RU2306364C2 - Composite material, method of manufacture of envelope-like case from this material and devices for realization of this method - Google Patents

Abstract

FIELD: aeronautical and space engineering.

SUBSTANCE: proposed composite material contains metal matrix made from aluminum-lithium alloy and magnesium-lithium alloy and strengthened with carbon fibers and carbon part strengthened with carbon fibers with outer layer of carbo-nitride compounds of titanium. Metal matrix and carbon part are connected by intermediate layer of carbonized polymer binder at heating within interval of polymer binder carbonization temperatures at simultaneous cooling of metal part with gas-and-liquid flow on base of nitrogen. Envelope-like case is assembled of at least two ferrules. Layer of polymer binder is applied on metal surface of welded zone between end bases of carbon parts strengthened with carbon fibers and carbon half-rings strengthened with carbon fibers are laid on it. Clearances are filled with polymer binder which is subjected to gas-dynamic sealing and heating for removal of hydrogen. Then binder is subjected to carbonization in clearance at simultaneous cooling of inner metal surface in zone of action of thermal source and graphitization of binder at simultaneous forming of outer layer from carbo-nitride titanium compounds by means of laser flame. Plasma torch is provided with Venturi nozzle with holes in nozzle body found after throat section for feeding the titanium powder into plasma flame.

EFFECT: enhanced strength and heat-resistance of articles; possibility of retaining preset geometric parameters.

7 cl, 6 dwg, 2 tbl

Description

The invention relates to a technology for manufacturing shells from composite material.

Known carbon-carbon (C-C) composite material (CM) containing carbon fabric and reinforced with carbon fiber (See Tuchinsky LI Composite materials obtained by the method of impregnation. M .: Metallurgy, 1986, p.186-190) .

The disadvantages of the known KM are:

- low heat resistance when used in air;

- low tightness of the material.

Closest to the proposed CM based on aluminum-lithium and magnesium-lithium alloys, reinforced with carbon fiber (RF patent No. 2171311, BIPM No. 21-2001).

A disadvantage of the known KM is low heat resistance and heat resistance during its operation in air.

A known method and device for the manufacture of parts such as shells of a metal composite material, comprising forming a composition of a metal matrix and carbon fiber, followed by impregnation with liquid metal, hot pressing and diffusion welding (RF Patent No. 2171311, BIPM No. 21-2001).

However, in the manufacture of a semi-finished product from a composite carbon-carbon material by a similar method in the known device it is difficult to provide a tight seal of the outer end layer of the base due to the increased elasticity of the material.

A known method and device for electron beam welding of shell-type housings, including a vacuum chamber, a mechanism for moving and rotating the workpiece, a manipulator for scanning the treated surfaces with a welding head along a given path (A.I. Chvertka and other equipment for electron beam welding. Kiev : Naukova Dumka, 1973)

The use of electron beam welding requires the use of a sealed chamber to create the necessary vacuum.

The aim of the present invention is to develop a CM with internal metal and external non-metal parts of the matrix reinforced with carbon fiber having an external external heat-resistant layer, and a method of manufacturing from it solid bodies such as shells with increased rates of specific strength, heat resistance and heat resistance, tightness, as well as devices, providing effective implementation of the method.

The technical result obtained as a result of the invention is the achievement of high indicators of specific strength, tightness, heat resistance and heat resistance of KM in the construction of shell-type housings, which leads to a significant reduction in mass, increased resistance to thermal effects and increased reliability of aviation, rocket and space products.

The goal is achieved by obtaining a CM containing a metal matrix made of aluminum-lithium alloy and magnesium-alloy alloys, hardened with carbon fiber, according to the invention it is equipped with a carbon part, hardened by carbon fiber, connected by an intermediate layer of a carbonized polymer binder with a metal matrix, and the outer layer of titanium carbonitride compounds.

A method of manufacturing parts such as shells of the inventive composite material consists of several stages.

