Gas turbine combustor inlet control

Abstract

The utility model discloses a kind of gas turbine combustor air intake control device, belong to air intake control technical field, comprising: outer tube, the inner chamber of outer tube is equipped with fan, the right side of outer tube is fixedly connected with combustion bin, the upper end of combustion bin is equipped with air intake regulating mechanism;Discharge pipe, the right side of combustion bin is inserted with discharge pipe, the inner chamber right side of combustion bin is equipped with exhaust regulating mechanism, the right side upper end of combustion bin is equipped with controller, by being equipped with air intake regulating mechanism, it is convenient to carry out air intake adjustment to combustion bin, ensure to carry out air intake adjustment according to this device requirement, maintain optimum air-fuel ratio, by exhaust regulating mechanism, by motor driving adjustment plate on rotating shaft, it is convenient to drive adjustment plate to rotate, it is convenient to control turbine outlet pressure, reduce turbine back pressure loss, to improve the thermal efficiency of this device.

Description

Technical Field

[0001] This utility model relates to the field of air intake control technology, and in particular to an air intake control device for a gas turbine burner. Background Technology

[0002] The intake control device of a gas turbine combustor is a key component to ensure efficient and stable combustion, and its design directly affects combustion efficiency, emission performance and operational safety.

[0003] Gas turbine burners need to control the intake air volume based on the internal temperature of the combustion chamber to maintain the optimal air-fuel ratio. However, existing gas turbine burners have difficulty effectively regulating the intake and exhaust air, which affects the combustion performance of the gas turbine burner. Therefore, it is necessary to provide a new gas turbine burner intake control device to solve the above-mentioned technical problems. Utility Model Content

[0004] Purpose of the invention: The purpose of this utility model is to provide a gas turbine burner intake control device to solve the problem that existing gas turbine burners are difficult to effectively regulate intake and exhaust, thus affecting the combustion effect of the gas turbine burner.

[0005] Technical solution: A gas turbine burner intake control device, comprising: an outer cylinder, a fan installed in the inner cavity of the outer cylinder, a combustion chamber fixedly connected to the right side of the outer cylinder, and an intake regulating mechanism installed at the upper end of the combustion chamber;

[0006] An exhaust pipe is inserted into the right side of the combustion chamber. An exhaust regulating mechanism is installed on the right side of the inner cavity of the combustion chamber. A controller is installed at the upper right end of the combustion chamber. By setting an intake regulating mechanism, it is convenient to regulate the intake of the combustion chamber to ensure that the intake is regulated according to the needs of the device and to maintain the optimal air-fuel ratio. By setting an exhaust regulating mechanism, it is convenient to control the turbine outlet pressure, reduce turbine back pressure loss, and thus improve the thermal efficiency of the device.

[0007] As a further description of the above technical solution: the intake adjustment mechanism includes a linear motor installed at the upper end of the combustion chamber. The power output end of the linear motor is connected to a connecting rod, and the other end of the connecting rod is fixedly connected to a first bevel gear. By providing a linear motor, it is convenient to drive the first bevel gear on the connecting rod to rotate.

[0008] As a further description of the above technical solution: a rotating rod is rotatably installed on the upper left side of the combustion chamber, a second bevel gear is fixedly connected to the upper end of the rotating rod, and an adjusting disc is fixedly connected to the bottom of the rotating rod. By setting the second bevel gear and the adjusting disc, the first bevel gear can rotate while driving the adjusting disc to rotate and adjust.

[0009] As a further description of the above technical solution: the first bevel gear meshes with the second bevel gear, so that the first rotating gear can drive the second bevel gear to rotate synchronously while the first rotating gear rotates.

[0010] As a further description of the above technical solution: the exhaust regulating mechanism includes fixed blocks installed at the upper and lower ends of the right side of the combustion chamber cavity. A rotating shaft is hinged to the left side of the lower fixed block. An adjusting plate is fixedly connected to the upper end of the rotating shaft. A motor is installed at the rear end of the rotating shaft. The power output end of the motor is connected to the rotating shaft, and the motor is installed on the combustion chamber. By setting the fixed blocks, it is easy to close the upper and lower ends of the combustion chamber cavity and to facilitate the installation of this device. By setting the rotating shaft and adjusting plate, it is easy to adjust according to the needs of this device and to facilitate the control of the exhaust of this device.

