 also can be used Fixing piece, such as rivet etc., and the open-celled structures such as the first screw hole, first positioning hole 121 and first through hole can be adjusted accordingly, herein It will not go into details.

Further, as depicted in figs. 1 and 2, in the present embodiment, gasket 120 and cushion block 110 pass through two bolts Connection, that is, the first screw hole, first positioning hole 121 and first through hole are two and are correspondingly arranged.Hereby it is possible to further The rotation for avoiding cushion block 110 and gasket 120 from generating relative to top airfoil 210 around bolt promotes what cushion block 110 was connect with gasket 120 Stability.In other embodiments, the quantity of bolt, the first screw hole, first positioning hole 121 and first through hole also can be by other Selection.Wherein, the quantity of the first screw hole, first positioning hole 121 and first through hole is advisable with arrangement with corresponding design, and When first screw hole, first positioning hole 121 and first through hole are that quantity is identical multiple, multiple first positioning holes 121 and multiple the One screw hole is advisable with one-to-one design, and multiple first through hole are advisable with multiple first screw holes with one-to-one design.

As depicted in figs. 1 and 2, in the present embodiment, the outer surface of the lower aerofoil 220 of wing 200 is arranged in fixing seat, And it is removably connected by the second fixing piece in the lower end of cushion block 110 112.Accordingly, when the lower end of fixing seat and cushion block 110 When portion 112 connects, then the whole lower aerofoil 220 with wing 200 of connection component 100 is connected and fixed.Wherein, VTOL horn 300 are removably mountable to fixing seat, and VTOL horn 300 is removably connected fixation by connection component 100 with this On wing 200, so that VTOL horn 300 be made to be conveniently replaceable maintenance, and convenient transportation.

Further, as depicted in figs. 1 and 2, in the present embodiment, the second fixing piece preferably uses bolt, i.e., solid Reservation with cushion block 110 is removably connected by bolt.Correspondingly, the lower end 112 of cushion block 110 offers the second screw hole, Fixing seat offers second location hole 131, and lower aerofoil 220 offers the second through-hole.Accordingly, bolt is arranged in second location hole 131, the second through-hole and it is bolted in the second screw hole, so that fixing seat to be removably connected to the lower end 112 of cushion block 110.? In other embodiments, second of other fixed connecting elements substitution bolt as connection cushion block 110 with fixing seat also can be used Fixing piece, such as rivet etc., and the open-celled structures such as the second screw hole, second location hole 131 and second through-hole can be adjusted accordingly, herein It will not go into details.

Further, as depicted in figs. 1 and 2, in the present embodiment, fixing seat and cushion block 110 pass through two bolts Connection, that is, the second screw hole, second location hole 131 and the second through-hole are two and are correspondingly arranged.Hereby it is possible to further The rotation for avoiding cushion block 110 and fixing seat from generating relative to lower aerofoil 220 around bolt, promotion cushion block 110 connect steady with fixing seat It is qualitative.In other embodiments, the quantity of bolt, the second screw hole, second location hole 131 and the second through-hole also can be by other choosings It selects.Wherein, the quantity of the second screw hole, second location hole 131 and the second through-hole is advisable with arrangement with corresponding design, and the When two screw holes, second location hole 131 and the second through-hole are that quantity is identical multiple, multiple second location holes 131 and multiple second Screw hole is advisable with one-to-one design, and multiple second through-holes are advisable with multiple second screw holes with one-to-one design.

As depicted in figs. 1 and 2, in the present embodiment, fixing seat mainly includes pedestal 130 and is removably fastened on The buckle 140 of pedestal 130.Specifically, the outer surface of the lower aerofoil 220 of wing 200 is arranged in pedestal 130, and by above-mentioned Second fixing piece is removably connected to the lower end 112 of cushion block 110.Buckle 140 is removably connected by third fixing piece Clip space is defined jointly in pedestal 130, and with pedestal 130, so that VTOL horn 300 is arranged in clip space.At it In his embodiment, other structures are can be used also to realize that VTOL horn 300 is removably mountable to fixing seat in fixing seat In, it is not limited with present embodiment.