It includes the manufacture of the metal part of the shell reinforced with carbon fiber, the manufacture of the carbon part reinforced with the carbon fiber and the outer layer of titanium carbide compounds, the assembly of the parts by putting the carbon part on the metal part, filling the gap between them with a polymer binder by vacuum absorption under inert gas overpressure and heated in the temperature range of carbonization of the polymer binder with simultaneous cooling of the metal part of the shell.

In addition, the cooling of the metal part of the shell in the zone of influence of the heat source is carried out by a gas-liquid stream based on nitrogen.

A shell type case of KM is made by welding metal parts of the shells, according to the invention, the body is assembled of at least two shells, a layer of polymer binder is applied onto the metal surface of the welded zone between the end bases of the carbon fiber-reinforced carbon parts of the shells, onto which carbon half-rings reinforced with carbon fiber are laid , fill the gaps with a polymer binder, carbon fiber and simultaneously conduct gas-dynamic compaction of the binder, warm up for hydrogen, conduct carbonization of the polymer binder in the gap with simultaneous cooling of the inner metal surface in the zone of influence of the heat source, and graphite the binder with the simultaneous formation of the outer layer of titanium carbonitride compounds by a plasma torch into which titanium powder is fed, and nitrogen gas is used as the plasma-forming medium .

For the manufacture of a shell for a housing such as a shell from KM, a device containing heating, vacuum and inert gas inlet systems, a prefabricated mandrel for forming and mounting parts of the shell, support and retaining rings, gaskets installed on the upper and lower end platforms of the shell, and a hollow shell are used composite rack, according to the invention, it is equipped with a mechanism for sealing the end surfaces of the metal and nonmetallic parts of the shell associated with the upper support ring, and the lower part is hollow The composite rack is filled with a polymer binder.

In addition, the device is equipped with a system for supplying and discharging the cooling medium, while the mandrel has internal cavities for the passage of the cooling medium.

A device for manufacturing a shell type of a shell made of KM contains a slipway with rotation and displacement drives, according to the invention it is equipped with a manipulator with a nozzle for supplying a polymer binder and its gas-dynamic seal for connecting the carbon-fiber reinforced carbon parts of the shells of the shell housing, including the Venturi nozzle, a movable ring heater for heating the outer metal surface of the welded zone, a movable ring cooler for cooling the inner metal the surface of the welded zone and a manipulator with a plasma torch, including a Venturi nozzle with holes in the nozzle body after a critical section for feeding titanium powder into the plasma torch.

To form titanium nitride compounds, titanium powder is fed into the plasma torch, and nitrogen gas is used as the plasma-forming medium.

In order to eliminate carbon oxidation during carbonization and graphitization, these processes are carried out in an inert medium, having previously removed oxygen.

In order to effectively remove hydrogen from the polymer binder, the latter is degassed by heating and evacuating hydrogen molecules from the surface with an inert gas stream.

The formation of a porous intermediate layer of a carbonized polymer binder is promoted by thermal insulation of the metal part of KM from external temperature influences during operation of the product.

Table 1 shows the calculated characteristics of the proposed CM with metal and nonmetallic parts of the matrix and a heat-resistant outer layer of titanium carbonitride compounds in comparison with the operational characteristics of aluminum-lithium alloy and carbon-carbon CM.

Table 1 Materials ρ, g / cm ³ σв, MPa E, GPa

Mp, ° C TJS, ° C Germetich Note 1. The proposed composite material, including: 1.7 761.8 204.0 448.1 4500 2400 1,0 Estimated data 1.1. Carbon Fiber Reinforced Aluminum Lithium and Magnesium Lithium Alloys 1.2. Porous carbonized carbon insulating material 1.3. Carbon-carbon material with a heat-resistant outer layer of titanium carbo-nitride compounds 2. 01420 (aluminum-lithium alloy) 2,4 420 90.0 175.0 600 400 1,0 Reference data 3. KM S-C (carbon-carbon composite material) 2.0 870.0 220.0 435.0 4500 400 <1.0 Reference data

As can be seen from table 1, the values of strength characteristics, specific strength, tightness and heat resistance significantly exceed the same parameters for known alloys and materials.

