Internal combustion engine

FIELD: machine building.

SUBSTANCE: invention relates to power engineering and can be used as an aircraft engine. Internal combustion engine includes tight housing (1) in form of truncated cone partially filled with heat carrier. Housing includes evaporator (2) and capacitor (3). In housing there is a heat-insulation ring (4), which is an element of housing and rigidly fastened with both evaporator and condenser of engine. To heat-insulation ring is rigidly attached impeller (5) of turbine with working blades, encircled by rim (6). Turbine wheel is rigidly secured to hollow shaft (7) of engine. Nozzle is installed on hollow shaft gear (8) of turbine, encircled by a rim (9), which is made up of internal annular magnet. Rims of both wheels are mounted so that annular gap (10) is formed with housing. Wheel with nozzle blades is installed with possibility of rotation relative to hollow shaft - on bearings (11). Above inner annular magnet there is outer annular magnet (12) rigidly connected to housing (13) of aircraft. On hollow motor shaft is rigidly fixed screw (14). In engine housing, in condensation zone, there are heat-conducting rods (15) on which are rigidly fixed plates (16), profile formed by technological operation "rolling" on both sides. Spiral is located around evaporator combustion chamber (17) with nozzles (18). Inside evaporator there is a metallic finely porous sponge (19).

EFFECT: higher engine power, safety of its transportation in idle state, as well as reduced weight and size.

3 cl, 8 dwg

 



 

Same patents:

FIELD: heating.

SUBSTANCE: in both variants, pipe includes case 2 with evaporation zone 3, transport zone 4 and condensation zone 5. In condensation zone, thermoelectric converters 9, radiators 11, cooling them, and elements for thermal contact of the converters with the case and radiators are mounted on the case. Both variants feature pipe where each converter 9 with the said elements is positioned in housing 7 and, together with radiator 14, forms removable heat removal module 6 mounted on the case 2. In the second variant, condensation zone can include a site with radiator contacting the case directly, along with all other components.

EFFECT: simplified pipe maintenance, enhanced reliability, extended utilisation possibilities.

13 cl, 6 dwg

FIELD: engines and pumps.

SUBSTANCE: this engine comprises sealed o shaped to truncated cone partially filled with heat carrier. Said housing accommodates evaporator and condenser, heat insulating ring rigidly secured with both evaporator and condenser sections. Turbine blades working wheels are rigidly secured to heat insulating ring. Turbine working wheels are rigidly secured to engine shaft. Turbine wheels with guide vanes are fitted on the shaft, rim composed of a circular magnet covering said guides vanes. Rims of all wheels are arranged to make a circular clearance with said housing. Wheels with guide vanes are fitted to spin relative to the shaft in bearings. Outer circular magnet rigidly coupled with the housing is arranged above inner circular magnet. Screw is rigidly fitted on engine shaft. Hollow bars are arranged in said condenser. Spiral-shape combustion chamber is arranged around evaporator and includes the nozzle. Radiators are secured to said bars from both inner and outer sides of the housing and composed of trapezoidal plates with bushes arranged radially, said bushes covering the bars with clearance filled with heat conducting paste.

EFFECT: decreased weight and overall dimensions.

6 dwg

FIELD: power industry.

SUBSTANCE: invention relates to heat engineering and can be used in heat exchangers with heat tubes. A heat exchanger with heat tubes for transfer of heat from hot gas to cold gas includes a housing with the first chamber for supply of hot gas through it, the second chamber for supply of cold gas through it and multiple heat tubes spreading between the first chamber and the second chamber. Partition panels are located in the chambers to divide the chambers into compartments with heat tubes; with that, partition panels are located in a plane that is generally parallel to a gas flow through the chambers; with that, direction of the gas flow through one compartment with heat tubes is parallel to gas direction through an adjacent compartment with heat tubes. Heat tubes are assembled into one or more cartridges located so that they can be removed from the corresponding compartments. Each cartridge with heat tubes includes a frame with a support panel, which, when the cartridge is being installed into the compartment, interacts with a partition wall between the first chamber and the second chamber so that gas-tight separation can be formed between the first and the second chambers. Heat tubes cross the support panel and are attached to it in a gas-tight way.