Further, as depicted in figs. 1 and 2, in the present embodiment, substantially it is in the section of VTOL horn 300 For circle, 130 lower part of pedestal is formed with the semicircle notching construction that Open Side Down, and buckle 140 is also in the semicircle of opening upwards Shape structure defines circular clip space after the two pairing jointly, is mounted on clip sky to wear for VTOL horn 300 Between in.In other embodiments, the shape of the shape in clip space, i.e. pedestal 130 and buckle 140 can also rise according to vertical The cross sectional shape of drop horn 300 is adjusted flexibly, and is not limited with present embodiment.

Further, as depicted in figs. 1 and 2, in the present embodiment, pedestal 130 can be fixed with buckle 140 by third Part (such as positioning pin, rivet or bolt etc.) realization is removably connected.Determine specifically, 130 bottom of pedestal offers third Position hole 132, buckle 140 offer the 4th location hole 141 corresponding with third location hole 132, and bolt is arranged in third positioning Hole 132 and the 4th location hole 141 are removably fixedly connected to buckle 140 with pedestal 130.

Further, as shown in Fig. 2, in the present embodiment, it is also provided with the 5th location hole 142 on buckle 140, this The position of five location holes 142 opened up when position is mounted on fixing seat with VTOL horn 300 is corresponding, and VTOL machine The 6th location hole corresponding with the 5th location hole 142 is offered on arm 300.Accordingly, when VTOL horn 300 wears installation In fixing seat, it is arranged in the 5th location hole 142 and the 6th location hole using fixing pieces such as rivets, thus by VTOL machine Arm 300 and buckle 140 are relatively fixed, further avoid VTOL horn 300 and generate axial float or torsion in clip space Turn, the effect of auxiliary positioning is provided, promotes the stability that VTOL horn 300 is installed.

Connection component embodiment two

In the illustrative embodiments, each primary structure composition and functional relationship and first embodiment of connection component The design of the connection component of middle explanation is roughly the same, and the main distinction is:

In the present embodiment, the lower aerofoil of wing is arranged in gasket, and is removably connected to by the first fixing piece The lower end of cushion block.The top airfoil of wing is arranged in fixing seat, and by the second shareholder and is removably connected to the upper of cushion block End.Accordingly, the connection component that present embodiment proposes, which can be realized, is removably mountable to wing for VTOL horn Top airfoil.

It should be noted here that being shown in attached drawing and the connection component that describes in the present specification is only can use this hair Two examples in many kinds of connection components of bright principle.It should be clearly understood that the principle of the present invention is only limitted to absolutely not attached drawing In show or any part of any details of connection component described in this specification or connection component.

Vertically taking off and landing flyer embodiment

Refering to Fig. 3 to Fig. 5, in the illustrative embodiments, the utility model proposes vertically taking off and landing flyer be with It is illustrated for unmanned plane with VTOL function.It will be readily appreciated by those skilled in the art that for this is vertical The design of landing unmanned plane is applied in other kinds of vertically taking off and landing flyer, and makes to following specific embodiments more Kind of remodeling, substitution, is deleted or other variations at addition, these variations still the utility model proposes vertically taking off and landing flyer In the range of principle.

As shown in Figures 3 to 5, in the present embodiment, the utility model proposes vertically taking off and landing flyer mainly include Fuselage, wing 200, VTOL horn 300 and VTOL power mechanism 400.Specifically, wing 200 is arranged in fuselage Above and there is top airfoil 210, lower aerofoil 220 and inner cavity 230, VTOL power mechanism 400 is arranged in VTOL horn 300.Wherein, VTOL horn 300 by the utility model proposes connection component 100 be removably connected in wing 200 Lower aerofoil 220.With reference to the explanation in the above-mentioned second embodiment about connection component 100, in other embodiments, hang down Straight landing horn 300 also can by the utility model proposes connection component 100 be removably connected the top airfoil in wing 200 210, it is not limited with present embodiment.

