Aerial rocket line detection device

Abstract

The invention belongs to the technical field of aviation detection, and provides an aviation rocket line detection device which comprises a case, a rocket detection module, a hanger detection module, a connection cable and an operation panel. The case is used for accommodating the rocket detection module and the hanger detection module; the rocket detection module is used for detecting a rocket line; the hanger detection module is used for detecting a hanger line. Specifically, an onboard signal is transmitted to a single chip microcomputer, the single chip microcomputer analyzes the transmitted signal and converts the signal into an output instruction for controlling a corresponding relay, so that the relay is controlled to be closed, different relays control different indicating lamps to be turned on and turned off, and whether a line is correct or not can be detected. The device is small in size and good in portability, and can conveniently and quickly detect the correctness of rocket launching control, control circuit and hanger internal line connection on the aircraft.

Description

Technical Field

[0001] The invention belongs to the field of aviation detection technology, and specifically relates to an aviation rocket line detection device, which is suitable for aircraft rocket launch control, detection of control circuits and testing of internal lines of a pylon. Background Art

[0002] Aerial rockets, also known as "airborne rockets", are unguided weapons powered by rocket engines that are launched from a pylon suspended under the fuselage or wing of the carrier aircraft. They are widely equipped on various combat aircraft. When performing ground maintenance, checking the correctness of the rocket launch control, control circuits and internal circuit connections on the aircraft is an important part of ground inspection work.

[0003] At present, when conducting ground inspections, the aircraft is moved to the hangar and the power supply and line detection equipment in the hangar are used to perform inspections. There are problems such as long inspection cycles, the need to move the aircraft, and a large number of operators. When combat aircraft are undergoing ground inspections and maintenance in the field, the current detection methods cannot meet the needs. Summary of the invention

[0004] In order to solve the problems existing in the prior art, the present invention provides an aviation rocket line detection device, which can quickly and conveniently detect the correctness of the connection of the rocket line and the internal line of the rack under field conditions.

[0005] The technical solution provided by the present invention is:

[0006] The aerospace rocket line detection device comprises a chassis, a rocket detection module, a rack detection module, a connecting cable, and an operation panel;

[0007] The rocket detection module includes a first single-chip microcomputer, a first transformer, a first relay and a plurality of rocket line detection indicator lights; the first transformer is used to convert the onboard alternating current into direct current to supply power to the first single-chip microcomputer and the first relay;

[0008] The rack detection module includes a second single-chip microcomputer, a second transformer, a second relay and a plurality of rack line detection indicator lights; the second transformer is used to convert the onboard alternating current into direct current to supply power to the second single-chip microcomputer and the second relay;

[0009] When the detection device is connected to the onboard control circuit through the connecting cable, the first single-chip microcomputer can receive the onboard rocket line manipulation and control signal, parse the rocket line manipulation and control signal into corresponding command instructions, and output it to the first relay; the first relay controls the corresponding rocket line detection indicator light on and off according to the command instructions output by the first single-chip microcomputer, so as to judge whether the rocket control signal sent by the onboard control circuit is correct;

[0010] The second single-chip microcomputer can receive the control signal of the onboard rack line, parse the rack line control signal into corresponding command instructions, and output it to the second relay; the second relay controls the corresponding rack line detection indicator light on and off according to the command instructions output by the second single-chip microcomputer, so as to judge whether the rack signal sent by the onboard control circuit is correct;

[0011] The chassis is used to accommodate the rocket detection module and the rack detection module; the operation panel is located on the front of the chassis, and the operation panel is provided with buttons for controlling rocket line manipulation and control signal detection and buttons for controlling rack line control signal detection, a voltage display meter, a rocket\rack selection switch button, a rocket line detection indicator light, a rack line detection indicator light, a launch selection knob and a power switch; the back of the chassis has heat dissipation holes, a cable interface and a power interface.

[0012] Furthermore, the chassis is no longer than 600 mm, no wider than 350 mm, and no higher than 250 mm.