The invention is illustrated in the drawing, which shows: Fig. 1 is a cross-sectional view of a proposed KM shell type case with a metal part of a matrix based on aluminum-lithium alloy and magnesium-lithium alloys reinforced with carbon fiber, and a carbon-carbon part with an outer layer of carbonitride compounds titanium, as well as an intermediate layer of carbonized polymer binder between them; figure 2 is a graph of the processes of evacuation, impregnation (filling) and carbonization of the polymer binder; figure 3 is a diagram of a device for degassing and filling with a polymer binder the gap between the metal and nonmetallic parts of the shell; figure 4 is a diagram of a device for the manufacture of shell-type housings (assembling half rings from CC CC on the surface of the welded zone of the metal part of the two shells, filling the gaps with a polymer binder, followed by its carbonization, graphite and the formation of a surface layer of titanium carbonitride compounds); figure 5 - diagram of the nozzle for applying a polymer binder; 6 is a diagram of a plasma torch for graphitizing a polymer binder and forming a surface layer of titanium carbonitride compounds.

KM (see figure 1) consists of the following elements:

A - aluminum-lithium alloy (Al-Li);

B - magnesium-lithium alloy (Mg-Li) with the structure of (α + β) - solid solution:

C - magnesium-lithium alloy (Mg-Li) with the structure of α - solid solution;

D is carbon fiber;

F - magnesium-lithium alloy (Mg-Li) with the structure of β - solid solution;

E - carbonized polymer binder;

K is the carbon-carbon part of KM;

T is the outer outer layer of titanium carbonitride compounds.

Figure 2 presents:

a is a graph of the process temperature (° C);

b - graph of changes in the external overpressure of the pressing gas (atm);

in - a graph of pressure changes over the surface of the molten polymer binder (ATM);

g is a graph of changes in the suction discharge of the internal cavity between the metal and non-metal parts of the CM (mm Hg)

Table 2 shows the process flow diagram of manufacturing a shell body from the proposed composite material.

