CN209441599U - Rack and aircraft for aircraft - Google Patents

Abstract

The utility model discloses a kind of rack and aircraft for aircraft, rack includes: fuselage, card line seat and connection component, and card line seat is connect with fuselage, and card line seat is equipped with the first retaining part and first and is slidably matched portion.Connection component is equipped with the second retaining part that the first retaining part offsets and is slidably matched portion with first portion compatible second that is slidably matched, second be slidably matched portion and the second retaining part is arranged along the extending direction interval of the second sliding part, when first is slidably matched portion with the cooperation of second portion of being slidably matched, the first retaining part and the second retaining part only support cooperation.Rack according to the present utility model for aircraft, when first is slidably matched portion with the cooperation of second portion of being slidably matched, first retaining part and the second retaining part mutually can only support cooperation, to limit the opposite sliding between connection component and card line seat, to realize the solid and reliable assembly between connection component and card line seat.

Description

Rack and aircraft for aircraft

Technical field

The utility model relates to vehicle technology field more particularly to a kind of racks and aircraft for aircraft.

Background technique

With the rapid development of unmanned air vehicle technique, the function of unmanned plane is also more and more, and unmanned plane is widely used in respectively Each industry of row.However, the function of unmanned plane increases, the connection line between each functional module of unmanned plane is also increase accordingly.It is related In technology, unmanned plane generates vibration in flight course, is easy to cause the line connection terminal between each functional module to loosen, shadow Ring the normal operation of unmanned plane.

Utility model content

The utility model aims to solve at least one of the technical problems existing in the prior art.For this purpose, the utility model mentions A kind of rack for aircraft out, the rack have the advantages that structure is simple, connects reliably.

The utility model, which also mentions, issues a kind of aircraft, and the aircraft includes the machine for aircraft described above Frame.

According to the rack for aircraft of the utility model embodiment, comprising: fuselage；Card line seat, the card line seat with Fuselage connection, the card line seat are equipped with the first retaining part and first and are slidably matched portion；Connection component, the connection component are set There is the second retaining part to offset with first retaining part, the connection component is equipped with and is adapted with first portion of being slidably matched Second be slidably matched portion, extension that portion and second retaining part be slidably matched portion along described second that described second is slidably matched The setting of direction interval, when described first be slidably matched portion and second portion of being slidably matched cooperate when, first retaining part with Second retaining part only supports cooperation, with the fixation connection component and the card line seat.

According to the rack for aircraft of the utility model embodiment, portion is slidably matched by first and the second sliding is matched Under the action of conjunction portion, the convenience assembled between connection component and card line seat and high efficiency can be improved.Moreover, when the first sliding When auxiliary section and second portion of being slidably matched cooperate, the first retaining part and the second retaining part mutually can only support cooperation, with the company of limitation Opposite sliding between connected components and card line seat, to realize the solid and reliable assembly between connection component and card line seat, has Effect avoids in aircraft operational process, vibration occurs and the problem that causes the circuit connection of aircraft unstable.

Some embodiments according to the present utility model, the connection component include: the first connection terminal, first connection Terminal is equipped with described second and is slidably matched portion and second retaining part；Second connection end, second connection end and institute State the electrical connection of the first connection terminal.

In some embodiments of the utility model, described second is slidably matched portion and second retaining part is set to institute State the surface towards the card line seat of the first connection terminal, first portion of being slidably matched be set to the card line seat towards institute State the surface of the first connection terminal.

Some embodiments according to the present utility model, the front side wall of the card line seat, which is equipped with, is directed away from first sliding The extension that auxiliary section extends, the part of the upper surface of the extension raises upward to form first retaining part.

In some embodiments of the utility model, the extension prolongs along direction inclination from the front to the back, from top to bottom It stretches.

Some embodiments according to the present utility model are equipped at intervals with multiple reinforcing ribs on the extension.

In some embodiments of the utility model, the cross section of second retaining part is triangle.

Some embodiments according to the present utility model, first connection terminal towards shown second connection end first End is equipped with assembles post, and second connection end is equipped with pilot hole compatible with the assembles post.