EFFECT: enlarging acoustic characteristics of a heat exchanger due to reduction of vibration induced with flows.

11 cl, 4 dwg

FIELD: heating.

SUBSTANCE: heat transfer panel can be used in temperature control systems of space vehicles (SV) for providing of temperature conditions of the equipment installed in earth satellites, interplanetary stations, landers and other space objects. SV heat transfer panel contains metal skin and built-in heat tubes. The panel is designed as sectional and consists of rigidly connected with each other separate hollow sections with heat tubes. Each section of the panel, including heat tubes, is designed as a uniform monolithic structure.

EFFECT: panel allows to improve the efficiency of heat contact between the cooled equipment and built-in heat tubes, unify the structure components, improve reliability and life of the panel, minimize pollution of SV internal atmosphere at the expense of avoidance of glue from used materials, and significantly simplify the technology of fabrication of instrument panel, which combines in itself heat and strength functions.

11 cl, 7 dwg

FIELD: radio engineering, communication.

SUBSTANCE: invention relates to devices for removing heat from electronic components with high heat dissipation, particularly heat pipes, and can be used in the electronics industry. A heat pipe using tubular fibre-optic structures, the inner side surface of which is lined with tubular optical glass fibres, and the coolant used inside said pipe is a volatile liquid. Use of the volatile liquid (alcohol) as a coolant intensifies heat exchange in the heat pipe via phase transition, thereby creating conditions for controlling temperature of the cooled object.

EFFECT: facilitating movement of liquid from a condensation area to an evaporation area and removing heat radiation from a cooled object.

2 dwg

FIELD: electricity.

SUBSTANCE: invention relates to electrical engineering, to dynamo-electric machines with a cooling system. Dynamo-electric machine (1) includes stator (2) and rotor (3). Winding system (4) is located in slots at least of stator (2). Basically, radial heat transfer is performed by means of heat tubes (5) to end surfaces (6) of stator (2). Each heat tube has evaporation zone (19) and condensation zone (7). Evaporation zone (19) is located inside a closed cooling circuit of the dynamo-electric machine. Heat tubes have woven structure (8) in one end section of the evaporation zone and/or the condensation zone to enlarge the surface of the evaporation zone and/or the condensation zone. Woven structure (8) is heat-conducting and has the possibility of providing air flow swirling in the evaporation zone and/or the condensation zone.

EFFECT: technical result consists in improvement of heat removal without any complication of the design.

14 cl, 5 dwg

FIELD: measurement equipment.

SUBSTANCE: invention relates to instrument-making industry and can be used at control of fluid medium flow rate and temperature. According to this invention, materials, components and methods are aimed at manufacture and use of macro-scale channels containing fluid medium, the temperature and flow rate of which is controlled by means of geometrical sizes of the macro-scale channel and configuration of at least some part of the wall of the macro-scale channel and a flow of composite particles, which form fluid medium. Besides, the wall of the macro-scale channel and the flow of composite particles have such a configuration that collisions between composite parts and the wall can be preferably accompanied by mirror rebound.

EFFECT: improving fluid medium temperature and flow rate control accuracy.

54 cl, 18 dwg

Cooling system // 2518982

FIELD: heating.

SUBSTANCE: cooling system refers to heat engineering, namely to heat mass exchange, and can be used for cooling of different heat releasing elements by removing heat from them to a cooler of any type by a heat pipe. The cooling system comprises a heat pipe as well as a heat releasing element and a cooler which are installed at the opposite pipe ends and are in thermal contact with the pipe. The heat releasing element and the cooler are set with the shift to the heat pipe centre according to the required heat resistance and transferred heat power of the cooling system.

EFFECT: proposed solution allows for significant decrease of cooling system's heat resistance and increase of the power it transfers due to slight shift of the said elements In a particular application example, provided the heat releasing element and the cooler are shifted by 10% of the heat pipe length, the heat resistance decreased by 22% and the transferred heat power increased from 180 W to 220 W.