table 2 1. Preparatory operations 1.1. Assembly of part of the semi-finished shell, frame from KM Al-Mg-C-Mg-Al Wrapping the mandrel with a sheet of aluminum-lithium alloy, tightly connecting the sheet along the longitudinal generatrix, wrapping the semi-finished product with sheets of magnesium-lithium alloys with structures (α + β) -, α-, and β- solid solutions, laying carbon fiber (winding), wrapping prefabricated sheets of magnesium-lithium alloys with structures of β-, α-, (α + β) - solid solutions, wrapping and tight connection of the sheet of aluminum-lithium alloy along the longitudinal generatrix. 1.2. Assembly of a part of a semi-finished shell, rings from KM С-С Wrapping the mandrel with a sheet of mild steel, hermetically welding the sheet along the longitudinal generatrix, wrapping the metal sheet with carbon fabric, flashing the fabric along the longitudinal generatrix, winding (laying) carbon fiber, wrapping the semi-finished product with carbon fabric and flashing along the longitudinal generatrix, wrapping the prefabricated sheet with titanium alloy and tight welding along the longitudinal generatrix, tightness control of welds. 2. Lithium impregnation, hot pressing and diffusion welding KM Al-Mg-Li-C-Li-Mg-Al Shell Parts 2.1. Installation of a part of a semi-finished product with a metal matrix in technological equipment; loading accessories with a semi-finished product into the furnace, connecting the accessories to a vacuum pumping system, inert gas inlet systems, sealing, hot isostatic pressing through the liquid phase of lithium, followed by diffusion welding of the composite material Mechanical tight connection of the surface (end) layers of the shell part with the evacuated cavities of the tool, loading the inner cavity of the rack with metal lithium, connecting the tool to the vacuum system and monitoring the tightness of the joints 3. Impregnation with a polymer binder, carbonization and graphitization of part of the shell from KM C-C. 3.1. Installation of a part of a semi-finished shell with a non-metal matrix in technological equipment, filling the internal cavity of the rack with a polymer binder, loading the equipment into the furnace; impregnation with a polymer binder of a matrix and a reinforcing fiber; carbonization of a polymer binder. Filling the internal cavity of the equipment rack with a polymer binder, tightly connecting the end surfaces of the metal and non-metal parts of the semi-finished shell with the evacuated equipment cavities, connecting the cooled equipment cavities to the cooling medium supply systems. 3.2. Graphitization of a carbonized polymer binder, nitriding of the outer outer titanium layer with simultaneous heat setting of the semifinished product bases and application of tensile stresses Loading the carbonized prefabricated shell into a high-temperature vacuum furnace, thermofixing the shell bases and applying tensile stress to the shell material between the bases. 4. Assembly of metal and non-metal parts of the shell (figure 1). Filling the gap between the metal and nonmetallic parts of the shell with a polymer binder, followed by its carbonization. 4.1. Installation of a semi-finished shell into technological equipment, loading of equipment into the furnace, connection to a vacuum pumping system, inert gas inlet systems, cooling and sealing systems; hot degassing of the polymer binder followed by its carbonization (figure 3) Filling the inner cavity of the equipment rack with a polymer binder, hermetically connecting the end surfaces of the metal and nonmetallic parts of the shell semi-finished product with evacuated equipment cavities, connecting the cooled equipment cavities to the cooling medium supply systems (according to the processing modes in FIG. 2) 5. Welding adjacent metal end surfaces of the shells and welding to the inner side of the welded zone of the shell of the frame from KM (Al-Mg-Li-C-Li-Mg-Al) 5.1. Preparation of end metal surfaces of shells, their welding in a protective environment. Mechanical
Electron beam welding 5.2. Welding to the inner metal surface of the welded zone of the shell body of the frame made of KM (Al-Mg-Li-C-Li-Mg-Al) Mechanical
Electron beam welding 6. Application of a polymer binder shell on the outer metal surface of the welded zone of the shell body, laying of half rings from KM C-C, filling the gap with a polymer binder, carbonization, graphitization and the formation of a surface layer of titanium carbonitride compounds. 6.1. Downloading the welded shell semi-finished product to the stand (Fig. 4), applying a polymer binder to the outer metal surface of the welded zone, laying half rings from KM С-С followed by carbonization of the polymer binder. Using a nozzle (Fig. 5), a polymer binder is applied to the metal surface, half rings made of KM C-C are laid, the polymer binder is heated using an annular heater (Fig. 4) until the carbonization process is complete, and the inner metal surface of the welded zone is cooled by gas-liquid flow based on liquid nitrogen. 6.2. Filling the gaps with a polymer binder, sealing and its carbonization (figure 4) Using the nozzle (figure 5) fill the gap with a polymer binder with its simultaneous gas-dynamic seal; using a heater (Fig. 4), the polymer binder is heated until hydrogen is completely removed; re-fill, compact and warm the polymer binder; the gap filled with a degassed binder is heated until the carbonization process is complete, while the internal metal surface of the weld zone is cooled by a gas-liquid stream based on liquid nitrogen. 6.3. Graphitization of a carbonized polymer binder in the gap with the simultaneous formation of a surface layer of titanium carbonitride compounds. Heating the carbonized filler in the gap with a plasma torch (Fig. 6) while supplying titanium powder to the plasma torch (nitrogen gas is used as the plasma-forming medium)

Figure 3 presents a device for implementing a method of manufacturing a shell of KM with metal and non-metal parts of the matrix by impregnating the filling of the gap between the parts of the matrix with a polymer binder followed by its carbonization.

It includes a vacuum furnace 1, a thermally insulated muffle 2 and accessories for impregnation (filling), degassing and carbonization of the polymer binder with simultaneous hot isostatic pressing of the material of the semi-finished shell.

The equipment includes upper 3 and lower 4 support rings. Each ring 3, 4 is provided with an annular protrusion 5 having the shape of a truncated cone.

