POSITIVE PRESSURIZATION SYSTEM IN LAUNCH VEHICLES

Abstract

The invention relates to a system to prevent the dangerous gases, such as pus, produced in missile launch vehicles in military sites from filling the vehicle cabin (10).

Description

1 Specifications POSITIVE PRESSURIZATION SYSTEM IN LAUNCH VEHICLES Technical Area 5 The invention relates to missile launch vehicles in military applications. The invention is particularly useful for removing hazardous materials such as smoke that are generated in missile launchers in military settings. The invention relates to a system developed to prevent gases from filling the cabin. In military fields, during the missile launch phase of missile launch vehicles, 10 atoms are emitted from the missile. Dangerous gases that should not be inhaled, such as pus, etc., are released during missile launch and subsequently, to protect the user by preventing them from entering the vehicle. It is related to the system. State of the Art Today, in military settings, during the missile launch phase of missile launch vehicles, Dangerous gases, such as purge emitted from the missile, are released into the environment and should not be inhaled. When current practices are examined, the main differences are; cost-effectiveness and less It consists of configuration units. There are 20 chemical gases in existing military sites. systems with CBRN filters, which are much more expensive for protection. CBRN filters are used for short-term purposes, but certain... It is essential to replace them during their usage periods. Again, document number CN207955444, titled "Drilling rocket launched a protected transport vehicle", 25 The invention is a protected drilling rig belonging to the field of vehicle-mounted drilling rig launch technology. It provides a rocket launch transport vehicle and this protected drilling rocket launch transport vehicle, car body, protector, director's guard, general front joint It includes the platform and adjustment device; the car body includes the driver's cab and frame. and the general front joint platform is mounted on the frame, and director protection 30 the housing and the general front joint platform respectively, the director protection housing and The general thoracic joint platform is connected to the swing joint, adjustment device, and protective device. The frame adjusts its position close to the driver's cab, protecting the driver's cab. It is located and is between the director's protective housing in the horizontal position. Above 2 The aforementioned protective cover is located between the driver's cab and the director's guard housing. The position adjustment and protection can absorb the partial impact force of the rocket, ensuring safety. It provides protection, ensuring the personal safety of the guard going to the driver's cab. Again, invention no. CN207922952, entitled “Rocket Launch Transport Vehicle”, refers to a vehicle-mounted 5 a drilling rocket launch vehicle belonging to the field of drilling rocket launch technology It provides and this drilling rocket launch transport vehicle, car body, director protection housing, adjustment device, general butt joint platform, damping device and It includes a protective cover, passes through the general front joint platform damping device, and chassis. It is mounted on top, and the damping device can be in elastic support mode or rigid support mode 10 You can configure the mode and the director protection housing and general front joint platform. respectively, director protection housing and general front joint platform oscillation It is attached to the joint, the adjustment device, and the guard, located in the frame near the driver's cab. The position settings are adjusted by the protective driver's cab and the horizontal position director. It is among the protective casings. Using a damping device can satisfy the rocket 15 and to protect the driver's cab in case of a user's request for transport or launch uses the protective device, revealing the potential safety hazard when the boiler is operated. prevents its departure or other factors that lead to the rocket being brought to its cruise partner, It protects the safety of your fellow passenger. Purpose of the Invention The invention aims to eliminate the disadvantages inherent in the prior art. One purpose is to protect personnel from hazardous gases such as purges produced in missile launch vehicles. The most cost-effective way to prevent water from entering the driver's cabin, which is the living space. Another aim of the invention is to have fewer configuration items. Another objective of the invention is to enable the user to complete the operation safely. Another advantage of the invention is that it requires less space. 30 Explanation of the Figures Figure 1 shows the application view of the system that is the subject of the invention. 3 Explanation of Reference Numbers Reference Number Reference Name 1 Compressed Air Cylinders 2 Pressure Gauges 3 Buttons 4 Air lines Check valves 6 Solenoid Valves 7-Manometer Regulator 8 Relays 9 Vehicle Compressors Vehicle cabin Detailed Description of the Invention The invention eliminates dangerous, rust-like fumes that form in missile launch vehicles in military settings. It is a system to prevent gases from filling the vehicle cabin (10). Figure 1 shows an application view of the system that is the subject of the invention. In the figure... As can be seen, compressed air cylinders (1) and which enable the storage of clean air. The compressed air cylinders (1) contain a manometer (2) which measures the air pressure. 10 The invention is for controlling the filling, emptying and on / off functions of the system. buttons (3) are used. The air line between the compressed air cylinders (1) shown in Figure 1 and the driver's cab air hoses (4) that provide air movement in one direction, check valves (5) that provide air movement in one direction, 15 directing air into the driver's cab (10), filling the compressed air cylinders solenoid valves (6) are used to control. The air that will come from the compressed air cylinders (1) to the driver's cab (10) Regulator with pressure gauge (7) to adjust the flow rate, to control the energy coming into the system 20 The relay used (8), the vehicle compressor used to produce air (9) are shown in Figure 1. It is seen. 4 The system described in the invention is designed to remove hazardous gases such as smoke produced in missile launch vehicles. to prevent the driver's cab (10), which is the living area of ​​the personnel, from filling up and It is designed to allow the user to complete the operation safely. In the application of the system described in the invention; Before operation, the compressed air cylinders (1) must be filled with clean air. System It is opened with the on / off button (3), and the compressed air cylinders (1) are filled with the tank filling button (3). It is filled with clean air. Scenario: 1 If the user is inside the vehicle driver's cab (10) during the missile launch operation; Press the positive pressurization button (3) at the start of the launch The solenoid valve (6) is opened and compressed air is drawn into the driver's cab (10). Clean air begins to fill the tubes (1). 15 By filling the driver's cab (10) with clean air from the compressed air cylinders (1). A pressure difference is created between the driver's cab (10) and the outside environment. The driver's cab (10) interior The pressure becomes greater than that of the external environment (atmospheric pressure). This allows the missile to... dangerous gases released enter the vehicle driver's cab (10) during firing 20 This is being prevented. Scenario: 2 During the missile launch operation, the user remotely controls the vehicle driver cabin (10) from outside. If it will provide control; 25 Once the launch is initiated, an electrical signal is received from the launch unit. This electrical signal... The signal causes the solenoid valve (6) to open and compressed air to enter the driver's cab (10). Clean air begins to fill the tubes (1). By filling the driver's cab (10) with clean air from the compressed air cylinders (1). A pressure difference is created between the driver's cab (10) and the outside environment. The driver's cab interior The pressure becomes greater than that of the external environment (atmospheric pressure). This allows the missile to... The dangerous gases released are unable to enter the vehicle's driver's cabin during the firing process, and The vehicle does not contain dangerous gases when the user gets inside.