[0011] As a further description of the above technical solution: a locking block is fixedly connected to the upper end of the adjusting plate, and the locking block has a locking groove adapted to the locking block. The adjusting plate and the locking block form a locking connection mechanism. By forming a locking connection mechanism between the adjusting plate and the locking block, it is easy to adjust the adjusting plate to a suitable position for positioning, avoiding excessive angle and affecting the exhaust adjustment effect.

[0012] As a further description of the above technical solution: temperature sensors are installed at both ends of the combustion chamber to facilitate uniform sensing of the temperature inside the combustion chamber.

[0013] As a further description of the above technical solution: the temperature sensor is electrically connected to the controller, which facilitates the controller to control the electrical components of the device based on the sensing information.

[0014] Beneficial effects: 1. By setting up an intake adjustment mechanism, the bevel gear on the connecting rod is driven by a linear motor to rotate, which in turn rotates the adjustment plate on the rotating rod, making it easy to adjust the intake of the combustion chamber and ensuring that the intake adjustment is carried out according to the needs of this device to maintain the optimal air-fuel ratio;

[0015] 2. By setting up an exhaust regulating mechanism, the regulating plate on the rotating shaft is driven by a motor, which facilitates the rotation of the regulating plate, making it easier to control the turbine outlet pressure, reduce turbine back pressure loss, and thus improve the thermal efficiency of this device. Attached Figure Description

[0016] Figure 1 This is a schematic diagram of the overall structure of a gas turbine burner intake control device proposed in this utility model;

[0017] Figure 2 This is a schematic diagram of the structure of this utility model.

[0018] Figure 3This is a schematic diagram of the intake adjustment mechanism of this utility model;

[0019] Figure 4 This is a schematic diagram of the exhaust regulating mechanism of this utility model.

[0020] Legend: 1. Outer cylinder; 2. Fan; 3. Combustion chamber; 4. Intake regulating mechanism; 401. Linear motor; 402. Connecting rod; 403. First bevel gear; 404. Second bevel gear; 405. Rotating rod; 406. Adjusting disc; 5. Exhaust pipe; 6. Exhaust regulating mechanism; 601. Fixing block; 602. Rotating shaft; 603. Adjusting plate; 604. Motor; 7. Temperature sensor; 8. Controller. Detailed Implementation

[0021] To make the technical solution of the present invention clearer, the present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments.

[0022] Example 1

[0023] refer to Figure 1 and Figure 2 This utility model discloses a gas turbine burner intake control device, which can solve the problem that existing gas turbine burners are difficult to effectively regulate intake and exhaust, thus affecting the combustion effect of the gas turbine burner. It includes an outer cylinder 1, a fan 2 installed in the inner cavity of the outer cylinder 1, a combustion chamber 3 fixedly connected to the right side of the outer cylinder 1, and an intake regulating mechanism 4 installed at the upper end of the combustion chamber 3.

[0024] An exhaust pipe 5 is inserted into the right side of the combustion chamber 3. An exhaust regulating mechanism 6 is installed on the right side of the inner cavity of the combustion chamber 3. A controller 8 is installed on the upper right side of the combustion chamber 3.

[0025] Working principle: The outer cylinder 1 and the fan 2 facilitate the intake of air into the combustion chamber 3. The intake regulating mechanism 4 facilitates the intake regulation of the combustion chamber 3 to ensure that the intake regulation is carried out according to the needs of this device and to maintain the optimal air-fuel ratio. The exhaust regulating mechanism 6 facilitates the control of the turbine outlet pressure, reduces turbine back pressure loss, and thus improves the thermal efficiency of this device. The controller 8 facilitates the switching of the electrical components of this device.