In addition, snap-in includes external locking rings 6, respectively upper and lower, assembly mandrel 7, hollow composite stand 8, 9, radial pipes 10 and connecting pipes 11 and 12. The pipes 10 are connected to the upper 9 and lower 8 parts of the rack and with upper 3 and lower 4 rings, respectively.

In each of the rings 3, 4, in the center of the protrusion 5, an annular groove 13 is made with a center of a circle coinciding with the center of the circumference of each ring 3, 4. In addition, radial channels 14 are made in the rings 3, 4, which are connected to the nozzles 10, and communicate with the annular grooves 13.

The lower 8 and upper 9 cavities of the rack are separated by a sealed partition 15. The lower part 8 of the hollow rack is fastened to the ring 4, and the upper part 9 to the ring 3 and through the connecting pipes 11,12 are connected with the inert gas inlet system and the vacuum system, respectively. (The latter are not shown in the drawing.)

The prefabricated mandrel 7 has a cylindrical shape and consists of several parts for mounting the shell-semi-finished product 16 and its dismantling.

The mandrel 7 has communicating cooled cavities 25 and is connected to the liquid-nitrogen gas-liquid supply system by a flexible pipe 24 with a flexible connector and a pipe 22 for removing nitrogen gas.

The upper and lower retaining rings 6 are connected by a technological shell 17.

The fixing outer rings 6 with the technological shell 17, the upper and lower external chamfers of the mandrel 7 fix the end outer layers of the shell matrix KM of the semi-finished product 16 through the annular sealing gaskets to the flat platforms of the conical protrusions of the rings 3, 4 facing each other.

The cavity formed by the technological shell 17 and the outer outer surface of the matrix KM of the semi-finished shell 16 is connected by a pipe 18 with a flexible connector with a vacuum and pressurized inert gas injection system.

To ensure uniform heating and cooling of the tooling and the mandrel 7 with the shell 16, the furnace 1 is equipped with a fan 19, a heat exchanger 20, valves 21.

The upper 3 support ring through a detachable connection is connected with the movement mechanism (seal) 23.

First, the prefabricated shell 16 is assembled on the mandrel 7. For this, the metal part of the shell of KM Al-Mg-Li-C-Li-Mg-Al is put on the mandrel 7, then the carbon-carbon part of the shell is often put on the metal shell.

Next, the mandrel 7 with the semi-finished product 16 is mounted in a snap.

The inner lower cavity of the rack 8 is filled with a polymer binder.

Lay the sealing ring gaskets on the conical protrusion 5 of the lower ring 4 and install the semi-finished shell 16 with the mandrel 7. The ring 4, the semi-finished product 16 with the bottom of the rack 8 are loaded into the muffle 2 of the furnace 1.

Then, the upper 3 of the support ring, the radial pipes 10, the upper 9 of the rack with the pipelines 11, 12 are assembled. The ring 3 and the upper part 9 of the rack are hung and fixed on the guide rods of the movement and sealing mechanism 23 of the furnace lid 1.

Dress the process shell 17 with the retaining rings 6 on the semi-finished shell 16, and the sealing ring gaskets are laid.

Pipelines 11, 12, 18, 24, 22 are connected to systems of evacuation, inert gas inlet, supply and removal of a cooling medium.

Lower the lid of the furnace 1 and install the upper ring 3 assembly with a conical flat protrusion on the O-rings and the mechanism 23 seals the gaps between the flat and conical protrusions of the rings 3.4 and the end outer layers of the composite material of the semi-finished shell 16, as well as between the upper 9 and lower 8 parts of the rack.

Then, in the device (Fig. 3), the gap between the metallic and non-metallic parts of the shell of the polymer binder is filled, degassed and carbonized. (The parameters of filling, degassing and carbonization are shown in figure 2.)

After sealing the furnace 1, turn on the pumps and vacuum the furnace 1 and the internal cavity of the matrix of the semi-finished shell 16 (through grooves 13, channels 14, nozzles 10, pipe 12), the cavity between the technological shell 17 and the outer outer surface of the non-metallic part of the semi-finished shell 16 through the pipe 18 to predetermined vacuum (see figure 2, 3).

