CN217049069U - Top cabin opening structure for unmanned aerial vehicle-mounted departure - Google Patents
Top cabin opening structure for unmanned aerial vehicle-mounted departure Download PDFInfo
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- CN217049069U CN217049069U CN202220591444.7U CN202220591444U CN217049069U CN 217049069 U CN217049069 U CN 217049069U CN 202220591444 U CN202220591444 U CN 202220591444U CN 217049069 U CN217049069 U CN 217049069U
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Abstract
The utility model discloses a top cabin structure of opening cabin of unmanned aerial vehicle machine-mounted departure relates to unmanned aerial vehicle machine-mounted departure technical field. The utility model comprises a cabin body and a sealing cover; the top of the cabin body is provided with a departure skylight; the sealing cover is hinged and matched with the departure skylight; the surface of the cabin body is fixedly connected with a guide assembly; the surface of the sealing cover is fixedly connected with a steel wire rope; one end of the steel wire rope sequentially penetrates through the guide assembly and the rope outlet pipe to enter the cabin body; one end of the steel wire rope is fixedly connected with a balancing weight; the bottom surface of the balancing weight is fixedly connected with a piston; the sealing tube is in sliding fit with the piston; the peripheral side surface of the sealing pipe is symmetrically provided with an air inlet hose and an air outlet pipe close to the bottom surface. The utility model discloses a gas injection in the control system control air pump of cabin internal portion to the sealed tube drives the piston and moves up together with the balancing weight under reset spring's elastic force for L shape push pedal promotes sealed lid, and sealed lid covers the skylight of dispatching a car, realizes that the automation of the sealed lid of skylight of dispatching a car is opened and sealed, improves work efficiency.
Description
Technical Field
The utility model belongs to the technical field of unmanned aerial vehicle carries the departure, especially relate to an unmanned aerial vehicle carries the overhead compartment structure of opening of departure.
Background
The unmanned airborne dispatching vehicle mainly serves as an unmanned airborne dispatching and networking management and control system, and the whole vehicle can be divided into three areas of an unmanned airborne dispatching cabin, an intelligent control comprehensive guarantee system and a cockpit; the unmanned aerial vehicle is dispatched by adopting a lifting platform to automatically control the unmanned aerial vehicle to be fixed in transportation, lifted out of the cabin and taken off.
For reducing use cost, the articulated form of two-sided sealing door is adopted mostly to the on-vehicle hatch door of current small-size unmanned aerial vehicle machine-mounted departure, and small-size unmanned aerial vehicle machine-mounted departure need open two-sided door earlier before work, carries out unmanned aerial vehicle transportation again and lifts out the cabin and take off, need close two-sided door after the use, and degree of automation is lower, has reduced work efficiency.
SUMMERY OF THE UTILITY MODEL
The utility model aims to provide a top cabin opening structure for unmanned aerial vehicle to take out, which pulls a steel wire rope to open a sealing cover under the gravity action of a balancing weight in an initial state, and the sealing cover pushes an L-shaped push plate to extrude a reset spring in the rotating process; gas injection in the control system control air pump to the sealed pipe through cabin body inside drives the piston and moves up together with the balancing weight, under reset spring's elastic force for L shape push pedal promotes sealed lid, and sealed lid covers the skylight of dispatching a car, realizes that the automation of the sealed lid of skylight of dispatching a car is opened and is sealed, improves work efficiency.
In order to solve the technical problem, the utility model discloses a realize through following technical scheme:
the utility model relates to a top cabin opening structure for unmanned aerial vehicle-mounted departure, which comprises a cabin body and a sealing cover; the top of the cabin body is provided with a departure skylight; the sealing cover is in hinged fit with the departure skylight; the surface of the cabin body is fixedly connected with a guide assembly; the surface of the cabin body is provided with a rope outlet pipe in a penetrating way; the surface of the sealing cover is fixedly connected with a steel wire rope; one end of the steel wire rope sequentially penetrates through the guide assembly and the rope outlet pipe to enter the cabin body;
one end of the steel wire rope is fixedly connected with a balancing weight; the bottom surface of the balancing weight is fixedly connected with a piston; the inner wall of the cabin body is fixedly connected with a fixing plate; a sealing pipe is fixedly connected between the fixing plate and the inner top surface of the cabin body; the sealing tube is in sliding fit with the piston;
the rope outlet pipe and the sealing pipe are coaxially arranged; and the peripheral side surface of the sealing pipe is symmetrically provided with an air inlet hose and an air outlet pipe close to the bottom surface.