[0013] Furthermore, the rack line detection indicator light includes an indicator light indicating whether the front explosion control is normal, an indicator light indicating whether the rear explosion control is normal, an indicator light indicating whether the release of bomb I is normal, an indicator light indicating whether the release of bomb II is normal, an indicator light indicating whether the tactical delivery is normal, an indicator light indicating whether the emergency delivery is normal, and an indicator light indicating whether the coordination signal is normal.

[0014] Furthermore, the n-shot salvo selection knob is divided into 2-shot salvo, 4-shot salvo and 7-shot salvo.

[0015] Furthermore, the button for controlling the detection of the control signal of the rack line is divided into a button for controlling the detection of the control signal of the inner rack line and a button for controlling the detection of the control signal of the outer rack line.

[0016] The method for inspecting the line of an aerospace rocket using the above-mentioned detection device specifically includes:

[0017] Inboard rocket "7 rounds" continuous firing control and control circuit inspection; Inboard rocket "2 rounds" salvo firing control and control circuit inspection; Inboard rocket "4 rounds" continuous firing control and control circuit inspection;

[0018] Outer rocket "7 rounds" continuous firing control and control circuit detection; Outer rocket "2 rounds" continuous firing control and control circuit detection; Outer rocket "4 rounds" continuous firing control and control circuit detection;

[0019] Internal line detection of the inner universal rack and the internal line detection of the outer universal rack.

[0020] The specific operations are as follows:

[0021] When performing the "7-shot" continuous firing control and control line detection of the inner rocket, press the "rocket" button and the "inner rack" button on the operation panel at the same time, point the rocket\rack selection switch button to "rocket", and rotate the n-shot selection knob to "7 shots", press the "weapon launch" button on the aircraft, if the corresponding rocket line detection indicator lights on the operation panel are lit and maintained in sequence according to the set rules, the line connection is correct, otherwise the measured line has a fault; the "rocket" button is the button for controlling the rocket line control and control signal detection; the "inner rack" button is the button for controlling the inner rack line control signal detection;

[0022] When conducting the "2-shot" salvo control and control line detection of the inner rocket, press the "rocket" button and the "inner rack" button on the operation panel at the same time, point the rocket\rack selection switch button to "rocket", and rotate the n-shot selection knob to "2 shots", and press the "weapon launch" button on the aircraft multiple times according to the rules. If the corresponding rocket line detection indicator lights on the operation panel light up and remain on in sequence according to the set rules, the line connection is correct, otherwise the tested line has a fault;

[0023] When conducting the "4-round" salvo control and control line detection of the inner rocket, press the "rocket" button and the "inner rack" button on the operation panel at the same time, point the rocket\rack selection switch button to "rocket", and rotate the n-round selection knob to "4 rounds", and press the "weapon launch" button on the aircraft multiple times according to the rules. If the corresponding rocket line detection indicator lights on the operation panel light up and remain on in sequence according to the set rules, the line connection is correct, otherwise the tested line has a fault;

[0024] When performing the "7-shot" continuous firing operation of the outer rocket and the control line detection, press the "rocket" button and the "outer rack" button on the operation panel at the same time, point the rocket\rack selection switch button to "rocket", and rotate the n-shot selection knob to "7 shots", and press the "weapon launch" button on the aircraft. If the corresponding rocket line detection indicator lights on the operation panel light up and remain on in sequence according to the set rules, the line connection is correct, otherwise the measured line has a fault; the "outer rack" button is the button for controlling the outer rack line control signal detection;

[0025] When conducting the "2-shot" salvo operation of the outer rockets and the control line detection, press the "rocket" button and the "outer rack" button on the operation panel at the same time, point the rocket\rack selection switch button to "rocket", and rotate the n-shot selection knob to "2 shots", and press the "weapon launch" button on the aircraft multiple times according to the rules. If the corresponding rocket line detection indicator lights on the operation panel light up and remain on in sequence according to the set rules, the line connection is correct, otherwise the tested line has a fault;

