High-pressure steam energy storage device for airplane

Abstract

The high-pressure steam energy storage device for the airplane comprises an energy storage tank and a pressure release valve, the pressure release valve is installed at the top end of the energy storage tank, an inspection frame is installed on the outer wall of the energy storage tank, a remote control switch is installed on the portion, on one side of the inspection frame, of the outer wall of the energy storage tank, and the remote control switch is connected with the remote control switch. A driving seat is installed on the outer wall of the energy storage tank on one side of the remote control switch, a timing switch is installed on the outer wall of the energy storage tank on one side of the driving seat, an air outlet pipe and a water supply pipe are installed on the outer wall of the energy storage tank above the driving seat, and a stepping motor is installed on the outer wall of the driving seat; a worm is installed at the output end of the stepping motor, and a rotating shaft is movably installed in the portion, on one side of the worm, of the driving base. According to the utility model, the energy storage device can be conveniently, remotely and regularly controlled to heat and store energy, water in the energy storage device can be conveniently and quickly stirred and heated, and the heating efficiency and the convenience of inspection and maintenance are improved.

Description

TECHNICAL FIELD

[0001] The utility model relates to energy storage device technical field, concretely is a kind of high-pressure steam energy storage device for airplane. BACKGROUND

[0002] The existing energy storage technology such as lithium battery is not safe and easy to catch fire, lead-acid battery has low energy density and pollutes the environment, in order to produce clean energy, so the way of high-pressure steam is used to store energy, the advantage of high-pressure steam energy storage is to store energy with water, and its energy density is greater than that of lithium battery under certain temperature and pressure, and it is completely safe and pollution-free, but the traditional high-pressure water energy storage needs manual operation, cannot remotely control the water temperature and water pressure inside the energy storage tank, it is relatively inconvenient to use, in order to improve the situation, a high-pressure steam energy storage device for airplane is provided.

[0003] As disclosed in the authorized announcement No. CN218916044U, a kind of storage device for high-pressure steam energy storage, including box, the box left end face is symmetric and fixed with two detection fixed plate, the detection fixed plate of both sides is fixedly connected with pressure detection box between the center one side end face, the box upper end face is fixed with upper end cover, the upper end cover upper end face is fixed with upper steam inlet, the box lower end face is fixed with four lower fixed frame;

[0004] Although it realizes the temperature insulation layer by the internal partition mechanism, the steam in the internal cavity and the external environment can be provided with a temperature insulation layer, and the pressure detection mechanism is provided on the left part, the steam in the internal cavity can be detected, so as to avoid the situation that the internal pressure of the internal cavity is too low, the molten salt storage rack is provided, the heat contained in the steam can be stored, so that the internal cavity can maintain a higher temperature for a period of time after the steam is discharged;

[0005] But it does not solve the problem that the existing energy storage device is not convenient for remote timing control of energy storage device heating energy storage, and the water in the energy storage device is not convenient for rapid stirring and heating, which affects the heating efficiency and the convenience of inspection and maintenance. UTILITY MODEL CONTENTS

[0006] The utility model aims at providing a kind of high-pressure steam energy storage device for airplane, to solve the problem that the energy storage device is not convenient for remote timing control of energy storage device heating energy storage in the above background technology, and the water in the energy storage device is not convenient for rapid stirring and heating, which affects the heating efficiency and the convenience of inspection and maintenance.

[0007] To achieve the above object, the utility model provides the following technical scheme: A high pressure steam energy storage device for airplane, including energy storage jar and pressure relief valve, the top of energy storage jar is installed with pressure relief valve, the outer wall of energy storage jar is installed with viewing frame, the outer wall of energy storage jar of viewing frame one side is installed with remote control switch, the outer wall of energy storage jar of remote control switch one side is installed with drive seat, the outer wall of energy storage jar of drive seat one side is installed with timing switch, the outer wall of energy storage jar above drive seat is installed with gas pipe and water supply pipe respectively, the outer wall of drive seat is installed with step motor, the output of step motor is installed with worm, the inside of drive seat of worm one side is movably installed with rotating shaft, and rotating shaft extends to the inside of energy storage jar, the surface of rotating shaft in the inside of energy storage jar is installed with two groups of heating rod, the surface of rotating shaft of worm one side is covered with worm wheel, and worm and worm wheel are interlocked, the inner wall of energy storage jar is installed with pressure sensor, the inner wall of energy storage jar below pressure sensor is installed with temperature sensor, the inner wall of energy storage jar below temperature sensor is installed with water level sensor.

[0008] Preferably, the side wall of the viewing frame on one side is provided with an adjusting frame, one end of the adjusting frame close to the viewing frame is provided with a movable shaft, and the adjusting frame is movably connected with the viewing frame through the movable shaft.