Further, an iron plate is fixedly connected to the side surface of the sealing cover; the side surface of the departure skylight is fixedly connected with a magnetic plate; the iron plate and the magnetic plate are mutually attracted.
Further, the guide assembly includes a support plate; the side surface of the supporting plate is fixedly connected with a first mounting plate and a second mounting plate from top to bottom in sequence; a guide wheel is rotationally matched on the side surface of the first mounting plate; pulleys are symmetrically and rotationally matched on the side surfaces of the second mounting plate, which are positioned on two sides of the steel wire rope; the steel wire rope sequentially penetrates through the guide wheel and the wheel grooves on the two pulleys.
Furthermore, the peripheral side surface of the air outlet pipe is provided with a control valve.
Furthermore, a sliding channel is formed on the surface of the cabin body close to the departure skylight; the surface of the cabin body is fixedly connected with a baffle plate; the sliding channel is in sliding fit with a sliding plate; and a return spring is fixedly connected between the sliding plate and the baffle.
Furthermore, a limiting rod is fixedly connected between the inner wall of the sliding channel and the side surface of the departure skylight; the sliding plate is in sliding fit with the limiting rod; the top of the sliding plate is fixedly connected with an L-shaped push plate.
The utility model discloses following beneficial effect has:
the utility model opens the sealing cover by pulling the steel wire rope under the gravity action of the balancing weight, and the sealing cover pushes the L-shaped push plate to extrude the reset spring in the rotating process; gas injection in to the sealed tube is controlled through the inside control system control air pump in cabin body, drives the piston and moves up together with the balancing weight, under reset spring's elastic force for L shape push pedal promotes sealed lid, and sealed lid covers the skylight of dispatching a car, realizes that the automation of the sealed lid of skylight of dispatching a car is opened and is sealed, improves work efficiency.
Drawings
In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments are briefly introduced below, it is obvious that the drawings in the description below are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.
Fig. 1 is a schematic structural view of the overhead cabin opening structure of the unmanned aerial vehicle equipped for departure.
Fig. 2 is a schematic structural view of the cabin of the present invention.
Fig. 3 is an enlarged view of a structure in fig. 2 according to the present invention.
In the drawings, the reference numbers indicate the following list of parts:
the car comprises a cabin body 1, a sealing cover 2, a car-departure skylight 3, a guide assembly 4, a rope outlet pipe 5, a steel wire rope 6, a counterweight 7, a piston 8, a fixing plate 9, a sealing pipe 10, an air inlet hose 11, an air outlet pipe 12, an iron plate 13, a magnetic plate 14, a support plate 15, a guide wheel 16, a pulley 17, a control valve 18, a sliding channel 19, a baffle plate 20, a sliding plate 21, a return spring 22, a limiting rod 23, a push plate 24-L-shaped, a first mounting plate 25 and a second mounting plate 26.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments of the present invention, all other embodiments obtained by a person of ordinary skill in the art without creative efforts belong to the protection scope of the present invention.