In some embodiments of the utility model, the periphery wall of the assembles post is equipped with cooperation hook, the cooperation Hook is scalable along the radial direction of the assembles post, and second connection end is equipped with the cooperation card being connected to the pilot hole Slot, when the assembles post protrudes into the pilot hole, the cooperation hook and the cooperation card slot are engaged by clamping.

Some embodiments according to the present utility model, first portion of being slidably matched are sliding slot, and described second is slidably matched Portion is sliding block, and the end of the open end of the sliding slot is equipped with guiding surface.

In some embodiments of the utility model, the described first be slidably matched portion and second portion of being slidably matched is one One is corresponding multiple.

According to the aircraft of the utility model embodiment, comprising: rack, the rack are described above for aircraft Rack.

According to the aircraft of the utility model embodiment, by first be slidably matched portion and second be slidably matched portion effect Under, the convenience assembled between connection component and card line seat and high efficiency can be improved.Moreover, being slidably matched portion and the when first When two portions of being slidably matched cooperate, the first retaining part and the second retaining part mutually can only support cooperation, to limit connection component and card Opposite sliding between line seat, to realize the solid and reliable assembly between connection component and card line seat, effectively prevents flying In row device operational process, vibration occurs and the problem that causes the circuit connection of aircraft unstable.

Some embodiments according to the present utility model, further include electronic equipment, the electronic equipment and the connection component Connection.

The additional aspect and advantage of the utility model will be set forth in part in the description, partially will be from following description In become obvious, or recognized by the practice of the utility model.

Detailed description of the invention

The above-mentioned and/or additional aspect and advantage of the utility model from the description of the embodiment in conjunction with the following figures will Become obvious and be readily appreciated that, in which:

Fig. 1 is the partial structural diagram according to the aircraft of the utility model embodiment；

Fig. 2 is the partial structurtes enlarged drawing for the part A that Fig. 1 centre circle shows；

Fig. 3 is the structural schematic diagram according to the card line seat of the rack for aircraft of the utility model embodiment；

Fig. 4 is the structural schematic diagram according to the card line seat of the rack for aircraft of the utility model embodiment；

Fig. 5 is the partial structurtes enlarged drawing for the part B that Fig. 4 centre circle shows；

Fig. 6 is shown according to the structure of the first connection terminal of the connection component for aircraft of the utility model embodiment It is intended to；

Fig. 7 is shown according to the structure of second connection end of the connection component for aircraft of the utility model embodiment It is intended to；

Fig. 8 is shown according to the structure of second connection end of the connection component for aircraft of the utility model embodiment It is intended to；

Fig. 9 is the partial structural diagram according to the aircraft of the utility model embodiment；

Figure 10 is the bottom view according to the aircraft of the utility model embodiment；

Figure 11 is the structural schematic diagram according to the aircraft of the utility model embodiment.

Appended drawing reference:

Aircraft 100,

Fuselage 10, bottom plate 11, top plate 12, installing frame 13, the first loading space 134, the second loading space 135, undercarriage 14,

Card line seat 20, extension 210, the first retaining part 211, reinforcing rib 212, first is slidably matched portion 220, guiding surface 221,

Connection component 30, the first connection terminal 310, second is slidably matched portion 311, the second retaining part 312, assembles post 313, Cooperating hook 3130, second connection end 320, pilot hole 321 cooperates card slot 322,

Electronic equipment 40, winged control module 410, communication module 420, electric mode transfer block 430, switching circuit board component 440,

Liquid storage container 810, battery 820,

Horn 90, Power Component 910.

Specific embodiment

The embodiments of the present invention are described below in detail, examples of the embodiments are shown in the accompanying drawings, wherein from beginning Same or similar element or element with the same or similar functions are indicated to same or similar label eventually.Below by ginseng The embodiment for examining attached drawing description is exemplary, and is only used for explaining the utility model, and should not be understood as to the utility model Limitation.

In the description of the present invention, it should be understood that term " length ", "upper", "lower", "front", "rear", The orientation or positional relationship of the instructions such as "inner", "outside", " radial direction " be based on the orientation or positional relationship shown in the drawings, merely to Convenient for describing the utility model and simplifying description, rather than the device or element of indication or suggestion meaning must have specific side Position is constructed and operated in a specific orientation, therefore should not be understood as limiting the present invention.In addition, define " first ", The feature of " second " can explicitly or implicitly include one or more of the features.In the description of the present invention, Unless otherwise indicated, the meaning of " plurality " is two or more.