[0026] When conducting the "4-round" salvo operation of the outer rockets and the control line detection, press the "rocket" button and the "outer rack" button on the operation panel at the same time, point the rocket\rack selection switch button to "rocket", and rotate the n-round selection knob to "4 rounds", and press the "weapon launch" button on the aircraft multiple times according to the rules. If the corresponding rocket line detection indicator lights on the operation panel light up and remain on in sequence according to the set rules, the line connection is correct, otherwise the tested line has a fault;

[0027] When checking the internal circuits of the inner universal rack, press the "Inner Rack" button on the operation panel and point the rocket\rack selection switch button to "Rack":

[0028] When the "weapon release" button on the aircraft is pressed, the "tactical release" indicator light on the operation panel lights up, and at the same time, the "bomb release I" and "bomb release II" indicators on the operation panel light up, which means the circuit is connected correctly, otherwise the measured circuit is faulty;

[0029] When the "Fuze N+T" is selected on the inner hanging point of the aircraft, and the "Weapon Release" button on the aircraft is pressed, the "Front Detonation Control", "Rear Detonation Control", "Bomb Release I", "Bomb Release II" and "Tactical Release" indicators on the operation panel are all on, which means the line connection is correct, otherwise the measured line is faulty;

[0030] When the "Emergency Release" button on the aircraft is pressed, the "Emergency Release" indicator light on the operation panel lights up, and at the same time, the "Bomb Release I", "Bomb Release II", and "Coordination Signal" indicators light up, which means the circuit connection is correct, otherwise the measured circuit has a fault;

[0031] When the bomb hook of the inner rack is released unilaterally, the "Bomb Release I", "Bomb Release II" and "Emergency Release" indicators on the operation panel are all on, which means the line connection is correct, otherwise the measured line is faulty;

[0032] When testing the internal circuits of the outer universal rack, press the "Outer Rack" button on the operation panel and point the rocket\rack selection switch button to "Rack":

[0033] When the "weapon release" button on the aircraft is pressed, the "tactical release" indicator light on the operation panel lights up, and at the same time, the "bomb release I" and "bomb release II" indicators on the operation panel light up, which means the circuit connection is correct, otherwise the measured circuit has a fault;

[0034] When the "Emergency Release" button on the aircraft is pressed, the "Emergency Release" indicator light on the operation panel lights up, and at the same time, the "Bomb Release I", "Bomb Release II", and "Coordination Signal" indicators light up, which means the circuit connection is correct, otherwise the measured circuit has a fault;

[0035] Release the bomb hook of the outer bracket on one side. If the "Bomb Release I", "Bomb Release II", "Emergency Release" and "Coordination Signal" indicators on the operation panel light up, the line connection is correct. Otherwise, the measured line is faulty.

[0036] The advantages of the present invention are as follows: the design of the present invention is simple and reasonable, and the launch control of the airborne rocket of the combat aircraft, the control circuit and the correctness of the internal line connection of the rack are effectively verified by turning on and off the indicator light, and the present invention is small in size and easy to carry under field conditions, and the correctness of the connection of the airborne rocket and the rack line can be quickly and conveniently detected, which reduces the workload of the maintenance personnel and ensures the maintenance quality of the combat aircraft. BRIEF DESCRIPTION OF THE DRAWINGS

[0037] Figure 1 : Working principle diagram of the aero-rocket line detection device of the present invention;

[0038] Figure 2 : Figure 1 The working principle diagram of the rocket detection module in the figure;

[0039] Figure 3 : Figure 1 The working principle diagram of the rack detection module in;

[0040] Figure 4 : Schematic diagram of the panel of the aviation rocket line detection device of the present invention. DETAILED DESCRIPTION

[0041] The present invention is further described in detail below in conjunction with the accompanying drawings and specific embodiments. The embodiments are exemplary and intended to be used to explain the present invention, but should not be construed as limiting the present invention.