When the temperature of the liquid state of the polymer binder (about 100 ... 200 ° C) is reached, the pipeline 12 is closed, the lower cavity 8 of the rack is connected to the inert gas inlet system and overpressure is created through the pipe 11 above the surface of the polymer binder.

The vacuum pumps are turned off, at the same time, the fan 19 is turned on and the working volume of the furnace 1 is filled with inert gas, an inert gas is pressed into the cavity between the process shell 17 and the external outer surface of the non-metallic part of the shell semi-finished product.

At the end of the process, the heating is turned off, the valves 21 are opened and the cooling medium is supplied to the heat exchanger 20, the equipment, the mandrel 7 with the shell 16 are cooled to ambient temperature, the overpressure is relieved, the tool, the mandrel 7 with the shell 16 are unloaded and the equipment and the mandrel are dismantled.

Figure 4 presents a diagram of a device for assembling a shell body: applying a polymer binder to the welded zone of the welded zone, laying half rings from KM C-C, filling the gap with a polymer binder, carbonization, graphitization, and forming a surface layer of titanium carbonitride compounds.

The device includes a slipway with drives for moving and rotating the welded shell of the shell 26, an annular heater 27 with a drive for moving along the outer surface of the housing 26, a ring cooler 28 with a drive for moving along the inner surface of the shell 26, a manipulator 29 with a nozzle 30 for spraying a polymer binder and with a drive for moving along the outer surface of the housing 26, the manipulator 31 with a plasma torch 32 and a displacement drive along the outer surface of the housing 26. (The drives are not shown in the drawing, schematically given in The pressure of the displacement drives.)

The ring heater 27 includes a thermally insulated housing 33, a heating element 34, an inert gas ring inlet 35.

The ring cooler 28 includes a spiral insulated pipe 36 for supplying cooled gaseous nitrogen, a spiral pipe 37 for supplying liquid nitrogen is placed inside the pipe 36. Both pipelines have coaxial openings on the side of the cooled inner metal surface of the housing 26 and are intended for supplying and forming a cooling gas-liquid medium based on liquid nitrogen.

The nozzle 30 (FIGS. 4, 5) includes a supply line 38 of a polymer binder, a supply of nitrogen gas 39, a mixing chamber 40 and a venturi nozzle 41.

The plasma torch 32 (FIGS. 4, 6) includes a plasma nitrogen gas supply line, a Venturi nozzle 42 with holes in the nozzle body after a critical section for supplying titanium powder through a collector 43 into a plasma torch.

The method of filling the gap with a polymer binder, carbonization, graphitization and the formation of the surface layer of titanium carbonitride compounds is as follows.

A prefabricated shell case assembled from several shells, consisting of metal and nonmetallic parts with a carbonized polymer bond, and a welded zone between the metal end parts of the shells, are mounted on the drive rollers of the slipway.

An annular cooler 28 is introduced into the inner metal part of the semi-finished shell body of the shell and set it opposite the inner surface of the welded zone.

Using the drive, the manipulator 29 with the nozzle 30 is moved to the area of the external weld of the metal parts of the shells.

In the nozzle 30 serves a polymer binder and gaseous nitrogen. A layer of polymer binder is sprayed onto the metal surface of the welded zone.

Stack (glue) the half rings from KM C-C and fill the gaps between them with a polymer binder with its simultaneous gas-dynamic compaction using the Venturi nozzle 41 of the nozzle 30.

The nozzle 30 is removed from the welded zone and the ring cooler 28 is moved against the inner surface of the welded zone with the help of drives, and the ring heater 27 is moved opposite the outer surface of the welded zone.

An annular heater 27 heats the polymer binder until hydrogen is completely removed (temperature 300 ... 400 ° C).

Next, the polymer binder, degassed by heating, is heated with a heater 27 until its carbonization is completed while cooling the inner metal surface of the welded zone using cooler 28 with a gas-liquid stream based on liquid nitrogen.