In the description of the present invention, it should be noted that unless otherwise clearly defined and limited, term " is pacified Dress ", " connection " shall be understood in a broad sense, for example, it may be being fixedly connected, may be a detachable connection, or be integrally connected；It can To be mechanical connection, it is also possible to be electrically connected；It can be directly connected, can also can be indirectly connected through an intermediary Connection inside two elements.For the ordinary skill in the art, above-mentioned term can be understood at this with concrete condition Concrete meaning in utility model.

Below with reference to Fig. 1-Figure 11 description according to the rack and aircraft for aircraft 100 of the utility model embodiment 100。

As shown in Figure 1-Figure 3, according to the rack for aircraft 100 of the utility model embodiment, rack includes: fuselage 10, card line seat 20 and connection component 30.

Specifically, as depicted in figs. 1 and 2, card line seat 20 is connect with fuselage 10.For example, card line seat 20 can pass through spiral shell Line fastener is fixedly connected with fuselage 10, and card line seat 20 can also, clamping Nian Jie with fuselage 10 or solid by other connection types Fixed connection.

As shown in Figure 3-Figure 5, card line seat 20 is equipped with the first retaining part 211 and first and is slidably matched portion 220.Correspondingly, such as Shown in Fig. 6, connection component 30 is equipped with the second retaining part 312 to offset with the first retaining part 211, and connection component 30 is equipped with and first The portion 220 compatible second that is slidably matched is slidably matched portion 311, and second is slidably matched portion 311 and the second retaining part 312 along second Be slidably matched portion 311 extending direction interval setting, when first be slidably matched portion 220 with second be slidably matched portion 311 cooperation when, First retaining part 211 and the second retaining part 312 only support cooperation, to be fixedly connected with component 30 and card line seat 20.

It should be noted that in assembly connection component 30, can be matched by first portion 220 that is slidably matched with the second sliding Cooperation between conjunction portion 311 makes connection component 30 be slidably matched with card line seat 20, when connection component 30 is sliding relative to card line seat 20 When moving to predetermined position, cooperation is only supported by the first retaining part 211 and the second retaining part 312.First is slidably matched portion 220 and Two are slidably matched under the mutual cooperation effect between portion 311, and can limit can only occur between connection component 30 and card line seat 20 Opposite sliding occurs for the extending direction for being slidably matched portion 220 along first.And when the first retaining part 211 and the second retaining part 312 stop When to cooperation, first portion 220 and second that is slidably matched can be prevented to be slidably matched between portion 311 opposite sliding occurs, thus real The reliable and stable assembly between connection component 30 and card line seat 20 is showed.

According to the rack for aircraft 100 of the utility model embodiment, it is slidably matched portion 220 and second by first It is slidably matched under the action of portion 311, the convenience assembled between connection component 30 and card line seat 20 and high efficiency can be improved.And And when first be slidably matched portion 220 and second be slidably matched portion 311 cooperate when, the first retaining part 211 and the second retaining part 312 Cooperation mutually can be only supported, to limit the opposite sliding between connection component 30 and card line seat 20, to realize connection component Solid and reliable assembly between 30 and card line seat 20 effectively prevents in 100 operational process of aircraft, and vibration occurs and causes to fly The unstable problem of the circuit connection of row device 100.

Some embodiments according to the present utility model, as shown in Fig. 2, Fig. 6-Fig. 8, connection component 30 includes: the first connection Terminal 310 and second connection end 320 are slidably matched portion 311 and second as shown in fig. 6, the first connection terminal 310 is equipped with second Retaining part 312.Thus, it is possible to by first be slidably matched portion 220 and second be slidably matched mutual cooperation between portion 311, with And the first connection terminal 310 is fixed to card line seat 20 by the first cooperation of only supporting between retaining part 211 and the second retaining part 312 On.