[0009] Preferably, the side wall of the viewing frame on the other side is provided with a linkage arm, one end of the linkage arm close to the viewing frame is provided with a hinged shaft, and the linkage arm is movably connected with the viewing frame through the hinged shaft.

[0010] Preferably, the linkage arm is provided with a viewing door at the center position, the side wall of the viewing door close to the linkage arm is provided with a connecting shaft, and the viewing door is movably connected with the linkage arm through the connecting shaft.

[0011] Preferably, the side wall of the adjusting frame is provided with a locking bolt, and the locking bolt is threadedly connected with the adjusting frame.

[0012] Preferably, the linkage arm can be clamped into the inside of the adjusting frame, the linkage arm is slidably connected with the adjusting frame, and the locking bolt extends to the surface of the linkage arm.

[0013] Compared with the prior art, the energy storage device not only realizes convenient remote timing control of the energy storage device heating energy storage, facilitates quick stirring and heating of the water in the energy storage device, but also improves the heating efficiency and the convenience of inspection and maintenance.

[0014] (1) the external water source is connected with the water supply pipe, the device is realized remote control through the remote control switch, water is input to the inside of the energy storage tank through the water supply pipe, when the water level reaches the water level sensor position, the water level sensor transmits the water level information to the controller, and the controller closes the water source, then the heating rod is opened, the device is realized timing heating through the timing switch, the water in the energy storage tank is heated by the heating rod, the temperature sensor and the pressure sensor capture the water temperature and pressure data in the energy storage tank respectively, when the heating reaches the required pressure or temperature value, the heating is stopped, if the pressure is too high, the pressure in the energy storage tank is released by the pressure relief valve, in order to heat the water in the energy storage tank faster, the step motor drives the worm to rotate, the worm drives the rotating shaft and the heating rod to rotate through the worm gear, the water in the energy storage tank is heated by the heating rod, so that the water in the energy storage tank is heated faster, after heating, steam is generated, the air outlet pipe is connected with the power mechanism of the airplane, the steam is transported into the power mechanism through the air outlet pipe, to provide power for the airplane to enable the airplane to fly, the energy storage device is realized convenient remote timing control heating, the water in the energy storage device is conveniently and quickly stirred and heated, and the heating efficiency is improved;

[0015] (2) when the scale in the energy storage tank needs to be cleaned or the inside of the energy storage tank needs to be inspected and maintained, the locking bolt is loosened, the linkage arm is separated from the adjusting frame, the adjusting frame is rotated, the adjusting frame rotates around the movable shaft, the adjusting frame is away from the linkage arm, then the linkage arm is rotated, the inspection door is rotated around the hinged shaft and driven by the linkage arm through the connecting shaft, to open the inspection door, then the inside of the energy storage tank can be entered through the inspection frame to inspect and maintain the parts in the inside of the energy storage tank, the convenience of inspection and maintenance is improved. BRIEF DESCRIPTION OF DRAWINGS

[0016] Figure 1 It is a three-dimensional structure schematic view of the utility model;

[0017] Figure 2 It is a three-dimensional structure schematic view of the utility model;

[0018] Figure 3 It is a side view sectional structure schematic view of the utility model;

[0019] Figure 4 It is a three-dimensional structure schematic view of the inspection frame of the utility model;

[0020] Figure 5 It is a top view sectional structure schematic view of the utility model.

[0021] In the figure: 1, energy storage tank; 2, pressure relief valve; 3, viewing frame; 4, remote control switch; 5, gas outlet pipe; 6, water supply pipe; 7, timing switch; 8, drive seat; 9, pressure sensor; 10, temperature sensor; 11, water level sensor; 12, heating rod; 13, rotating shaft; 14, stepping motor; 15, worm; 16, worm gear; 17, hinged shaft; 18, connecting shaft; 19, linkage arm; 20, locking bolt; 21, adjusting frame; 22, movable shaft; 23, viewing door. DETAILED DESCRIPTION

[0022] In order to further illustrate the technical means and effects adopted by the utility model to achieve the predetermined utility model purposes, the specific embodiments, structures, features and effects according to the utility model are described in detail as follows in combination with the drawings and preferred embodiments.