[0042] For a certain type of aircraft, the detection indicators of airborne rockets are:

[0043] 1) The launch control and control circuits of the inner rocket are correct, including the following three situations:

[0044] ① "7 rounds" continuous firing; ② "2 rounds" volley firing; ③ "4 rounds" volley firing;

[0045] 2) The launch control and control circuits of the outer rocket are correct, including the following three situations:

[0046] ① "7 rounds" continuous firing; ② "2 rounds" volley firing; ③ "4 rounds" volley firing;

[0047] 3) The internal wiring of the inner universal bracket is correct;

[0048] 4) The internal wiring of the outer universal bracket is correct.

[0049] In order to realize the rapid and convenient detection of the correctness of the connection of the onboard rocket and the pylon circuit under field conditions, the present invention proposes an aviation rocket circuit detection device.

[0050] like Figure 1 As shown, the aviation rocket line detection device includes a chassis, a rocket detection module, a rack detection module, a connecting cable, and an operation panel;

[0051] like Figure 2 As shown, the rocket detection module includes a first single-chip microcomputer, a first transformer, a first relay and signal indicator lights 1 to 14; the first transformer is used to convert the 220V onboard AC power supply into 5V and 12V DC, wherein the 5V DC is used to power the first single-chip microcomputer, and the 12V DC is used to power the first relay; the first single-chip microcomputer is used to receive the control signal of the rocket circuit on the aircraft, parse the control signal of the rocket circuit into corresponding command instructions, and output it to the first relay; the first relay controls the on and off of the signal indicator lights 1 to 14 according to the command instructions output by the first single-chip microcomputer, so as to judge whether the rocket control signal sent by the aircraft is correct;

[0052] like Figure 3 As shown, the pylon detection module includes a second single-chip microcomputer, a second transformer, a second relay and a signal indicator light; the second transformer is used to convert the 220V on-board AC power supply into 5V and 12V DC, wherein the 5V DC is used to power the second single-chip microcomputer, and the 12V DC is used to power the second relay; the second single-chip microcomputer is used to receive the control signal of the on-board pylon line, parse the control signal of the pylon line into corresponding command instructions, and output it to the second relay; the second relay controls the on and off of the signal indicator lights 15 to 21 according to the command instructions output by the second single-chip microcomputer, so as to judge whether the signal of the pylon sent by the aircraft is correct; in this embodiment, the indicator light 15 indicates whether the front explosion control is normal, the indicator light 16 indicates whether the rear explosion control is normal, the indicator light 17 indicates whether the bomb release I is normal, the indicator light 18 indicates whether the bomb release II is normal, the indicator light 19 indicates whether the tactical delivery is normal, the indicator light 20 indicates whether the emergency delivery is normal, and the indicator light 21 indicates whether the coordination signal is normal;

[0053] The chassis is a rectangular parallelepiped, with a length of 600 mm, a width of 350 mm, and a height of 250 mm, and is used to accommodate the rocket detection module and the rack detection module; Figure 3 As shown, the operation panel is located on the front of the chassis, and is provided with a voltage display meter, a rocket or rack line detection switching button, a rocket line detection indicator light, a rack line detection indicator light, a fuse indicator light, a reset indicator light, an n-shot salvo selection knob and a power switch; the back of the chassis has heat dissipation holes, a cable interface and a power interface.

[0054] According to the requirements for field inspection of combat aircraft, the following eight inspections are required:

[0055] 1. Inspection of the inner rocket "7-shot" continuous firing control and control circuit;

[0056] 2. Inspection of the inner rocket "two-shot" salvo operation and control circuits;

[0057] 3. Inspection of the inner rocket "4-shot" salvo operation and control circuits;

[0058] 4. Inspection of the outer rocket "7-shot" continuous firing control and control circuits;

[0059] 5. Inspection of the outer rocket "two-shot" salvo operation and control circuits;

[0060] 6. Inspection of the outer rocket "4-shot" salvo operation and control circuits;

[0061] 7. Internal circuit inspection of the inner universal rack;

[0062] 8. Internal circuit inspection of the outer universal bracket.

