Plug-in type high-temperature-resistant ablation prefabricated part for flow guide groove of launching station and construction method of fire-resistant protective layer

A construction method and technology of diversion grooves, which are applied to rocket launchers, manufacturing tools, ceramic molding machines, etc., can solve problems such as poor high-temperature ablation resistance, damaged structures, and structural damage, and achieve excellent high-temperature ablation resistance , Strong environmental adaptability and increased service life

Pending Publication Date: 2019-01-08
中国人民解放军63926部队
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Poor maintainability: the diversion channel of the launching station adopts a cast-in-place integrated structure with internal reinforcement mesh, and the damage speed of each part varies greatly during use. The damage speed is the highest, and the advection section is basically not damaged due to the structural protective design, so it is necessary to repair the severely damaged local parts after several uses
Although the current overall cast-in-place structure has good integrity, it cannot be partially dismantled and repaired
[0005] Poor environmental adaptability: The construction environment of refractory castables belongs to the open air environment, and the construction performance and technical indicators of castables are greatly affected by environmental factors such as temperature and humidity. Although the construction performance of castables can be corrected by adding additive technology, but However, it is difficult to achieve the technical indicators in the standard testing environment, so that its performance cannot be guaranteed to the maximum extent.
[0006] Poor high-temperature ablation resistance: Since cast-in-place materials cannot be baked, the amount of cement added is usually fully increased in order to obtain high strength, and too high an amount of cement added will significantly reduce the refractoriness of the material, resulting in deterioration of its high-temperature performance
Compared with the baked refractory castables, the unbaked refractory castables have lower bonding strength and poorer erosion resistance
In addition, when the direct-flow section is impacted by high-temperature airflow, the crystal water in the cast-in-place refractory concrete will gasify rapidly, which will easily cause the material to burst and damage the structure. The structure is abnormally damaged and the service life does not meet the requirements.

Method used

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  • Plug-in type high-temperature-resistant ablation prefabricated part for flow guide groove of launching station and construction method of fire-resistant protective layer
  • Plug-in type high-temperature-resistant ablation prefabricated part for flow guide groove of launching station and construction method of fire-resistant protective layer
  • Plug-in type high-temperature-resistant ablation prefabricated part for flow guide groove of launching station and construction method of fire-resistant protective layer

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0031] Such as Figure 1~5 As shown, a ready-to-install high-temperature ablation-resistant prefabricated part for the diversion tank of the launching station, the prefabricated part includes a high-temperature ablation-resistant main body 1 made of refractory castable, and the high-temperature ablation-resistant main body is provided with a vacancy Structure 2 and upper and lower layers of reinforcement mesh 3; the reinforcement mesh 3 is composed of criss-cross reinforcement rods embedded in the refractory castable and extending beyond the refractory castable; the vacancy structure 2 is located in the upper and lower layers of reinforcement Between the nets 3, the vacancy structure 2 is composed of regular grooves 4 formed by vacancies inside the refractory castable. The vacancy structure 2 includes upper and lower layers of grooves 4, the cross section of the groove 4 is trapezoidal or triangular, and the edge of the cross section of the vacancy structure 2 is a continuous ...

Embodiment 2

[0034] This embodiment is the same as Embodiment 1 except that the vacancy structure is changed.

[0035] Such as Figure 6~8 As shown, the cross section of the groove 4 is rectangular, and a T-shaped anchoring structure is arranged between the upper and lower layers of grooves.

Embodiment 3

[0037] A construction method for fire-resistant protective layer of a diversion channel at a launch station, in which the prefabricated part described in embodiment 1 or embodiment 2 is arranged at a certain position in the diversion channel, and the refractory castable around the prefabricated part is cast in place, and the reinforcement mesh of the prefabricated part 3 is docked with the steel bars of the surrounding diversion channel matrix, and the void structure 2 in the prefabricated part is riveted with the cast-in-place refractory castable to complete the structural integration of the diversion channel.

[0038] The prefabricated parts are prefabricated by pouring in the factory. The specific preparation method is: 1) Make the mold according to the drawing, 2) Place the steel mesh in the mold, and pre-embed the riveting structure corresponding to the required vacant structure shape, 3) According to the Technical solution Prepare refractory castables, 4) carry out pourin...

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Abstract

The invention discloses a plug-in type high-temperature-resistant ablation prefabricated part for a flow guide groove of a launching station and a construction method of a fire-resistant protective layer. The prefabricated part comprises a high-temperature-resistant ablation main body (1) prepared from a refractory castable, a vacancy structure (2) and an upper-and-lower two layer steel bar net (3) is arranged on the high-temperature-resistant ablation main body (1); the steel bar net (3) is composed of reinforced bars which are inlaid in the refractory castable and extend out of the refractory castable and are in a criss-cross mode; and the vacancy structure (2) is located between the upper-and-lower two layer steel bar net (3), and is composed of a groove (4) formed by the vacancy insidethe refractory castable. The prefabricated part is arranged at a certain part in the flow guide groove, the fire-resistant protective layer with an integrated structure is finished through the cast-in-place refractory castable at the periphery of the prefabricated part; and the prefabricated part and the method have the advantages that the prefabricated part used in the construction of the flow guide groove is strong in maintainability, high in environmental adaptability, and long in service life.

Description

technical field [0001] The invention belongs to the technical field of civil engineering, and in particular relates to the construction technology of a diversion channel for a rocket launch station, in particular to a construction method for a ready-to-install high-temperature ablation-resistant prefabricated part and a fire-resistant protective layer for a guide channel for a launch station. technical background [0002] The main function of the diversion groove at the launch station is to discharge the high-temperature and high-velocity plume generated by the booster ignition during rocket launch in the design direction, so as to ensure the normal operation of the rocket engine and eliminate its damage to surrounding facilities. At present, the main structure of the diversion tank is mostly reinforced concrete, and its working layer is a cast-in-place refractory reinforced concrete protective layer to resist the high temperature thermal shock during rocket launch. [0003]...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B28B23/02F41F3/04
CPCF41F3/04B28B23/02
Inventor 李博平邓智平王坤张孝春王兆肖
Owner 中国人民解放军63926部队
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