Referring to fig. 1-3, the present invention relates to a top cabin opening structure for unmanned aerial vehicle-mounted departure, which comprises a cabin body 1 and a sealing cover 2; the top of the cabin 1 is provided with a departure skylight 3; the sealing cover 2 is hinged and matched with the departure skylight 3; the surface of the cabin body 1 is fixedly connected with a guide component 4; the surface of the cabin body 1 is provided with a rope outlet pipe 5 in a penetrating way; the surface of the sealing cover 2 is fixedly connected with a steel wire rope 6; one end of a steel wire rope 6 sequentially penetrates through the guide assembly 4 and the rope outlet pipe 5 to enter the cabin body 1;
one end of the steel wire rope 6 is fixedly connected with a balancing weight 7; the bottom surface of the balancing weight 7 is fixedly connected with a piston 8; the inner wall of the cabin body 1 is fixedly connected with a fixing plate 9; a sealing pipe 10 is fixedly connected between the fixing plate 9 and the inner top surface of the cabin body 1; the sealing tube 10 is in sliding fit with the piston 8;
the rope outlet pipe 5 and the sealing pipe 10 are coaxially arranged; an air inlet hose 11 and an air outlet pipe 12 are symmetrically arranged on the peripheral side surface of the sealing pipe 10 close to the bottom surface;
opening process of the sealing cover 2: the control valve 18 is in a closed state, and under the action of gravity of the balancing weight 7, the control valve and the piston 8 pull the steel wire rope 6 to descend along the sealing pipe 10, so that the sealing cover 2 is driven to rotate and open;
closing process of the sealing cover 2: the control valve 18 is in an open state, the control system in the cabin 1 controls the air pump to inject air into the sealing tube 10 through the air inlet hose 11, the piston 8 and the counterweight 7 are driven to ascend along the sealing tube 10, and the L-shaped push plate 24 is driven to push the sealing cover 2 to reset under the elastic acting force of the reset spring 22, so that the sealing cover 2 covers the departure skylight 3.
Wherein, the side surface of the sealing cover 2 is fixedly connected with an iron plate 13; the side surface of the departure skylight 3 is fixedly connected with a magnetic plate 14; the iron plate 13 and the magnetic plate 14 attract each other;
when the sealing cover 2 covers the sunroof 3, the iron plate 13 and the magnetic plate 14 attract each other to prevent the sealing cover 2 from rattling.
Wherein the guide assembly 4 comprises a support plate 15; the side surface of the supporting plate 15 is fixedly connected with a first mounting plate 25 and a second mounting plate 26 from top to bottom in sequence; the guide wheel 16 is rotatably matched on the side surface of the first mounting plate 25; pulleys 17 are symmetrically and rotatably matched on the side surfaces of the second mounting plates 26, which are positioned on the two sides of the steel wire rope 6; the steel wire rope 6 sequentially passes through the guide wheel 16 and the wheel grooves on the two pulleys 17;
one end of the steel wire rope 6 is fixedly installed on the surface of the sealing cover 2, and the other end of the steel wire rope passes through the guide wheel 16, the two pulleys 17 and the rope outlet pipe 5 once to enter the sealing pipe 10 and is fixedly connected with the surface of the balancing weight 7, so that the steel wire rope 6 is guided and limited.
Wherein, the peripheral side surface of the air outlet pipe 12 is provided with a control valve 18;
during the opening of the sealing cap 2, the control valve 18 is in the closed state; the control valve 18 is in an open state during the closing of the sealing cap 2.
Wherein, the surface of the cabin body 1 is provided with a sliding channel 19 near the departure skylight 3; the surface of the cabin body 1 is fixedly connected with a baffle plate 20; the sliding channel 19 is in sliding fit with a sliding plate 21; a return spring 22 is fixedly connected between the sliding plate 21 and the baffle plate 20;
a limiting rod 23 is fixedly connected between the inner wall of the sliding channel 19 and the side surface of the departure skylight 3; the sliding plate 21 is in sliding fit with the limiting rod 23; the top of the sliding plate 21 is fixedly connected with an L-shaped push plate 24;
during the rotation opening of the sealing cover 2, the L-shaped push plate 24 is pushed to slide along the sliding channel 19, thereby pressing the return spring 22.
The utility model discloses a concrete theory of operation does:
opening process of the sealing cover 2: the control valve 18 is in a closed state, and under the action of the gravity of the balancing weight 7, the control valve and the piston 8 pull the steel wire rope 6 to descend along the sealing pipe 10, so that the sealing cover 2 is driven to rotate and open; during the process of rotating and opening the sealing cover 2, the L-shaped push plate 24 is pushed to slide along the sliding channel 19, so that the return spring 22 is pressed;
closing process of the sealing cover 2: the control valve 18 is in an open state, the air pump is controlled by the control system in the cabin 1 to inject air into the sealing tube 10 through the air inlet hose 11, the piston 8 and the counterweight 7 are driven to ascend along the sealing tube 10, and the L-shaped push plate 24 is driven to push the sealing cover 2 to reset under the elastic action of the reset spring 22, so that the sealing cover 2 covers the departure skylight 3; the iron plate 13 and the magnetic plate 14 attract each other.
