CN211810295U

CN211810295U - Cabin body and automatic airport

Info

Publication number: CN211810295U
Application number: CN202020005052.9U
Authority: CN
Inventors: 杨祥磊
Original assignee: Beijing Jingdong Qianshi Technology Co Ltd
Current assignee: Beijing Jingdong Qianshi Technology Co Ltd
Priority date: 2020-01-02
Filing date: 2020-01-02
Publication date: 2020-10-30
Anticipated expiration: 2030-01-02

Abstract

The utility model discloses a cabin body and automatic airport relates to aircraft technical field. This cabin body includes casing, cabin cover, take off and land platform and connecting rod, and fore-and-aft slide opening has been seted up to the side of casing, wherein: the hatch cover is connected to the top of the shell in a sliding manner and is connected with the upper end of the connecting rod; the lifting platform is located inside the shell, the side portion of the lifting platform penetrates through the sliding hole to be connected with the lower end of the connecting rod, and the lifting platform can slide along the sliding hole. The embodiment can complete the lifting and uncovering of the automatic airport under the driving of a single power source, and the system has a simple structure and high opening speed.

Description

Cabin body and automatic airport

Technical Field

The utility model relates to an aircraft technical field, concretely relates to cabin body and automatic airport.

Background

At present, be equipped with automatic airport for unmanned aerial vehicle and become commodity circulation unmanned aerial vehicle, patrol and examine the new direction of development of unmanned aerial vehicle etc. automatic airport can provide the platform of taking off and land for unmanned aerial vehicle, realizes automatic taking off and land to and automatic charging or automatic battery of changing have the personnel that reduce and participate in, raise the efficiency, extend effects such as journey.

The automatic airport mainly comprises three parts, namely an airport, an unmanned aerial vehicle and a patrol operation management system. The airfield mainly has the following two structures: one of the cabin covers is a cabin cover, the cabin cover can provide a storage space for the unmanned aerial vehicle, but the cabin cover has high requirements on structural rigidity and strength, and the device has extremely high weight, so that the requirements on a power device are high, and the cost is high; its two are flat lid, because the flat board can not provide the storage space for unmanned aerial vehicle, consequently need increase the platform of taking off and land, go up and down through the platform and provide unmanned aerial vehicle parking space, nevertheless uncap and take off and land the transmission that the platform needs two sets of power, open earlier and cover jacking again, the system is complicated, and opening speed is slow, and is with high costs.

SUMMERY OF THE UTILITY MODEL

For the system complicacy among the solution prior art, require the height to power device to and the higher problem of cost, the utility model provides a cabin body and automatic airport can accomplish the lift and the uncapping of automatic airport under the drive of single power supply, and system simple structure opens fastly.

To achieve the above objects, according to one aspect of the embodiments of the present invention, a capsule is provided.

The utility model discloses cabin body, including casing, cabin cover, take off and land platform and connecting rod, fore-and-aft slide opening has been seted up to the side of casing, wherein:

the hatch cover is connected to the top of the shell in a sliding manner and is connected with the upper end of the connecting rod;

the lifting platform is located inside the shell, the side portion of the lifting platform penetrates through the sliding hole to be connected with the lower end of the connecting rod, and the lifting platform can slide along the sliding hole.

Optionally, the lifting device is arranged on the lower side of the lifting platform and used for driving the lifting platform to lift.

Optionally, the lifting device is an electric push rod, a lead screw mechanism or a scissor lift platform.

Optionally, the hatch cover comprises a hatch cover plate and a connecting rod seat, and the side of the landing platform is provided with an angle plate, wherein:

the cabin cover plate is arranged in a groove shape, and the inner side edge of the cabin cover plate is connected with a connecting rod seat;

the angle plate penetrates through the sliding hole and is connected with the lower end of the connecting rod;

the upper ends of the connecting rods are connected with the connecting rod seats.

Optionally, the cabin cover plate further comprises a sliding rail, the upper side of the sliding rail is connected with the edge of the groove of the cabin cover plate, and the lower side of the sliding rail is connected with the shell.

Optionally, a slider is disposed on the top of the housing, and the slider is connected to the lower side of the slide rail.

Optionally, a longitudinal guide rail is arranged in the shell, and the lifting platform is provided with a guide sleeve in sliding fit with the guide rail.