3 dwg

Condenser // 2505768

FIELD: power industry.

SUBSTANCE: condenser uses heat exchange tubes made from heat-resistant and heat-insulating material as a waste steam cooling device; thermobatteries, the cold junctions of which face inside the tube and the hot ones face the outer side, are mounted in the above heat exchange tubes. Hot air from inter-tube space of the condenser is used for heating of rooms during winter time.

EFFECT: simpler design.

2 cl, 1 dwg

FIELD: transport.

SUBSTANCE: invention relates to spacecraft thermal-control equipment. Proposed system comprises two two-chamber fluid thermal boards 22 to support the equipment. Said thermal boards are mounted at manned compartment 1. External heat sink 12 is composed of four diametrically opposite heat exchange panels 14. Panel 14 is furnished with heat pipe with condenser 15 arranged inside panel 14 and evaporator 19 integrated with self-contained heat transfer element 16 mounted at spacecraft outer surface nearby panel 14. Element 16 comprises two one-chamber fluid thermal boards 18. Evaporator 19 is furnished with steam temperature regulator 17 to shut off or open heat pipe circuit depending upon set temperature. Thermal boards 22 are hydraulically communicated by circuits 13, 21 with appropriate one-way fluid thermal boards 18 of elements 16 to make one-phase working body line. Every circuit 13, 21 comprises electrically driven pump 3, drain-fill valves 5, hydropneumatic accumulator 8, pressure and flow rate gages 4, 7, 10, flow rate controller 11 and electric heaters 23. Every circuit 13, 21 has working body temperature transducers 20. Replaceable elements of said circuits are connected in main lines via hydraulic joints. Main lines are fitted in manned comportment 1 via sealed lead-ins 6. Heat control system comprises also the two-chamber gas-fluid heat exchanger 24 with two replaceable fans included into both circuits 13, 21.

EFFECT: expanded application range, higher reliability and reparability.

1 dwg

FIELD: engines and pumps.

SUBSTANCE: this engine comprises sealed o shaped to truncated cone partially filled with heat carrier. Said housing accommodates evaporator and condenser, heat insulating ring rigidly secured with both evaporator and condenser sections. Turbine blades working wheels are rigidly secured to heat insulating ring. Turbine working wheels are rigidly secured to engine shaft. Turbine wheels with guide vanes are fitted on the shaft, rim composed of a circular magnet covering said guides vanes. Rims of all wheels are arranged to make a circular clearance with said housing. Wheels with guide vanes are fitted to spin relative to the shaft in bearings. Outer circular magnet rigidly coupled with the housing is arranged above inner circular magnet. Screw is rigidly fitted on engine shaft. Hollow bars are arranged in said condenser. Spiral-shape combustion chamber is arranged around evaporator and includes the nozzle. Radiators are secured to said bars from both inner and outer sides of the housing and composed of trapezoidal plates with bushes arranged radially, said bushes covering the bars with clearance filled with heat conducting paste.

EFFECT: decreased weight and overall dimensions.

6 dwg

FIELD: engines and pumps.

SUBSTANCE: external combustion engine includes sealed housing in the form of flattened cone, which is partially filled with heat carrier. Housing includes evaporator and condenser. The housing includes heat-insulating ring being the element of the housing and rigidly attached both to evaporative section, and to condensation section of the engine housing. Turbine impellers with moving blades enclosed with a rim are rigidly attached to heat-insulating ring. Turbine impellers are rigidly attached to engine shaft. Turbine wheels with guide vanes enclosed with the rim representing an internal annular magnet are installed on the shaft. Rims of all wheels are installed so that an annular gap with housing is formed. Wheels with guide vanes are installed with possibility of being rotated in relation to the shaft - on bearings. External annular magnet rigidly attached to the housing is installed above internal annular magnet. Propeller is rigidly fixed on the engine shaft. The condenser includes bars, on which there rigidly fixed are cone-shaped plates of wave-like profile both on internal, and external sides of the housing. Combustion chamber with injectors is located around evaporator.