Second connection end 320 is electrically connected with the first connection terminal 310.It should be noted that the difference on aircraft 100 It can be realized and be connected with each other by connection component 30 between electronic equipment 40, for example, it may be by the first connection terminal 310 and its Middle a part of electronic equipment 40 connects, and second connection end 320 is connect with another part electronic equipment 40.First connection terminal It is connected with each other between 310 and second connection end 320.Thus, it is possible to realize between distinct electronic apparatuses 40 signal transmission and The functions such as electric current transmission.

In some embodiments of the utility model, as shown in fig. 6, second is slidably matched portion 311 and the second retaining part 312 The surface towards card line seat 20 of the first connection terminal 310 can be set to.Correspondingly, as shown in Figure 4 and Figure 5, the first sliding Auxiliary section 220 is set to the surface of the first connection terminal 310 of direction of card line seat 20.As a result, convenient for the first connection terminal 310 and card Fixing assembling between line seat 20.

Specifically, as shown in figs 2-4, card line seat 20 is fixed on fuselage 10, and the first connection terminal 310 is fixed on card line The upper surface of seat 20, the upper surface of card line seat 20 are equipped with first and are slidably matched portion 220 and the first retaining part 211.Correspondingly, as schemed Shown in 6, the lower end surface of the first connection terminal 310 is equipped with second and is slidably matched portion 311 and the second retaining part 312.It is sliding by first Dynamic auxiliary section 220 and the second mutual cooperation for being slidably matched between portion 311, the first retaining part 211 and the second retaining part 312 can be with First connection terminal 310 is stablized, is efficiently assembled on card line seat 20.

Some embodiments according to the present utility model, as shown in Figure 3-Figure 5, the front side wall of card line seat 20, which is equipped with, to be directed away from First extension 210 for being slidably matched the extension of portion 220, the part of the upper surface of extension 210 raises upward to be formed and first be stopped Support 211.It is convenient for the processing and manufacturing of the first retaining part 211 as a result,.As shown in Figure 3 and Figure 4, edge on the front side wall of card line seat 20 The length direction of card line seat 20 is equipped at intervals with multiple extensions 210, and first retaining part is provided on each extension 210 211.Thus, it is possible to by the fixed multiple connection components 30 of card line seat 20, so as to improve the vdiverse in function of aircraft 100 Property.

In some embodiments of the utility model, as shown in Figure 4 and Figure 5, extension 210 can along from the front to the back, by Upper downwardly direction (front-rear direction up and down as shown in Figures 4 and 5) inclination extends.It should be noted that by that will extend Portion 210 is set as the structure that inclination extends, and the structural strength of extension 210 can be improved, furthermore, it is possible to have extension 210 There is good elastic deformation ability.When assembling the first connection terminal 310, second can be slidably matched portion 311 and first sliding Dynamic auxiliary section 220 is slidably matched, when second be slidably matched portion 311 slide into predetermined position when, extension can be pressed down on 210, it engages the first retaining part 211 and the second retaining part 312 and cooperates.The first connection terminal 310 and card line seat are improved as a result, The fastness and reliability assembled between 20.

Some embodiments according to the present utility model can be equipped at intervals with multiple as shown in Figure 4 and Figure 5, on extension 210 Reinforcing rib 212.It is understood that multiple reinforcing ribs 212 are arranged by being spaced on extension 210, extension can be improved 210 structural strength effectively prevents extension 210 and is broken because stress is excessive, to improve the stabilization of the structure of rack Property and reliability.

In some embodiments of the utility model, as shown in fig. 6, the cross section of the second retaining part 312 can be triangle Shape.It is convenient for the processing and manufacturing of the second retaining part 312 as a result,.Moreover, triangular structure has good structural stability and structure The fastness and reliability cooperated between the first retaining part 211 and the second retaining part 312 can be improved, furthermore, it is possible to have in intensity Imitate the defect for avoiding the second retaining part 312 from being broken because stress is excessive.

Some embodiments according to the present utility model, as shown in Figure 6 and Figure 8, the first connection terminal 310 is towards shown second The first end of connection terminal 320 is equipped with assembles post 313, and second connection end 320 is equipped with pilot hole compatible with assembles post 313 321.When installing the first connection terminal 310 and second connection end 320, assembles post 313 can be protruded into corresponding pilot hole In 321, structure is simple, easy to assembly.