Optionally, the side of the landing platform is further provided with a reinforcing rib.

Optionally, the top of the housing is connected with symmetrically arranged hatches, and the two hatches are respectively connected with the lifting platform through connecting rods on two sides, so that the two hatches can synchronously slide towards each other or oppositely.

To achieve the above object, according to still another aspect of the embodiments of the present invention, a rotorcraft is provided.

The utility model discloses an automatic airport, including aircraft, charging device, stand-by battery and the utility model discloses the cabin body of the embodiment, wherein:

the charging device and the standby battery are arranged in the shell of the cabin body;

the landing platform of the cabin is used for parking at least one aircraft.

An embodiment in the above-mentioned utility model has following advantage or beneficial effect:

1. the vertical motion of the lifting platform is converted into the horizontal motion of the hatch cover through the connecting rod, so that the lifting and the uncovering of an automatic airport are completed under the driving of a single power source, and the system has a simple structure and high opening speed;

2. the flat plate type hatch cover has smaller volume, can meet the requirements of rigidity and strength by using less materials, and has lower cost;

3. the sliding rail is used for connecting the shell and the hatch cover, so that the hatch cover can flexibly slide on the top of the shell, and the sliding process is smooth;

4. the longitudinal sliding of the lifting platform is reliable vertical movement through the sliding fit of the guide sleeve and the guide rail as well as the angle plate and the sliding hole.

Drawings

Fig. 1 is a schematic view of a cabin according to an embodiment of the present invention;

fig. 2 is a partial sectional view of a cabin according to an embodiment of the present invention;

fig. 3 is a schematic view of a shell of a cabin according to an embodiment of the present invention;

fig. 4 is a schematic view of a landing platform of a cabin according to an embodiment of the present invention;

fig. 5 is a schematic view of a deck lid of a cabin according to an embodiment of the present invention;

fig. 6 is a schematic view of a closed state of a cabin according to an embodiment of the present invention.

In the figure, the position of the upper end of the main shaft,

1-a shell; 11-a slide hole; 12-a slide block; 13-a guide rail; 2-a hatch cover; 21-a deck plate; 22-connecting rod seat; 3-a take-off and landing platform; 31-gussets; 32-a guide sleeve; 4-a connecting rod; 5-a lifting device; 6-a slide rail; 7-an aircraft.

Detailed Description

Exemplary embodiments of the invention are described below with reference to the accompanying drawings, in which various details of embodiments of the invention are included to assist understanding, and which are to be considered exemplary only. Accordingly, those of ordinary skill in the art will recognize that various changes and modifications of the embodiments described herein can be made without departing from the scope and spirit of the invention. Also, descriptions of well-known functions and constructions are omitted in the following description for clarity and conciseness.

The automatic airport is a movable device responsible for professional and complete maintenance of the unmanned aerial vehicle, and comprises automatic cabin opening and closing, automatic lifting of a take-off platform, intelligent temperature and humidity regulation, centering and returning of the unmanned aerial vehicle, quick charging and the like.

The existing airfield mainly has the following two structures:

1. the cabin cover is of an unclosed plate shell structure, is large in size and is like a stainless steel bowl divided into two halves in structure, if the rigidity is insufficient, large deformation occurs, and the strength is insufficient, so that damage is easy to occur, the cabin cover has high requirements on structural rigidity and strength, the material consumption needs to be increased for increasing the rigidity and the strength, and the overall weight of little molehill is increased;

2. the flat lid because the flat board can not provide the storage space for unmanned aerial vehicle, consequently need increase the platform of taking off and land, goes up and down through the platform and provides unmanned aerial vehicle parking space, nevertheless uncaps and takes off and land the transmission that the platform needs two sets of power, uncaps earlier and jacks again, and the system is complicated, and opening speed is slow, and is with high costs.

Therefore, the utility model discloses a cabin body and automatic airport to the cabin is automatic opens and shuts and automatic lift, provides a simple structure, can the automatic airport transmission system that links.

As shown in fig. 1, an embodiment of the present invention provides a cabin body mainly including: the device comprises a shell 1, a hatch cover 2, a take-off and landing platform 3 and a connecting rod 4.

