Abstract: The present invention specifically relates to equipment and a method for preparing an aerogel thermal insulation mortar for a high-temperature kiln thereof. The equipment comprises a top box, a support frame platform, a processing mechanism, an agitation mechanism, a receiving mechanism and a docking mechanism, wherein the top box is provided with a partition frame capable of dividing an inner space thereof into a first material discharge cavity, a second material discharge cavity, a third material discharge cavity and a fourth material discharge cavity respectively; the receiving mechanism is mounted on an inner top of the support frame platform and docked with the top box; the docking mechanism is mounted on the receiving mechanism; an inner bottom of the support frame platform is provided with a collection box; one side of the top box is provided with a door panel.

Abstract: The present invention specifically relates to equipment and a method for preparing an aerogel thermal insulation mortar for a high-temperature kiln thereof. The equipment comprises a top box, a support frame platform, a processing mechanism, an agitation mechanism, a receiving mechanism and a docking mechanism, wherein the top box is provided with a partition frame capable of dividing an inner space thereof into a first material discharge cavity, a second material discharge cavity, a third material discharge cavity and a fourth material discharge cavity respectively; the receiving mechanism is mounted on an inner top of the support frame platform and docked with the top box; the docking mechanism is mounted on the receiving mechanism; an inner bottom of the support frame platform is provided with a collection box; one side of the top box is provided with a door panel.

Abstract: Disclosed are a cabin pipeline using a super thermal insulation material and a preparation method thereof, comprising an electrically conductive inner pipe, an anti-corrosion coating coated on the electrically conductive inner pipe, a thermal insulation layer formed by a super thermal insulation material wound on the anti-corrosion coating, and a resin sealing layer coated on an outside of the thermal insulation layer. The electrically conductive inner pipe has excellent corrosion resistance to liquefied natural gas in the pipeline; the protective layer formed by the anti-corrosion coating and the resin sealing layer can prevent the electrically conductive inner pipe from being directly exposed to the environment due to long-term seawater infiltration or accidental damage of the outer layer, avoid electrochemical corrosion and further improve the corrosion resistance.

Abstract: The invention discloses an integrated manufacturing system and method for a small-deformation self-diagnosis shield segment, wherein the designed installation process saves time and effort, and all the sensing modules are provided inside the segment without disturbing the space outside the segment. Integration of all the deformation self-diagnosis shield segments is achieved by comprehensively monitoring inclination, displacement, strain, pressure and temperature of the shield segments via five monitoring modules. At the same time, the obtained data is uploaded to a database, and various contents are displayed in real time according to indication information input by a user.

Abstract: Disclosed are a cabin pipeline using a super thermal insulation material and a preparation method thereof, comprising an electrically conductive inner pipe, an anti-corrosion coating coated on the electrically conductive inner pipe, a thermal insulation layer formed by a super thermal insulation material wound on the anti-corrosion coating, and a resin sealing layer coated on an outside of the thermal insulation layer. The electrically conductive inner pipe has excellent corrosion resistance to liquefied natural gas in the pipeline; the protective layer formed by the anti-corrosion coating and the resin sealing layer can prevent the electrically conductive inner pipe from being directly exposed to the environment due to long-term seawater infiltration or accidental damage of the outer layer, avoid electrochemical corrosion and further improve the corrosion resistance.

Abstract: The present application discloses an aerogel composite heat preservation fire-proof plate and a manufacturing process thereof. The aerogel composite heat preservation fire-proof plate comprises an upper surface layer, a fire-proof layer, a heat insulation layer, a polyurethane layer, and a lower surface layer which are compositely arranged from top to bottom in sequence. The interior of the fire-proof layer is hollow and filled with aluminum hydroxide particles. Working holes are uniformly formed in the fire-proof layer. Sealing double-screw bolts are connected in the working holes. Aerogel mounting grooves are uniformly formed in the surface, close to the fire-proof layer, of the heat insulation layer. There are heat insulation air cavities at one side, far away from the fire-proof layer, of the mounting grooves. The air cavities are communicated with all the mounting grooves. Aerogel fillers are arranged in the mounting grooves.

Abstract: The present disclosure discloses a high-temperature aerogel heat insulation coating, preparation equipment and a use method for the preparation equipmen. A supporting leg frame is arranged on the outer side wall of the reaction tank; a storage cavity is formed in the upper outer box; a dispersing shaft is arranged in the storage cavity; dispersing blades are installed on the dispersing shaft; a dispersing motor and a material guiding pipe are arranged outside the upper outer box; an unloading mechanism is arranged under the reaction tank; and an exhaust hole and a feeding hole are formed in the outer part of the reaction tank.

Abstract: The present application discloses an aerogel composite heat preservation fire-proof plate and a manufacturing process thereof. The aerogel composite heat preservation fire-proof plate comprises an upper surface layer, a fire-proof layer, a heat insulation layer, a polyurethane layer, and a lower surface layer which are compositely arranged from top to bottom in sequence. The interior of the fire-proof layer is hollow and filled with aluminum hydroxide particles. Working holes are uniformly formed in the fire-proof layer. Sealing double-screw bolts are connected in the working holes. Aerogel mounting grooves are uniformly formed in the surface, close to the fire-proof layer, of the heat insulation layer. There are heat insulation air cavities at one side, far away from the fire-proof layer, of the mounting grooves. The air cavities are communicated with all the mounting grooves. Aerogel fillers are arranged in the mounting grooves.

Abstract: The present disclosure discloses a high-temperature aerogel heat insulation coating, preparation equipment and a use method for the preparation equipmen. A supporting leg frame is arranged on the outer side wall of the reaction tank; a storage cavity is formed in the upper outer box; a dispersing shaft is arranged in the storage cavity; dispersing blades are installed on the dispersing shaft; a dispersing motor and a material guiding pipe are arranged outside the upper outer box; an unloading mechanism is arranged under the reaction tank; and an exhaust hole and a feeding hole are formed in the outer part of the reaction tank.

Abstract: The invention belongs to the technical field of ships, and relates to an aerogel heat preservation ship rescue cabin, which comprises a cabin body. The cabin body and arc-shaped plates are made of aerogel materials. Water pumping devices are symmetrically sleeved outside the cabin body near two sides. A straight pipe is connected between the two water pumping devices. Strip-shaped water outlet holes are formed at front and rear sides of the straight pipe in a penetrating manner. A heat insulation plate is sleeved on the cabin body and hollow, and two ends thereof are communicated with the water outlet holes at front and rear sides of the straight pipe. Multiple drainage holes are formed in the inner wall, opposite to the cabin body, of the heat insulation plate in a penetrating manner. Multiple evaporation holes are formed in the top of the heat insulation plate in a penetrating manner.