In some embodiments of the utility model, as shown in fig. 6, the periphery wall of assembles post 313 is equipped with cooperation hook 3130, cooperation hook 3130 is scalable along the radial direction of assembles post 313.That is, the periphery wall of assembles post 313 is equipped with It can be with the cooperation hook 3130 of radial expansion.Correspondingly, as shown in Figure 7 and Figure 8, second connection end 320 is equipped with and pilot hole The cooperation card slot 322 of 321 connections, when assembles post 313 protrudes into pilot hole 321, cooperation hook 3130 is matched with the cooperation clamping of card slot 322 It closes.Thus, it is possible to improve the reliability and stability connected between the first connection terminal 310 and second connection end 320.

When assembling the first connection terminal 310 and second connection end 320, assembles post 313 can be protruded into pilot hole 321 Interior, during assembles post 313 protrudes into pilot hole 321, the internal perisporium extrusion fit hook 3130 of pilot hole 321 is radially It is flexible.When assembles post 313 stretches to predetermined position, cooperation hook 3130 is radially popped up, to be engaged to cooperation card In slot 322, to realize the stabilization between the first connection terminal 310 and second connection end 320, be reliably connected.

Referring to figs. 7 and 8, cooperation card slot 322 is connected to pilot hole 321 and through second connection end 320.It is tearing open When unloading the first connection terminal 310 and second connection end 320, press-fit hook 3130 can be pressed by cooperation card slot 322, make to match It closes hook 3130 radially to inside contract, so as to extract assembles post 313 out from pilot hole 321.

Some embodiments according to the present utility model, as shown in figure 5, first portion 220 that is slidably matched can be sliding slot.Accordingly Ground, as shown in fig. 6, second is slidably matched portion 311 as that can be equipped with guiding surface 221 with sliding block, the end of the open end of sliding slot.By This, when sliding block and sliding slot cooperate, guiding surface 221 can play the role of guiding, consequently facilitating sliding block slides into sliding slot.

In some embodiments of the utility model, as shown in Figure 5 and Figure 6, first be slidably matched portion 220 and second sliding Auxiliary section 311 can be one-to-one multiple.Cooperate between the first connection terminal 310 and card line seat 20 thus, it is possible to improve Fastness and reliability.As shown in figure 5, the upper surface of card line seat 20 is set, there are two sliding slots, correspondingly, as shown in fig. 6, first The lower end surface of connection terminal 310 is set there are two sliding block, and two sliding blocks and two sliding slots correspond and cooperate.

According to the aircraft 100 of the utility model embodiment, aircraft 100 includes: rack, and rack is use described above In the rack of aircraft 100.

According to the aircraft 100 of the utility model embodiment, it is slidably matched portion by first portion 220 and second that is slidably matched Under the action of 311, the convenience assembled between connection component 30 and card line seat 20 and high efficiency can be improved.Moreover, when first Be slidably matched portion 220 and second be slidably matched portion 311 cooperate when, the first retaining part 211 and the second retaining part 312 can mutually stop To cooperation, to limit the opposite sliding between connection component 30 and card line seat 20, to realize connection component 30 and card line seat Solid and reliable assembly between 20 effectively prevents in 100 operational process of aircraft, and vibration occurs and leads to aircraft 100 The unstable problem of circuit connection.

Some embodiments according to the present utility model, aircraft 100 can also include electronic equipment 40, electronic equipment 40 with Connection component 30 connects.It is understood that aircraft 100 can be improved by the way that electronic equipment 40 is arranged on aircraft 100 Functional diversity.Moreover, electronic equipment 40 is connected by connection component 30, the reliability of the connection of electronic equipment 40 can be improved Stability is starved well, effectively prevents the reliability and stability that aircraft 100 occurs vibration and influences the connection of electronic equipment 40.

In some embodiments of the utility model, electronic equipment 40 can be winged control module 410, communication module 420, electricity Mode transfer block 430 or switching circuit board component 440 etc..It should be noted that flying control module 410 can be used for controlling aircraft 100 Flight attitude；Communication module 420 can be used for the communication of aircraft 100, and aircraft 100 is made to have good signal interaction function Energy；Electric mode transfer block 430 can be used for controlling the revolving speed of the Power Component 910 of aircraft 100, to control the flight of aircraft 100 Speed and heading；Adapter plate for circuit component 440 can be used for transferring the connection line of each module, make the line of aircraft 100 Road layout is more compact and reasonable.As a result, by the way that different electronic equipments 40 is arranged on aircraft 100, aircraft can be improved 100 overall performance.