Wherein, the hatch 2 is slidably connected to the top of the housing 1, that is, the hatch 2 is covered on the top of the housing 1, and the hatch 2 can slide along the top of the housing 1 transversely. The lifting platform 3 is located inside the shell 1, a longitudinal sliding hole 11 is formed in the side face of the shell 1, and the lifting platform 3 can slide along the sliding hole 11. The side part of the lifting platform 3 passes through the sliding hole 11 to be connected with the lower end of the connecting rod 4, and the hatch cover 2 is connected with the upper end of the connecting rod 4. Due to the limitation of the sliding hole 11, the lifting platform 3 can only longitudinally slide when in work, the cabin cover 2 is in sliding connection with the shell 1, the cabin cover 2 can only transversely slide when in work, when the lifting platform 3 slides upwards, the lower end of the connecting rod 4 moves upwards under the driving of the lifting platform 3, but the connecting rod 4 cannot push the cabin cover 2 upwards but transversely push the cabin cover 2, so that the cabin cover 2 slides outwards from the top of the shell 1, and the cabin body is opened; when the lifting platform 3 slides downwards, the lower end of the connecting rod 4 moves downwards under the driving of the lifting platform 3, but the connecting rod 4 cannot pull the cabin cover 2 downwards, but pulls the cabin cover 2 transversely, so that the cabin cover 2 slides inwards from the top of the shell 1, and the cabin body is closed. Vertical motion of the take-off and landing platform 3 is converted into horizontal motion of the hatch cover 2 through the connecting rod 4, lifting and uncovering of the automatic airport are achieved under the driving of a single power source, a power system special for opening and closing the hatch cover 2 does not need to be added, the system is simple in structure and high in opening speed, the flat hatch cover 2 is small in size, requirements for rigidity and strength can be met by using few materials, and the cost is low.

As shown in fig. 1 and 2, a cabin according to an embodiment of the present invention may further include a lifting device 5 and a sliding rail 6.

Wherein, the lifting device 5 is arranged at the lower side of the lifting platform 3 and used for driving the lifting platform 3 to lift. The lifting device 5 may be a lifting structure such as an electric push rod, a screw mechanism or a scissor-type lifting platform, wherein the electric push rod is an electric driving device for converting the rotary motion of a motor into the linear reciprocating motion of the push rod. The device can be used as an execution machine in various simple or complex process flows to realize remote control, centralized control or automatic control; the screw rod lifter is also called a spiral transmission mechanism. The screw rod lifter is mainly used for converting rotary motion into linear motion or converting linear motion into rotary motion, and comprises a worm gear reducer and a screw rod, wherein the speed reduction part is in worm transmission, the worm drives the worm gear to realize speed reduction, and the worm gear is equivalent to a nut of the lifting screw rod and is matched with the lifting screw rod; a scissor type lifting platform is a lifting device for lifting goods or a lifting operation platform by utilizing a scissor structure, and has the characteristics of stable structure, low failure rate, reliable operation, safety, high efficiency and simple and convenient maintenance. In addition, when adopting electric putter as taking off and land device 5, connect two electric putter at the downside of taking off and land platform 3, and can make two electric putter be located the central line of taking off and land platform 3 to with the central symmetry of taking off and land platform 3, thereby make the platform 3 atress of taking off and land more even.

The sliding rail 6 is also called a guide rail or a slideway, and refers to a hardware connecting component which is fixed on a cabinet body of furniture and is used for the in-and-out movement of a drawer or a cabinet plate of the furniture, and is suitable for the connection of wooden parts of cabinets, furniture, document cabinets, bathroom cabinets and the like and drawers of furniture such as steel drawers and the like. The utility model discloses the cabin body utilizes slide rail 6 to connect casing 1 and cabin cover 2, specifically, the upside of slide rail 6 and the recess edge connection of cabin cover board 21 (not shown in the figure), and the downside of slide rail 6 is connected with slider 12 (not shown in the figure) to make cabin cover 2 can slide in the top of casing 1 is nimble, and the process of sliding is smooth and easy, just can promote cabin cover 2 as long as exert less power, realizes that the level of cabin cover 2 is opened.