Further, as shown in figure 5, being equipped with the knot of rib 240 in the inner cavity 230 of the wing 200 based on existing unmanned plane Structure design, in the present embodiment, cushion block 110 is preferably fitted and connected in rib 240.Hereby it is possible to make the setting of cushion block 110 It is more firm, and can further be transmitted through rib 240 lift caused by the VTOL power mechanism 400 by such as rotor To wing 200.

Further, as shown in Figures 3 to 5, in the present embodiment, VTOL horn 300 preferably passes through multiple groups Connection component 100 is removably connected to wing 200, and multiple groups connection component 100 is in the direction that VTOL horn 300 extends Upper arranged for interval.Hereby it is possible to make wing 200 and VTOL horn 300 be connected to have it is quick, removable simultaneously, It easily facilitates operator and quickly connects the two according to the correct direction between wing 200 and VTOL horn 300, to mention For foolproof function.

It should be noted here that being shown in attached drawing and the vertically taking off and landing flyer that describes in the present specification is only to adopt With an example in many kinds of vertically taking off and landing flyer of the principle of the invention.It should be clearly understood that the principle of the present invention is exhausted It is non-to be only limitted to show in attached drawing or any details or vertically taking off and landing flyer of vertically taking off and landing flyer described in this specification Any part.

For example, as shown in Figures 3 to 5, in the present embodiment, the utility model proposes vertically taking off and landing flyer Preferably using high current connector 500 as connecting being electrically connected for wing 200 and the Internal cable of VTOL horn 300 The lower aerofoil 220 (or top airfoil 210) of wing 200 is arranged in first connector 510 of device, i.e. 500 side of high current connector, And the second connector 520 of 500 other side of high current connector is arranged on VTOL horn 300.Accordingly, work as VTOL When horn 300 is fixedly connected on lower aerofoil 220 (or top airfoil 210) of wing 200 by connection component 100, the first connector 510 dock with the second connector 520.In addition, due to the space limitation between VTOL horn 300 and wing 200, Neng Goubao It demonstrate,proves the first connector 510 and docking for the second connector 520 is close.

For another example, in the present embodiment, each cable of vertically taking off and landing flyer is preferably in wing 200 and VTOL machine 300 interior cabling of arm, and be connected to the first connector 510 and the second connector 520 and realize electrical connection.Hereby it is possible to real The not exposed effect of existing cable, structure is safe and reliable, stablizes, and will not generate additional friction to vertically taking off and landing flyer.

In conclusion the utility model proposes connection component and with the vertically taking off and landing flyer of the connection component, lead to Cross the design that cushion block is arranged in wing inner cavity, and the design by the way that cushion block and gasket and fixing seat are cooperatively connected, Neng Goushi Now VTOL horn is consolidated, is securely attached on wing.Meanwhile the utility model is removable by VTOL horn Ground is installed on the design of fixing seat, can be realized and is removably connected between VTOL horn and wing, replacement easy to repair.

Be described in detail above and/or illustrate the utility model proposes connection component and with the connection component hang down The illustrative embodiments of straight landing aircraft.But the embodiments of the present invention is not limited to particular implementation as described herein Mode, on the contrary, the component part of each embodiment and/or step can be with other component parts as described herein and/or steps It is rapid independent and be used separately.Each component part of one embodiment and/or each step can also be with other embodiments Other component parts and/or step are used in combination.Introduce it is described here and/or diagram element/component part/wait whens, Term "one", " one " and " above-mentioned " etc. to indicate there are one or more elements/component part/etc..Term "comprising", " comprising " and " having " to indicate the open meaning being included and refer in addition to list element/component part/ Also may be present Deng except other element/component part/etc..In addition, term " first " in claims and specification and " second " etc. only uses as label, is not the numerical limit to its object.

Although according to different specific embodiments to the utility model proposes connection component and have the connection component Vertically taking off and landing flyer be described, but it will be recognized by those skilled in the art can be in spirit and scope of the claims The interior implementation to the utility model is modified.