[0026] Example 2

[0027] Reference Figure 3 and Figure 4This embodiment solves the problem that existing gas turbine burners are difficult to effectively regulate intake and exhaust, thus affecting the combustion effect of the gas turbine burner. The gas turbine burner intake control device further includes an intake adjustment mechanism 4 comprising a linear motor 401 mounted on the upper end of the combustion chamber 3. A connecting rod 402 is connected to the power output end of the linear motor 401, and a first bevel gear 403 is fixedly connected to the other end of the connecting rod 402. A rotating rod 405 is rotatably mounted on the upper left side of the combustion chamber 3. A second bevel gear 404 is fixedly connected to the upper end of the rotating rod 405, and an adjustment disc 406 is fixedly connected to the bottom of the rotating rod 405. The first bevel gear 403 and the second bevel gear 404... 4. The exhaust regulating mechanism 6 includes fixed blocks 601 installed at the upper and lower ends of the right side of the combustion chamber 3. A rotating shaft 602 is hinged to the left side of the lower fixed block 601. An adjusting plate 603 is fixedly connected to the upper end of the rotating shaft 602. A motor 604 is installed at the rear end of the rotating shaft 602. The power output end of the motor 604 is connected to the rotating shaft 602, and the motor 604 is installed on the combustion chamber 3. A locking block is fixedly connected to the upper end of the adjusting plate 603. The fixed block 601 has a locking groove that matches the locking block. The adjusting plate 603 and the fixed block 601 form a locking connection mechanism. Temperature sensors 7 are installed at the front and rear ends of the combustion chamber 3. The temperature sensors 7 are electrically connected to the controller 8.

[0028] Working principle: When this device is in use, the temperature sensor 7 monitors the temperature inside the combustion chamber 3. When the temperature inside the combustion chamber 3 is too high, the linear motor 401 drives the bevel gear on the connecting rod 402 to rotate, causing the adjusting plate 406 on the rotating rod 405 to rotate. This facilitates the intake adjustment of the combustion chamber 3, ensuring that the intake adjustment is performed according to the needs of this device and maintaining the optimal air-fuel ratio. While the intake adjustment mechanism 4 is adjusting, the motor 604 drives the adjusting plate 603 on the rotating shaft 602 to rotate, which facilitates the control of the turbine outlet pressure, reduces turbine back pressure loss, thereby improving the thermal efficiency of this device and ensuring effective adjustment of the intake and exhaust of this device.

[0029] The embodiments described above are merely illustrative of several implementations of the present invention, and while the descriptions are specific and detailed, they should not be construed as limiting the scope of the present invention. It should be noted that those skilled in the art can make various modifications and improvements without departing from the concept of the present invention, and these modifications and improvements all fall within the scope of protection of the present invention. Therefore, the scope of protection of this patent should be determined by the appended claims.

Claims

1. A gas turbine combustor inlet control device, characterized in that, include: The outer cylinder (1) has a fan (2) installed in its inner cavity. The combustion chamber (3) is fixedly connected to the right side of the outer cylinder (1). An air intake regulating mechanism (4) is installed at the upper end of the combustion chamber (3). An exhaust pipe (5) is inserted into the right side of the combustion chamber (3). An exhaust regulating mechanism (6) is installed on the right side of the inner cavity of the combustion chamber (3). A controller (8) is installed on the upper right side of the combustion chamber (3). The intake adjustment mechanism (4) includes a linear motor (401) installed at the upper end of the combustion chamber (3). The power output end of the linear motor (401) is connected to a connecting rod (402), and the other end of the connecting rod (402) is fixedly connected to a first bevel gear (403). The exhaust regulating mechanism (6) includes a fixed block (601) installed at the upper and lower ends of the right side of the combustion chamber (3). A rotating shaft (602) is hinged to the left side of the lower fixed block (601). An adjusting plate (603) is fixedly connected to the upper end of the rotating shaft (602). A motor (604) is installed at the rear end of the rotating shaft (602). The power output end of the motor (604) is connected to the rotating shaft (602), and the motor (604) is installed on the combustion chamber (3).

2. The gas turbine combustor inlet control device according to claim 1, characterized in that, A rotating rod (405) is rotatably mounted on the upper left side of the combustion chamber (3). A second bevel gear (404) is fixedly connected to the upper end of the rotating rod (405), and an adjusting disc (406) is fixedly connected to the bottom of the rotating rod (405).

3. The gas turbine combustor inlet control device according to claim 1, characterized in that, The first bevel gear (403) meshes with the second bevel gear (404).

4. The gas turbine combustor inlet control device according to claim 1, characterized in that, The upper end of the adjusting plate (603) is fixedly connected to a locking block, and the fixing block (601) has a locking groove adapted to the locking block. The adjusting plate (603) and the fixing block (601) form a locking connection mechanism.

5. The gas turbine combustor inlet control device according to claim 1, characterized in that, Temperature sensors (7) are installed at both ends of the inner cavity of the combustion chamber (3).

6. The gas turbine combustor inlet control device according to claim 5, characterized in that, The temperature sensor (7) is electrically connected to the controller (8).

Images