As shown in fig. 3, the hatch 2 is a flat plate-type plate shell structure, the hatch 2 may include a hatch 21 and a connecting rod seat 22, the hatch 21 is configured in a groove shape (i.e. three sides of the plate shell are bent downward, so that the hatch 21 can reduce dust or rain water from entering the shell 1 after covering the shell 1), and the connecting rod seat 22 is connected to an inner edge of the hatch 21, and the connecting rod seat 22 is used for connecting with a connecting rod 4 (not shown) to transmit power provided by the lifting device 5 (not shown) to the hatch 21.

As shown in fig. 4, the casing 1 has a rectangular parallelepiped structure, and can be formed by assembling a frame with pipes inside and providing wall plates outside, and the wall plates at the front and back sides are provided with two longitudinal elongated slits as sliding holes 11 for transmitting the power of the lifting device 5 (not shown) to the connecting rod 4 (not shown). On both sides of the top of the housing 1, sliders 12 are arranged for cooperation with slide rails under the hatch 2 (not shown in the figures) so that the hatch 2 can only slide laterally. Four vertical cylindrical guide rails are provided at four corners inside the housing 1, and are used as guide rails 13 for guiding the landing platform 3 (not shown). In addition, other parts of the housing 1 can be arranged according to the needs, such as adding wheels at the bottom and the like.

As shown in fig. 5, the lifting platform 3 has a rectangular flat plate structure as a whole, and the lifting platform 3 may further include angle plates 31, guide sleeves 32, and reinforcing ribs (not shown). Wherein, the angle plate 31 is arranged at the side of the landing platform 3, four angle plates 31 (two on each side) can be arranged at two sides of the landing platform 3, the angle plates 31 are connected with the lower end of the connecting rod 4 (not shown in the figure) through the sliding holes 11 (not shown in the figure), and the power transmission provided by the landing device 5 (not shown in the figure) is transmitted through the angle plates 31; the position of the guide sleeve 32 can correspond to the position of the guide rail 13, the guide sleeve 32 is arranged at four corners of the lifting platform 3, the guide sleeve 32 is sleeved outside the guide rail 13 (not shown in the figure), and the longitudinal sliding of the lifting platform 3 is reliable vertical movement through the sliding fit of the guide sleeve 32 and the guide rail 13 and the angle plate 31 and the sliding hole 11. The strengthening rib can set up in the side of platform 3 that takes off and land, improves whole platform 3's that takes off and land rigidity through the strengthening rib, in addition, can carry out the turn-ups to platform 3 that takes off and land, will turn up the part and regard as the strengthening rib. Flanging refers to a method for forming a straight wall or a flange with a certain angle along a closed or unclosed curve edge on a plane part or a curved part of a blank by using the action of a die.

With continued reference to fig. 1, 2 and 6, as a preferred embodiment, the cabin of the embodiment of the present invention may be in a split form, i.e. two covers 2 symmetrically arranged on the top of the casing 1, and the two covers 2 can slide towards or away from each other. Each hatch 2 is connected to the top of the shell 1 through two slide rails 6, and each hatch 2 is connected with the lifting platform 3 through two connecting rods 4 on two sides, and correspondingly, two slide holes 11 are respectively arranged on the front and back sides of the shell 1, and two angle plates 31 are respectively arranged on two sides of the lifting platform 3.

It is to be noted that each hatch 2 can be connected to the landing platform 3 using one or more links 4, and accordingly each link 4 corresponds to a particular gusset 31 and slide opening 11, i.e. the number of links 4, gussets 31 and slide openings 11 is the same and the position corresponds. When the angle plate 31 slides to the lower part of the sliding hole 11, the two cabin covers 2 are contacted, and the cabin body is closed; when the corner plate 31 is slid to the upper part of the slide hole 11, the two hatch covers 2 are separated and the hatch is opened.

It should be noted that the utility model discloses the cabin body can regard as the automatic airport that aircraft such as unmanned aerial vehicle used, can also regard as show cupboard or express delivery storing compartment etc..

Furthermore, the embodiment of the utility model provides an automatic airport is still provided, mainly include aircraft 7, charging device, stand-by battery and the utility model provides a cabin body.