Claims (11)

1. a kind of connection component, for connecting wing and VTOL horn, the wing has top airfoil, lower aerofoil and interior Chamber, which is characterized in that the connection component includes:

Cushion block, is set in the inner cavity and pad is set between the top airfoil and the lower aerofoil, and it is right respectively that the cushion block has The both ends of top airfoil described in Ying Yu and the lower aerofoil；

Gasket, set on the outer surface of one of the top airfoil and the lower aerofoil, and it is removable by the first fixing piece Ground is connected to the wherein one end of the cushion block；And

Fixing seat, set on wherein another outer surface of the top airfoil and the lower aerofoil, and it is removable by the second fixing piece Dress it is connected to wherein the other end of the cushion block；

Wherein, the VTOL horn is removably mountable to the fixing seat.

2. connection component according to claim 1, which is characterized in that the cushion block both ends are respectively upper end and lower end Portion, the upper end correspond to the top airfoil, and the lower end corresponds to the lower aerofoil；Wherein, the gasket is set to institute The outer surface of top airfoil is stated, and the upper end is removably connected to by first fixing piece, the fixing seat is set to The outer surface of the lower aerofoil, and the lower end is removably connected to by second fixing piece.

3. connection component according to claim 1, which is characterized in that first fixing piece is bolt；Wherein, the pad The upper end of block offers the first screw hole, and the gasket offers first positioning hole, and the top airfoil offers first through hole, institute Bolt is stated to be arranged in the first positioning hole, the first through hole and be bolted in first screw hole, the gasket is removable Dress it is connected to the upper end of the cushion block.

4. connection component according to claim 3, which is characterized in that first screw hole, the first positioning hole and institute Stating first through hole is that quantity is identical multiple, and multiple first positioning holes and multiple first screw holes correspond, and more A first through hole and multiple first screw holes correspond.

5. connection component according to claim 1, which is characterized in that second fixing piece is bolt；Wherein, the pad The lower end of block offers the second screw hole, and the fixing seat offers second location hole, and the lower aerofoil offers the second through-hole, The bolt is arranged in the second location hole, second through-hole and is bolted in second screw hole, by the fixing seat It is removably connected to the lower end of the cushion block.

6. connection component according to claim 5, which is characterized in that second screw hole, the second location hole and institute Stating the second through-hole is that quantity is identical multiple, and multiple second location holes and multiple second screw holes correspond, and more A second through-hole and multiple second screw holes correspond.

7. connection component according to claim 1, which is characterized in that the fixing seat includes:

Pedestal, set on wherein another outer surface of the top airfoil and the lower aerofoil, and can by second fixing piece It is removably connected to wherein the other end of the cushion block；And

Buckle, is removably connected to the pedestal by third fixing piece, and define clip space jointly with the pedestal, with The clip space is arranged in for the VTOL horn.

8. a kind of vertically taking off and landing flyer, including fuselage, wing, VTOL horn and VTOL power mechanism, the machine The wing is set to the fuselage and has top airfoil, lower aerofoil and inner cavity, and the VTOL power mechanism is set to the VTOL Horn, which is characterized in that the VTOL horn passes through the described in any item connection components of claim 1~7 removably It is connected to the wing.

9. vertically taking off and landing flyer according to claim 8, which is characterized in that rib is equipped in the inner cavity of the wing, The cushion block is fitted and connected in the rib.

10. vertically taking off and landing flyer according to claim 8, which is characterized in that the VTOL horn passes through multiple groups The connection component is removably connected to the wing, and connection component described in multiple groups is in the side that the VTOL horn extends Upward arranged for interval.

11. vertically taking off and landing flyer according to claim 8, which is characterized in that the vertically taking off and landing flyer further includes Electric connector, the electric connector include two connectors matched；One of them described connector is set to the wing Lower aerofoil, and connect with the cable in the inner cavity of the wing；Connector described in another one is set to the VTOL machine Arm, and connect with the cable in the VTOL horn, the position of two connectors is corresponding.