[0063] First, the aviation rocket line detection device of the present invention is connected to the onboard control circuit through a connecting cable, and power is taken from the onboard control circuit. The onboard rocket control and control signals and the internal line signals of the pylon are transmitted to the single-chip microcomputer of the detection device of the present invention through the connecting cable. The single-chip microcomputer parses the line signals into corresponding command instructions and controls the on and off of the corresponding signal indicator lights on the operation panel, thereby judging whether the onboard rocket control and control lines and the internal lines of the pylon are connected correctly. Specifically:

[0064] When performing the "7-round" continuous firing of the inner rocket and the control line detection, press the "rocket" button and the "inner rack" button on the operation panel at the same time, rotate the rocket\rack selection switch button to point to "rocket", and rotate the n-round salvo selection knob to point to "7 rounds", and press the "weapon launch" button on the aircraft. If the rocket line detection indicator lights 1 to 7 on the operation panel light up in sequence and remain on, the line connection is correct, otherwise the tested line has a fault;

[0065] When conducting the "2-shot" salvo operation of the inner rocket and the control line test, press the "rocket" button and the "inner rack" button on the operation panel at the same time, rotate the rocket\rack selection knob to point to "rocket", and rotate the n-shot salvo selection knob to point to "2 shots". When the "weapon projection" button on the aircraft is pressed for the first time, indicator lights 1 to 2 on the operation panel light up and remain on in sequence; when the "weapon projection" button on the aircraft is pressed for the second time, indicator lights 3 to 4 on the operation panel light up and remain on in sequence; when the "weapon projection" button is pressed for the third time, indicator lights 5 to 6 on the operation panel light up and remain on in sequence, then the line connection is correct, otherwise the measured line has a fault;

[0066] When conducting the "4-round" salvo operation of the inner rocket and the control line inspection, press the "rocket" button and the "inner rack" button on the inspection device operation panel at the same time, rotate the rocket\rack selection knob to point to "rocket", and rotate the n-round salvo selection knob to point to "4 rounds". When the "weapon release" button on the aircraft is pressed for the first time, indicator lights 1 to 4 on the operation panel light up and remain on in sequence; when the "weapon release" button on the aircraft is pressed for the second time, indicator lights 5 to 7 on the operation panel light up and remain on in sequence, which means the line connection is correct, otherwise the tested line is faulty;

[0067] When performing the "7-round" burst firing of the outer rocket and the control circuit test, press the "rocket" button and the "outer rack" button on the inspection device operation panel at the same time, rotate the rocket\rack selection knob to point to "rocket", and rotate the n-round salvo selection knob to point to "7 rounds". When pressing the "weapon launch" button on the aircraft, indicator lights 8 to 14 on the operation panel light up in sequence and remain on, which means the circuit connection is correct, otherwise the tested circuit has a fault;

[0068] When conducting the "2-shot" salvo operation of the outer rockets and the control line inspection, press the "rocket" button and the "outer rack" button on the inspection device operation panel at the same time, rotate the rocket\rack selection knob to point to "rocket", and rotate the n-shot salvo selection knob to point to "2 shots". When the "weapon projection" button on the aircraft is pressed for the first time, indicator lights 8 to 9 on the operation panel light up and remain on in sequence; when the "weapon projection" button on the aircraft is pressed for the second time, indicator lights 10 to 11 on the operation panel light up and remain on in sequence; when the "weapon projection" button on the aircraft is pressed for the third time, indicator lights 12 to 13 on the operation panel light up and remain on in sequence, then the line connection is correct, otherwise the measured line has a fault;