Claims

6 REQUESTS 1. The invention relates to the purging of rust-like substances that form in missile launch vehicles in military settings. To prevent dangerous gases from filling the vehicle cabin (10), a system containing a vehicle compressor (9) used to produce air 5 being; compressed air cylinders that enable the storage of clean air (1), measuring the air pressure in the mentioned compressed air cylinders (1) manometer (2), 10 to control the system's filling, emptying, and on / off functions buttons used (3), air line between compressed air cylinders (1) and driver cab (10) providing overhead line (4), Check valves that allow the air to move in one direction (5), directing air to the driver's cab (10), compressed air cylinders 15 solenoid valves (6) that control the filling Compressed air cylinders (1) will come to the driver's cab (10) regulator with pressure gauge that adjusts the air flow (7), relay (8) used to control the energy coming into the system, It is characterized by its inclusion. 20 2. The invention is a system described in claim 1, the characteristic of which is: The system is turned on with the on / off button (3), tank filling button (3) and compressed air cylinders (1) with clean air ensuring it is filled, 25 If the user is inside the vehicle driver's cab (10) during the missile launch operation, with the initiation of launch, press the positive pressurization button (3) opening the solenoid valve (6) by pressing it, During the missile launch operation, the user remotely controls the vehicle driver's cab (10) outside the vehicle driver's cab. If command and control will be provided, the launch will begin and the launch will be completed in 30 seconds. The solenoid valve (6) is opened upon receiving an electrical signal from the unit, By opening the solenoid valve (6), compressed air enters the driver's cab (10). filling of the tubes (1) with clean air, 7 a pressure difference is created between the driver's cab (10) and the outside environment Dangerous gases from the missile during the firing enter the vehicle driver's cabin (10) preventing entry It includes the steps of the process.

3. It is a system that conforms to claim 2, and its feature is that the solenoid valve (6) is opened. Clean air cylinders (1) inside the driver's cab (10) After the air fills; the internal pressure of the driver's cab (10) is different from the external environment. (Atmospheric pressure) is greater.

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