Referring to Fig. 1-Figure 11 with a specific embodiment detailed description according to the flight of the utility model embodiment Device 100.It is worth understanding, described below is only exemplary description, rather than to the concrete restriction of the utility model.

As shown in Figure 1, Figure 2, shown in Fig. 9-Figure 11, aircraft 100 can be unmanned plane.Aircraft 100 can be used for agro-farming production The activities such as pesticide spraying or moisture sprinkling irrigation are carried out to crops in industry.Certainly, aircraft 100 can be used for Forest Fire The other fields such as the sprinkling of extinguishing fluid, photography of taking photo by plane, electric inspection process, environmental monitoring, forest fire protection and disaster inspection in calamity.

Referring to shown in Fig. 9-Figure 11, aircraft 100 includes: fuselage 10, horn 90, undercarriage 14, Power Component 910, storage Liquid container 810, battery 820, electronic equipment 40 and connection component 30 etc..Horn 90 is distributed in around fuselage 10 and and fuselage 10 are fixedly connected.Undercarriage 14 is fixed on 10 lower section of fuselage to guarantee the stability of 100 take-off and landing of aircraft, Power Component 910 are fixed on end of the horn 90 far from fuselage 10, and Power Component 910 provides lift, liquid storage container for the flight of aircraft 100 810 are equipped on fuselage 10 for containing article to be sprayed or to be transported, and battery 820 is fixed on fuselage 10 for flight The Power Component 910 of device 100 provides power, and electric mode transfer block 430 and control module are fixed on fuselage 10, for controlling flight The flight attitude of device 100.

Referring to shown in Fig. 9, fuselage 10 includes top plate 12, bottom plate 11 and installing frame 13, wherein top plate 12 is used for bottom plate 11 Carry described electronic equipment 40 etc..Installing frame 13 has the first loading space 134 and the second loading space 135, liquid storage container 810 In the first loading space 134, battery 820 is set in the second loading space 135.Thus, it is possible to avoid 810 He of liquid storage container It is interfered between battery 820, improves the fastness and reliability that liquid storage container 810 and battery 820 are fixed.

As shown in Figure 3-Figure 5, card line seat 20 is connect with fuselage 10, and the upper surface of card line seat 20 is equipped with the first retaining part 211 It is slidably matched portion 220 with first.Wherein, first portion 220 is slidably matched as sliding slot, sliding slot is spaced two, sliding slot Open end is equipped with guiding surface 221.

In conjunction with shown in Fig. 2, Fig. 6-Fig. 8, connection component 30 includes: the first connection terminal 310 and second connection end 320, First connection terminal 310 is electrically connected with second connection end 320, and the lower end surface of the first connection terminal 310 is equipped with the second sliding and matches Conjunction portion 311 and the second retaining part 312, the cross section of the second retaining part 312 are triangle, and second is slidably matched portion 311 as interval Two sliding blocks being arranged.

The front side wall of card line seat 20 is equipped with the multiple extensions 210 for being directed away from sliding slot extension, and multiple extensions 210 are along card The length direction interval of line seat 20 is arranged, and each extension 210 is tilted along direction from the front to the back, from top to bottom to be extended, and extends Multiple reinforcing ribs 212 are equipped at intervals in portion 210, the part of the upper surface of extension 210 raises upward to form the first retaining part 211。

As shown in fig. 6, the first end of the first connection terminal 310 towards shown second connection end 320 is equipped with assembles post 313, the periphery wall of assembles post 313 is equipped with cooperation hook 3130, and cooperation hook 3130 can be stretched along the radial direction of assembles post 313 Contracting.Second connection end 320 is equipped with pilot hole 321 compatible with assembles post 313.Second connection end 320 is additionally provided with and fills The cooperation card slot 322 that distribution 321 is connected to, when assembles post 313 protrudes into pilot hole 321, cooperation hook 3130 and cooperation card slot 322 block Connect cooperation.