[0069] When conducting the "4-round" salvo operation of the outer rockets and the control line inspection, press the "rocket" button and the "outer rack" button on the inspection device operation panel at the same time, rotate the rocket\rack selection knob to point to "rocket", and rotate the n-round salvo selection knob to point to "4 rounds". When the "weapon launch" button on the aircraft is pressed for the first time, indicator lights 8 to 11 on the operation panel light up and remain on in sequence; when the "weapon launch" button on the aircraft is pressed for the second time, indicator lights 12 to 14 on the operation panel light up and remain on in sequence, which means the line connection is correct, otherwise the tested line has a fault;

[0070] When checking the internal circuit of the inner universal rack, press the "Inner Rack" button on the inspection device operation panel and rotate the rocket\rack selection knob to point to "Rack":

[0071] When the "weapon release" button on the aircraft is pressed, the "tactical release" indicator light on the operation panel lights up, and at the same time, the "bomb release I" and "bomb release II" indicators on the operation panel light up, which means the circuit is connected correctly, otherwise the measured circuit is faulty;

[0072] When the "Fuze N+T" is selected on the inner hanging point of the aircraft and the "Weapon Release" button on the aircraft is pressed, the "Front Detonation Control", "Rear Detonation Control", "Bomb Release I", "Bomb Release II" and "Tactical Release" indicators on the operation panel are all on, which means the line connection is correct, otherwise the measured line is faulty;

[0073] When the "Emergency Release" button on the aircraft is pressed, the "Emergency Release" indicator light on the operation panel lights up, and at the same time, the "Bomb Release I", "Bomb Release II", and "Coordination Signal" indicators light up, which means the circuit connection is correct, otherwise the measured circuit has a fault;

[0074] When a certain type of bomb hook on the inner rack is released unilaterally, the "Bomb Release I", "Bomb Release II" and "Emergency Release" indicators on the operation panel are all on, which means the line connection is correct, otherwise the measured line is faulty.

[0075] When testing the internal circuit of the outer universal rack, press the "Outer Rack" button on the inspection device operation panel and rotate the rocket\rack selection knob to point to "Rack":

[0076] When the "weapon release" button on the aircraft is pressed, the "tactical release" indicator light on the operation panel lights up, and at the same time, the "bomb release I" and "bomb release II" indicators on the device operation panel light up, which means the circuit connection is correct, otherwise the measured circuit has a fault;

[0077] When the "Emergency Release" button on the aircraft is pressed, the "Emergency Release" indicator light on the operation panel lights up, and at the same time, the "Bomb Release I", "Bomb Release II", and "Coordination Signal" indicators light up, which means the circuit connection is correct, otherwise the measured circuit has a fault;

[0078] Release a certain type of bomb hook on the outer rack unilaterally, and the "Bomb Release I", "Bomb Release II", "Emergency Release" and "Coordination Signal" indicators on the operation panel will light up, which means the line connection is correct; otherwise, the measured line is faulty.

[0079] The above description is only a specific implementation mode of the present invention, but the protection scope of the present invention is not limited thereto. Any technician familiar with the technical field can easily think of various equivalent modifications or substitutions within the technical scope disclosed in the present invention, and these modifications or substitutions should be included in the protection scope of the present invention.