[0023] Please refer to Figures 1-5 The utility model provides an embodiment: a high pressure steam energy storage device for airplane, including energy storage tank 1 and pressure relief valve 2, the top of energy storage tank 1 is installed pressure relief valve 2, the outer wall of energy storage tank 1 is installed viewing frame 3, the outer wall of energy storage tank 1 on the one side of viewing frame 3 is installed remote control switch 4, the outer wall of energy storage tank 1 on the one side of remote control switch 4 is installed drive seat 8, the outer wall of energy storage tank 1 on the one side of drive seat 8 is installed timing switch 7, the outer wall of energy storage tank 1 above drive seat 8 is installed gas outlet pipe 5 and water supply pipe 6 respectively, the outer wall of drive seat 8 is installed stepping motor 14, the output of stepping motor 14 is installed worm 15, the inside of drive seat 8 on the one side of worm 15 is movably installed rotating shaft 13, and rotating shaft 13 extends to the inside of energy storage tank 1, the surface of rotating shaft 13 in the inside of energy storage tank 1 is installed two groups of heating rod 12, the surface of rotating shaft 13 on the one side of worm 15 is sleeved with worm gear 16, and worm 15 and worm gear 16 are mutually engaged, the inner wall of energy storage tank 1 is installed pressure sensor 9, the inner wall of energy storage tank 1 below pressure sensor 9 is installed temperature sensor 10, the inner wall of energy storage tank 1 below temperature sensor 10 is installed water level sensor 11;

[0024] The external water source is connected with the water supply pipe 6, the device is remotely controlled through the remote control switch 4, water is input into the inside of the energy storage tank 1 through the water supply pipe 6, when the water level reaches the position of the water level sensor 11, the water level information is transmitted to the controller by the water level sensor 11, and the water source is closed by the controller, then the heating rod 12 is opened, the device is heated by the timing switch 7, the water in the energy storage tank 1 is heated by the heating rod 12, the temperature and pressure data of the water in the energy storage tank 1 are captured by the temperature sensor 10 and the pressure sensor 9 respectively, when the heating reaches the required pressure or temperature value, the heating is stopped, if the pressure is too high, the pressure in the energy storage tank 1 is released by the pressure relief valve 2, in order to heat the water in the energy storage tank 1 faster, the step motor 14 is opened, the worm 15 is driven to rotate by the step motor 14, under the mutual meshing of the worm 15 and the worm gear 16, the rotating shaft 13 and the heating rod 12 are driven to rotate by the worm 15 through the worm gear 16, the water in the energy storage tank 1 is stirred and heated by the heating rod 12, so that it is heated faster, after heating, steam is generated, the air outlet pipe 5 is connected with the power mechanism of the airplane, the steam is transported into the power mechanism through the air outlet pipe 5, to provide power for the airplane to enable the airplane to fly, realizing convenient remote timing control of the energy storage device for heating energy storage, facilitating fast stirring and heating of the water in the energy storage device, and improving the heating efficiency;

[0025] An adjusting frame 21 is arranged on the side wall of one side of the viewing frame 3, the adjusting frame 21 is arranged with a movable shaft 22 close to one end of the viewing frame 3, and the adjusting frame 21 is movably connected with the viewing frame 3 through the movable shaft 22; a linkage arm 19 is arranged on the side wall of the other side of the viewing frame 3, the linkage arm 19 is arranged with a hinged shaft 17 close to one end of the viewing frame 3, and the linkage arm 19 is movably connected with the viewing frame 3 through the hinged shaft 17;

[0026] A viewing door 23 is arranged at the center position of the linkage arm 19, the viewing door 23 is arranged with a connecting shaft 18 close to the side wall of the linkage arm 19, and the viewing door 23 is movably connected with the linkage arm 19 through the connecting shaft 18; a locking bolt 20 is arranged on the side wall of the adjusting frame 21, and the locking bolt 20 is threadedly connected with the adjusting frame 21;

[0027] The linkage arm 19 can be clamped into the inside of the adjusting frame 21, the linkage arm 19 is slidably connected with the adjusting frame 21, and the locking bolt 20 extends to the surface of the linkage arm 19;

[0028] When the need to clean the scale inside the energy storage tank 1 or to inspect the inside of the energy storage tank 1, loosen the locking bolt 20, make the linkage arm 19 and the adjusting frame 21, turn the adjusting frame 21, the adjusting frame 21 rotates around the movable shaft 22, make the adjusting frame 21 away from the linkage arm 19, then turn the linkage arm 19, the linkage arm 19 drives the inspection door 23 to rotate around the hinge shaft 17 through the connecting shaft 18, to open the inspection door 23, then enter the energy storage tank 1 through the inspection frame 3 to inspect and repair the internal parts, improve the convenience of inspection and repair.