The automatic airport can be used for logistics transportation, inspection operation and the like. Wherein, the platform 3 that takes off and land of cabin body is used for parking at least an aircraft 7, and charging device and reserve battery set up in the casing 1 of cabin body, and charging device charges for aircraft 7, and reserve battery can make 7 quick supplementary electric quantities of aircraft, improves work efficiency. The automatic airport can provide a take-off and landing platform for aircrafts 7 such as unmanned planes and the like, and realizes automatic take-off and landing, automatic charging or automatic battery replacement and other operations.

As can be seen from the above description, the cabin and the automatic airport according to the embodiments of the present invention have at least the following advantages or beneficial effects:

1. the vertical motion of the take-off and landing platform 3 is converted into the horizontal motion of the hatch cover 2 through the connecting rod 4, so that the automatic lifting and uncovering of the airport are completed under the driving of a single power source, and the system has a simple structure and high opening speed;

2. the flat plate type hatch cover 2 has smaller volume, can meet the requirements of rigidity and strength by using less materials, and has lower cost;

3. the sliding rail 6 is used for connecting the shell 1 and the hatch cover 2, so that the hatch cover 2 can flexibly slide on the top of the shell 1, and the sliding process is smooth;

4. the longitudinal sliding of the lifting platform 3 is reliably vertical movement through the sliding fit of the guide sleeve 32 and the guide rail 13, and the angle plate 31 and the sliding hole 11.

The above is only a preferred embodiment of the present invention, and should not be limited to the present invention, and any modifications, equivalent replacements, simple improvements and the like made in the spirit of the present invention should be included in the protection scope of the present invention.

Claims

1. The utility model provides a cabin body, its characterized in that, includes casing (1), cabin cover (2), take-off and landing platform (3) and connecting rod (4), and fore-and-aft slide opening (11) have been seted up to the side of casing (1), wherein:

the hatch cover (2) is connected to the top of the shell (1) in a sliding manner, and the hatch cover (2) is connected with the upper end of the connecting rod (4);

the lifting platform (3) is positioned in the shell (1), the side part of the lifting platform (3) penetrates through the sliding hole (11) to be connected with the lower end of the connecting rod (4), and the lifting platform (3) can slide along the sliding hole (11).

2. The cabin body according to claim 1, further comprising a lifting device (5), wherein the lifting device (5) is disposed at the lower side of the lifting platform (3) and is used for driving the lifting platform (3) to lift.

3. Cabin according to claim 2, wherein the lifting device (5) is an electric push rod, a lead screw mechanism or a scissor lift platform.

4. Cabin according to claim 1, wherein the deck lid (2) comprises a deck lid (21) and a linkage base (22), and wherein the landing platform (3) is provided with gussets (31) at its sides, wherein:

the cabin cover plate (21) is arranged in a groove shape, and the inner side edge of the cabin cover plate (21) is connected with a connecting rod seat (22);

the angle plate (31) passes through the sliding hole (11) and is connected with the lower end of the connecting rod (4);

the upper end of the connecting rod (4) is connected with a connecting rod seat (22).

5. Cabin according to claim 4, further comprising a sliding rail (6), wherein the upper side of the sliding rail (6) is connected with the edge of the groove of the cabin cover plate (21), and the lower side of the sliding rail (6) is connected with the shell (1).

6. Cabin according to claim 5, wherein the top of the shell (1) is provided with a sliding block (12), and the sliding block (12) is connected with the lower side of the sliding rail (6).

7. Cabin according to claim 1, wherein longitudinal guide rails (13) are arranged in the housing (1), and the lifting platform (3) is provided with guide sleeves (32), wherein the guide sleeves (32) are in sliding fit with the guide rails (13).

8. Cabin according to claim 1, wherein the landing platform (3) is further provided with reinforcing ribs on its sides.

9. A cabin according to any one of claims 1-8, characterized in that the top of the shell (1) is connected with symmetrically arranged hatches (2), and both hatches (2) are connected with the take-off and landing platform (3) by connecting rods (4) on both sides, respectively, so that both hatches (2) can synchronously slide towards each other or oppositely.

10. An automated airport, comprising an aircraft (7), a charging device, a battery backup and a cabin according to any one of claims 1 to 9, wherein:

the charging device and the standby battery are arranged in a shell (1) of the cabin body;

the landing platform (3) of the cabin is used for parking at least one aircraft (7).