The preferred embodiments of the present invention disclosed above are intended only to help illustrate the present invention. The preferred embodiments are not intended to be exhaustive or to limit the invention to the precise forms disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the invention and its practical applications, thereby enabling others skilled in the art to best understand the invention and its practical application. The present invention is limited only by the claims and their full scope and equivalents.
Claims (6)
1. A top cabin opening structure for unmanned aerial vehicle-mounted departure comprises a cabin body (1) and a sealing cover (2); the top of the cabin body (1) is provided with a departure skylight (3); the sealing cover (2) is in hinged fit with the departure skylight (3);
the method is characterized in that:
the surface of the cabin body (1) is fixedly connected with a guide assembly (4); a rope outlet pipe (5) penetrates through the surface of the cabin body (1); the surface of the sealing cover (2) is fixedly connected with a steel wire rope (6); one end of the steel wire rope (6) sequentially penetrates through the guide assembly (4) and the rope outlet pipe (5) to enter the cabin body (1);
one end of the steel wire rope (6) is fixedly connected with a balancing weight (7); the bottom surface of the balancing weight (7) is fixedly connected with a piston (8); the inner wall of the cabin body (1) is fixedly connected with a fixing plate (9); a sealing pipe (10) is fixedly connected between the fixing plate (9) and the inner top surface of the cabin body (1); the sealing tube (10) is in sliding fit with the piston (8);
the rope outlet pipe (5) and the sealing pipe (10) are coaxially arranged; the side surface of the periphery of the sealing tube (10) is symmetrically provided with an air inlet hose (11) and an air outlet tube (12) close to the bottom surface.
2. The structure for opening the top compartment of the unmanned aerial vehicle, according to claim 1, wherein an iron plate (13) is fixedly connected to the side of the sealing cover (2); the side surface of the departure skylight (3) is fixedly connected with a magnetic plate (14); the iron plate (13) and the magnetic plate (14) are mutually attracted.
3. The structure for the overhead cabin opening of a departure car on board an unmanned aerial vehicle according to claim 1, characterized in that said guide assembly (4) comprises a support plate (15); the side surface of the supporting plate (15) is fixedly connected with a first mounting plate (25) and a second mounting plate (26) from top to bottom in sequence; a guide wheel (16) is rotationally matched on the side surface of the first mounting plate (25); pulleys (17) are symmetrically matched with the side surface of the second mounting plate (26) in a rotating way and are positioned on two sides of the steel wire rope (6); the steel wire rope (6) sequentially passes through the guide wheel (16) and the wheel grooves on the two pulleys (17).
4. The structure of claim 1, wherein a control valve (18) is provided on the peripheral side of the outlet pipe (12).
5. The top cabin opening structure for the unmanned aerial vehicle to get out of the vehicle according to claim 1, wherein a sliding channel (19) is formed on the surface of the cabin body (1) close to the skylight (3) for getting out of the vehicle; the surface of the cabin body (1) is fixedly connected with a baffle plate (20); the sliding channel (19) is in sliding fit with a sliding plate (21); and a return spring (22) is fixedly connected between the sliding plate (21) and the baffle plate (20).
6. The overhead cabin opening structure for unmanned aerial vehicle-mounted departure according to claim 5, wherein a limiting rod (23) is fixedly connected between the inner wall of said sliding channel (19) and the side surface of the departure skylight (3); the sliding plate (21) is in sliding fit with the limiting rod (23); the top of the sliding plate (21) is fixedly connected with an L-shaped push plate (24).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220591444.7U CN217049069U (en) | 2022-03-17 | 2022-03-17 | Top cabin opening structure for unmanned aerial vehicle-mounted departure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202220591444.7U CN217049069U (en) | 2022-03-17 | 2022-03-17 | Top cabin opening structure for unmanned aerial vehicle-mounted departure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN217049069U true CN217049069U (en) | 2022-07-26 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202220591444.7U Active CN217049069U (en) | 2022-03-17 | 2022-03-17 | Top cabin opening structure for unmanned aerial vehicle-mounted departure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN217049069U (en) |
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2022
- 2022-03-17 CN CN202220591444.7U patent/CN217049069U/en active Active
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