[0029] Working principle: Connect the external water source with the water supply pipe 6, control the device remotely through the remote control switch 4, input water into the inside of the energy storage tank 1 through the water supply pipe 6, when the water level reaches the water level sensor 11 position, the water level sensor 11 transmits the water level information to the controller and closes the water source by the controller, then opens the heating rod 12, controls the device by the timing switch 7, heats the water in the energy storage tank 1 by the heating rod 12, captures the water temperature and pressure data in the energy storage tank 1 by the temperature sensor 10 and the pressure sensor 9 respectively, stops heating when the required pressure or temperature value is reached, if the pressure is too high, the pressure relief valve 2 will relieve the pressure in the energy storage tank 1, in order to heat the water in the energy storage tank 1 faster, the step motor 14 drives the worm 15 to rotate, the worm 15 drives the rotating shaft 13 and the heating rod 12 to rotate through the worm gear 16, the heating rod 12 stirs the water in the energy storage tank 1 to heat it faster, after heating, the steam will be generated, the exhaust pipe 5 will be connected with the power mechanism of the airplane, the steam will be transported to the power mechanism through the exhaust pipe 5 to provide power for the airplane to enable the airplane to fly, when the need to clean the scale inside the energy storage tank 1 or to inspect the inside of the energy storage tank 1, loosen the locking bolt 20, make the linkage arm 19 and the adjusting frame 21, turn the adjusting frame 21, the adjusting frame 21 rotates around the movable shaft 22, make the adjusting frame 21 away from the linkage arm 19, then turn the linkage arm 19, the linkage arm 19 drives the inspection door 23 to rotate around the hinge shaft 17 through the connecting shaft 18, to open the inspection door 23, then enter the energy storage tank 1 through the inspection frame 3 to inspect and repair the internal parts, the above is the whole use of the high-pressure steam energy storage device for airplane.

[0030] The above merely describes preferred embodiments of the present application and is not intended to limit the present application in any form. Although the present application has been disclosed with preferred embodiments, it is not intended to limit the present application. Any person skilled in the art can make minor changes or modifications to the disclosed technical content to obtain equivalent embodiments with equivalent changes, as long as the changes or modifications do not deviate from the technical solution of the present application. Any indirect modification, equivalent change and modification of the above embodiments based on the technical essence of the present application still belong to the scope of the technical solution of the present application.

Claims

1. A high-pressure steam energy storage device for aircraft, comprising an energy storage tank (1) and a pressure relief valve (2), characterized in that: A pressure relief valve (2) is installed at the top of the energy storage tank (1). An inspection frame (3) is installed on the outer wall of the energy storage tank (1). A remote control switch (4) is installed on the outer wall of the energy storage tank (1) on one side of the inspection frame (3). A drive seat (8) is installed on the outer wall of the energy storage tank (1) on one side of the remote control switch (4). A timer switch (7) is installed on the outer wall of the energy storage tank (1) on one side of the drive seat (8). An air outlet pipe (5) and a water supply pipe (6) are respectively installed on the outer wall of the energy storage tank (1) above the drive seat (8). A stepper motor (14) is installed on the outer wall of the drive seat (8). A worm gear (15) is installed at the output end of the stepper motor (14). A rotating shaft (13) is movably installed inside the drive seat (8) on one side of the worm (15), and the rotating shaft (13) extends into the interior of the energy storage tank (1). Two sets of heating rods (12) are installed on the surface of the rotating shaft (13) inside the energy storage tank (1). A worm wheel (16) is fitted on the surface of the rotating shaft (13) on one side of the worm (15), and the worm (15) and the worm wheel (16) mesh with each other. A pressure sensor (9) is installed on the inner wall of the energy storage tank (1). A temperature sensor (10) is installed on the inner wall of the energy storage tank (1) below the pressure sensor (9). A water level sensor (11) is installed on the inner wall of the energy storage tank (1) below the temperature sensor (10).

2. The high-pressure steam energy storage device for aircraft according to claim 1, characterized in that: An adjustment frame (21) is provided on one side wall of the inspection frame (3). A movable shaft (22) is provided at one end of the adjustment frame (21) near the inspection frame (3), and the adjustment frame (21) is movably connected to the inspection frame (3) through the movable shaft (22).

3. The high-pressure steam energy storage device for aircraft according to claim 2, characterized in that: A linkage arm (19) is provided on the side wall of the other side of the inspection frame (3). A hinge shaft (17) is provided at one end of the linkage arm (19) near the inspection frame (3), and the linkage arm (19) is movably connected to the inspection frame (3) through the hinge shaft (17).

4. The high-pressure steam energy storage device for aircraft according to claim 3, characterized in that: An inspection door (23) is provided at the center of the linkage arm (19). A connecting shaft (18) is provided on the side wall of the inspection door (23) near the linkage arm (19), and the inspection door (23) is movably connected to the linkage arm (19) through the connecting shaft (18).

5. The high-pressure steam energy storage device for aircraft according to claim 2, characterized in that: The side wall of the adjustment frame (21) is provided with a locking bolt (20), and the locking bolt (20) is threadedly connected to the adjustment frame (21).

6. The high-pressure steam energy storage device for aircraft according to claim 3, characterized in that: The linkage arm (19) can be inserted into the interior of the adjustment frame (21), and the linkage arm (19) is slidably connected to the adjustment frame (21), and the locking bolt (20) extends to the surface of the linkage arm (19).

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