It is slidably matched under the action of portion 311 by first portion 220 and second that is slidably matched as a result, connection group can be improved The convenience and high efficiency assembled between part 30 and card line seat 20.Moreover, when first portion 220 that is slidably matched is slidably matched with second When portion 311 cooperates, the first retaining part 211 and the second retaining part 312 mutually can only support cooperation, to limit connection component 30 and card Opposite sliding between line seat 20, to realize the solid and reliable assembly between connection component 30 and card line seat 20, effectively keeps away Exempt from 100 operational process of aircraft, vibration has occurred and the problem that causes the circuit connection of aircraft 100 unstable.

In the description of this specification, reference term " one embodiment ", " some embodiments ", " illustrative examples ", The description of " example ", " specific example " or " some examples " etc. means specific features described in conjunction with this embodiment or example, knot Structure, material or feature are contained at least one embodiment or example of the utility model.In the present specification, to above-mentioned art The schematic representation of language may not refer to the same embodiment or example.Moreover, description specific features, structure, material or Person's feature can be combined in any suitable manner in any one or more of the embodiments or examples.

While there has been shown and described that the embodiments of the present invention, it will be understood by those skilled in the art that: These embodiments can be carried out with a variety of variations, modification, replacement in the case where not departing from the principles of the present invention and objective And modification, the scope of the utility model are defined by the claims and their equivalents.

Claims (13)

1. a kind of rack for aircraft characterized by comprising

Fuselage；

Card line seat, the card line seat are connect with the fuselage, and the card line seat is equipped with the first retaining part and first and is slidably matched portion；

Connection component, the connection component are equipped with the second retaining part to offset with first retaining part, and the connection component is set Have and be slidably matched portion with described first portion compatible second that is slidably matched, described second portion that is slidably matched only is supported with described second Portion along described second be slidably matched portion extending direction interval be arranged, when described first be slidably matched portion and it is described second slide match When conjunction portion cooperates, first retaining part and second retaining part only support cooperation, with the fixation connection component and the card Line seat.

2. the rack according to claim 1 for aircraft, which is characterized in that the connection component includes:

First connection terminal, first connection terminal are equipped with described second and are slidably matched portion and second retaining part；

Second connection end, second connection end are electrically connected with first connection terminal.

3. the rack according to claim 2 for aircraft, which is characterized in that described second is slidably matched portion and described Second retaining part is set to the surface towards the card line seat of first connection terminal, and first portion of being slidably matched is set to The surface towards first connection terminal of the card line seat.

4. the rack according to claim 2 for aircraft, which is characterized in that the front side wall of the card line seat is equipped with court To the extension extended far from first portion of being slidably matched, the part of the upper surface of the extension raises upward to be formed State the first retaining part.

5. the rack according to claim 4 for aircraft, which is characterized in that the extension along from the front to the back, by Upper downwardly direction inclination extends.

6. the rack according to claim 4 for aircraft, which is characterized in that be equipped at intervals on the extension multiple Reinforcing rib.

7. the rack according to claim 2 for aircraft, which is characterized in that the cross section of second retaining part is Triangle.

8. the rack according to claim 2 for aircraft, which is characterized in that first connection terminal is shown in The first end of second connection end is equipped with assembles post, and second connection end is equipped with assembly compatible with the assembles post Hole.

9. the rack according to claim 8 for aircraft, which is characterized in that the periphery wall of the assembles post is equipped with Cooperate hook, the cooperation hook is scalable along the radial direction of the assembles post, second connection end equipped with it is described The cooperation card slot of pilot hole connection, when the assembles post protrudes into the pilot hole, the cooperation hook and the cooperation card slot card Connect cooperation.

10. the rack according to claim 1 for aircraft, which is characterized in that first portion of being slidably matched is to slide Slot, second portion of being slidably matched are sliding block, and the end of the open end of the sliding slot is equipped with guiding surface.

11. the rack according to claim 1 for aircraft, which is characterized in that described first is slidably matched portion and institute It is one-to-one multiple for stating second portion of being slidably matched.

12. a kind of aircraft characterized by comprising rack, the rack are according to any one of claim 1-11 The rack for aircraft.

13. aircraft according to claim 12, which is characterized in that it further include electronic equipment, the electronic equipment and institute State connection component connection.