Heater 27 is removed from the welded zone and, using a drive, the manipulator 31 with the plasma torch 32 is moved to the welded zone.

The carbonized polymer binder is heated in the gap between the half rings of KM C-C plasma torch 32 with the simultaneous supply of titanium powder to the plasma torch through the holes of the Venturi nozzle 42.

Nitrogen gas is used as the plasma forming medium.

Upon completion of the graphitization processes and the formation of the surface layer of titanium carbonitride compounds (by the formation of titanium nitride compounds in the plasma torch and their subsequent interaction with the carbon surface), the supply of titanium powder 32 to the plasma torch is stopped, the plasma is turned off, and nitrogen gas supply is stopped.

Turn off the supply of gaseous and liquid nitrogen to the cooler 28.

Using the drive of the stand, the shell element 26 is removed from the range of the manipulators 29, 31, the heater 27, the cooler 28.

Compared with the known analogues, the proposed composite material and the method of manufacturing shell-type housings from it allow a higher level of strength, heat resistance and tightness to be obtained, and the proposed devices for implementing the method will require significantly lower capital investments and costs.

Claims (7)

1. Composite material containing a metal matrix made of aluminum-lithium alloy and magnesium-lithium alloys, hardened with carbon fiber, characterized in that it is provided with a carbon part, hardened by carbon fiber, connected by an intermediate layer of a carbonized polymer binder with a metal matrix and the outer a layer of titanium carbonitride compounds. 2. A method of manufacturing a shell for a shell type shell made of composite material, comprising manufacturing a metal part of a shell reinforced with carbon fiber, characterized in that the carbon part reinforced with a carbon fiber is fabricated, put on a metal part, and the gap between them is filled with a polymer binder by vacuum suction under overpressure of an inert gas and heated in the temperature range of carbonization of the polymer binder with simultaneous cooling of the metal th part of the shell. 3. The method according to claim 2, characterized in that the cooling of the metal part of the shell in the zone of influence of the heat source is carried out by a gas-liquid stream based on nitrogen. 4. A method of manufacturing a shell type shell made of composite material, including welding of metal parts of the shells, characterized in that the body is assembled of at least two shells, a layer of polymer binder is applied to the metal surface of the welded zone between the end bases of the carbon parts reinforced with carbon fiber shells, which are laid with carbon fiber-reinforced carbon half rings, fill the gaps with a polymer binder and at the same time conduct gas-dynamic compaction of the binder, they are heated to remove hydrogen, the polymer binder is carbonized in the gap with simultaneous cooling of the inner metal surface in the zone of influence of the heat source, and the binder is graphitized with the formation of the outer layer of titanium carbonitride compounds by a plasma torch into which titanium powder is fed, and as a plasma-forming medium, gaseous nitrogen. 5. A device for manufacturing a shell for a shell type shell made of composite material, containing heating, vacuum and inert gas inlet systems, a prefabricated mandrel for forming and mounting parts of the shell, support and fixing rings, gaskets installed on the upper and lower end pads of the shell, and a hollow composite stand, characterized in that it is equipped with a sealing mechanism for the end surfaces of the metal and nonmetallic parts of the shell associated with the upper support ring, and the bottom nn integral part of the hollow rack filled with a polymer binder. 6. The device according to claim 5, characterized in that it is provided with a system for supplying and discharging a cooling medium, while the mandrel has internal cavities for the passage of the cooling medium. 7. A device for manufacturing a housing such as a shell made of composite material, containing a slipway with rotation and displacement drives, characterized in that it is equipped with a manipulator with a nozzle for supplying a polymer binder and its gas-dynamic seal to connect the carbon fiber reinforced carbon parts of the shell shell shells, including Venturi nozzle, movable ring heater for heating the outer metal surface of the welded zone, movable ring cooler for cool the inner metal surface of a welded zone and a manipulator with a plasma torch, comprising a venturi nozzle holes in the nozzle body after the critical section, for supplying a plasma torch titanium powder.

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