Claims

1. Aerospace rocket line detection device, including chassis, rocket detection module, rack detection module, connecting cable, and operation panel; The rocket detection module includes a first single-chip microcomputer, a first transformer, a first relay and a plurality of rocket line detection indicator lights; the first transformer is used to convert the onboard alternating current into direct current to supply power to the first single-chip microcomputer and the first relay; The rack detection module includes a second single-chip microcomputer, a second transformer, a second relay and a plurality of rack line detection indicator lights; the second transformer is used to convert the onboard alternating current into direct current to supply power to the second single-chip microcomputer and the second relay; When the detection device is connected to the onboard control circuit through the connecting cable, the first single-chip microcomputer can receive the onboard rocket line manipulation and control signal, parse the rocket line manipulation and control signal into corresponding command instructions, and output it to the first relay; the first relay controls the corresponding rocket line detection indicator light on and off according to the command instructions output by the first single-chip microcomputer, so as to judge whether the rocket control signal sent by the onboard control circuit is correct; The second single-chip microcomputer can receive the control signal of the onboard rack line, parse the rack line control signal into corresponding command instructions, and output it to the second relay; the second relay controls the corresponding rack line detection indicator light on and off according to the command instructions output by the second single-chip microcomputer, so as to judge whether the rack signal sent by the onboard control circuit is correct; The chassis is used to accommodate the rocket detection module and the rack detection module; the operation panel is located on the front of the chassis, and the operation panel is provided with buttons for controlling rocket line manipulation and control signal detection and buttons for controlling rack line control signal detection, a voltage display meter, a rocket\rack selection switch button, a rocket line detection indicator light, a rack line detection indicator light, a launch selection knob and a power switch; the back of the chassis has heat dissipation holes, a cable interface and a power interface.

2. The aerospace rocket line detection device according to claim 1, characterized in that: The chassis length shall not exceed 600mm, the width shall not exceed 350mm, and the height shall not exceed 250mm.

3. The aerospace rocket line detection device according to claim 1, characterized in that: The rack line detection indicator lights include an indicator light indicating whether the front explosion control is normal, an indicator light indicating whether the rear explosion control is normal, an indicator light indicating whether the bomb release I is normal, an indicator light indicating whether the bomb release II is normal, an indicator light indicating whether the tactical delivery is normal, an indicator light indicating whether the emergency delivery is normal, and an indicator light indicating whether the coordination signal is normal.

4. The aerospace rocket line detection device according to claim 1, characterized in that: The n-shot salvo selection knob is divided into 2-shot salvo, 4-shot salvo and 7-shot salvo.

5. The aerospace rocket line detection device according to claim 4, characterized in that: The button for controlling the detection of the control signal of the rack line is divided into a button for controlling the detection of the control signal of the inner rack line and a button for controlling the detection of the control signal of the outer rack line.

6. A method for inspection using the detection device according to claim 5, characterized in that: include: Inboard rocket "7 rounds" continuous firing control and control circuit inspection; Inboard rocket "2 rounds" salvo firing control and control circuit inspection; Inboard rocket "4 rounds" continuous firing control and control circuit inspection; Outer rocket "7 rounds" continuous firing control and control circuit inspection; Outer rocket "2 rounds" continuous firing control and control circuit inspection; Outer rocket "4 rounds" continuous firing control and control circuit inspection; Internal line detection of the inner universal rack and the internal line detection of the outer universal rack.

7. The method according to claim 6, characterized in that: When performing the "7-shot" continuous firing control of the inner rocket and the control line detection, press the "rocket" button and the "inner rack" button on the operation panel at the same time, point the rocket\rack selection switch button to "rocket", and rotate the n-shot selection knob to "7 shots", press the "weapon launch" button on the aircraft, if the corresponding rocket line detection indicator lights on the operation panel are lit and maintained in sequence according to the set rules, the line connection is correct, otherwise the measured line has a fault; the "rocket" button is the button for controlling the rocket line control and control signal detection; the "inner rack" button is the button for controlling the inner rack line control signal detection; When conducting the "2-shot" salvo operation of the inner rocket and the control line detection, press the "rocket" button and the "inner rack" button on the operation panel at the same time, point the rocket\rack selection switch button to "rocket", and rotate the n-shot selection knob to "2 shots", and press the "weapon launch" button on the aircraft multiple times according to the rules. If the corresponding rocket line detection indicator lights on the operation panel light up and remain on in sequence according to the set rules, the line connection is correct, otherwise the tested line has a fault; When conducting the "4-round" salvo control of the inner rocket and the control line detection, press the "rocket" button and the "inner rack" button on the operation panel at the same time, point the rocket\rack selection switch button to "rocket", and rotate the n-round selection knob to "4 rounds", and press the "weapon launch" button on the aircraft multiple times according to the rules. If the corresponding rocket line detection indicator lights on the operation panel light up and remain on in sequence according to the set rules, the line connection is correct, otherwise the tested line has a fault; When performing the "7-round" continuous firing operation of the outer rocket and the control line detection, press the "rocket" button and the "outer rack" button on the operation panel at the same time, point the rocket\rack selection switch button to "rocket", and rotate the n-round selection knob to "7 rounds", and press the "weapon launch" button on the aircraft. If the corresponding rocket line detection indicator lights on the operation panel light up and remain on in sequence according to the set rules, the line connection is correct, otherwise the measured line has a fault; the "outer rack" button is the button for controlling the outer rack line control signal detection; When conducting the "2-round" salvo operation of the outer rockets and the control line detection, press the "rocket" button and the "outer rack" button on the operation panel at the same time, point the rocket\rack selection switch button to "rocket", and rotate the n-round selection knob to "2 rounds", and press the "weapon launch" button on the aircraft multiple times according to the rules. If the corresponding rocket line detection indicator lights on the operation panel light up and remain on in sequence according to the set rules, the line connection is correct, otherwise the tested line has a fault; When conducting the "4-round" salvo operation of the outer rockets and the control line detection, press the "rocket" button and the "outer rack" button on the operation panel at the same time, point the rocket\rack selection switch button to "rocket", and rotate the n-round selection knob to "4 rounds", and press the "weapon launch" button on the aircraft multiple times according to the rules. If the corresponding rocket line detection indicator lights on the operation panel light up and remain on in sequence according to the set rules, the line connection is correct, otherwise the tested line has a fault; When checking the internal circuits of the inner universal rack, press the "Inner Rack" button on the operation panel and point the rocket\rack selection switch button to "Rack": When the "weapon release" button on the aircraft is pressed, the "tactical release" indicator light on the operation panel lights up, and at the same time, the "bomb release I" and "bomb release II" indicators on the operation panel light up, which means the circuit connection is correct, otherwise the measured circuit has a fault; When the "Fuze N+T" is selected for the inner hanging point on the aircraft, and the "Weapon Release" button on the aircraft is pressed, the "Front Detonation Control", "Rear Detonation Control", "Bomb Release I", "Bomb Release II" and "Tactical Release" indicators on the operation panel are all on, which means the line connection is correct, otherwise the measured line is faulty; When the "Emergency Release" button on the aircraft is pressed, the "Emergency Release" indicator light on the operation panel lights up, and at the same time, the "Bomb Release I", "Bomb Release II", and "Coordination Signal" indicators light up, which means the circuit connection is correct, otherwise the measured circuit has a fault; When the bomb hook of the inner rack is released unilaterally, the "Bomb Release I", "Bomb Release II" and "Emergency Release" indicators on the operation panel are all on, which means the line connection is correct, otherwise the measured line is faulty; When testing the internal circuits of the outer universal rack, press the "Outer Rack" button on the operation panel and point the rocket\rack selection switch button to "Rack": When the "weapon release" button on the aircraft is pressed, the "tactical release" indicator light on the operation panel lights up, and at the same time, the "bomb release I" and "bomb release II" indicators on the operation panel light up, which means the circuit connection is correct, otherwise the measured circuit has a fault; When the "Emergency Release" button on the aircraft is pressed, the "Emergency Release" indicator light on the operation panel lights up, and at the same time, the "Bomb Release I", "Bomb Release II", and "Coordination Signal" indicators light up, which means the circuit connection is correct, otherwise the measured circuit has a fault; Release the bomb hook of the outer rack unilaterally, and the "Bomb Release I", "Bomb Release II", "Emergency Release" and "Coordination Signal" indicators on the operation panel light up, which means the line connection is correct, otherwise the measured line is faulty.

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