EFFECT: reducing mass and dimensions characteristics of the engine; enlarging its functional capabilities.

3 cl, 6 dwg

The invention relates to the field of heat, the primary area of application - heat-and-power

The invention relates to energy, in particular to a steam power plant, which converts thermal energy into mechanical

FIELD: engines and pumps.

SUBSTANCE: external combustion engine includes sealed housing in the form of flattened cone, which is partially filled with heat carrier. Housing includes evaporator and condenser. The housing includes heat-insulating ring being the element of the housing and rigidly attached both to evaporative section, and to condensation section of the engine housing. Turbine impellers with moving blades enclosed with a rim are rigidly attached to heat-insulating ring. Turbine impellers are rigidly attached to engine shaft. Turbine wheels with guide vanes enclosed with the rim representing an internal annular magnet are installed on the shaft. Rims of all wheels are installed so that an annular gap with housing is formed. Wheels with guide vanes are installed with possibility of being rotated in relation to the shaft - on bearings. External annular magnet rigidly attached to the housing is installed above internal annular magnet. Propeller is rigidly fixed on the engine shaft. The condenser includes bars, on which there rigidly fixed are cone-shaped plates of wave-like profile both on internal, and external sides of the housing. Combustion chamber with injectors is located around evaporator.

EFFECT: reducing mass and dimensions characteristics of the engine; enlarging its functional capabilities.

3 cl, 6 dwg

FIELD: engines and pumps.

SUBSTANCE: this engine comprises sealed o shaped to truncated cone partially filled with heat carrier. Said housing accommodates evaporator and condenser, heat insulating ring rigidly secured with both evaporator and condenser sections. Turbine blades working wheels are rigidly secured to heat insulating ring. Turbine working wheels are rigidly secured to engine shaft. Turbine wheels with guide vanes are fitted on the shaft, rim composed of a circular magnet covering said guides vanes. Rims of all wheels are arranged to make a circular clearance with said housing. Wheels with guide vanes are fitted to spin relative to the shaft in bearings. Outer circular magnet rigidly coupled with the housing is arranged above inner circular magnet. Screw is rigidly fitted on engine shaft. Hollow bars are arranged in said condenser. Spiral-shape combustion chamber is arranged around evaporator and includes the nozzle. Radiators are secured to said bars from both inner and outer sides of the housing and composed of trapezoidal plates with bushes arranged radially, said bushes covering the bars with clearance filled with heat conducting paste.

EFFECT: decreased weight and overall dimensions.

6 dwg

FIELD: machine building.

SUBSTANCE: invention relates to power engineering and can be used as an aircraft engine. Internal combustion engine includes tight housing (1) in form of truncated cone partially filled with heat carrier. Housing includes evaporator (2) and capacitor (3). In housing there is a heat-insulation ring (4), which is an element of housing and rigidly fastened with both evaporator and condenser of engine. To heat-insulation ring is rigidly attached impeller (5) of turbine with working blades, encircled by rim (6). Turbine wheel is rigidly secured to hollow shaft (7) of engine. Nozzle is installed on hollow shaft gear (8) of turbine, encircled by a rim (9), which is made up of internal annular magnet. Rims of both wheels are mounted so that annular gap (10) is formed with housing. Wheel with nozzle blades is installed with possibility of rotation relative to hollow shaft - on bearings (11). Above inner annular magnet there is outer annular magnet (12) rigidly connected to housing (13) of aircraft. On hollow motor shaft is rigidly fixed screw (14). In engine housing, in condensation zone, there are heat-conducting rods (15) on which are rigidly fixed plates (16), profile formed by technological operation "rolling" on both sides. Spiral is located around evaporator combustion chamber (17) with nozzles (18). Inside evaporator there is a metallic finely porous sponge (19).

EFFECT: higher engine power, safety of its transportation in idle state, as well as reduced weight and size.

3 cl, 8 dwg

Microcooling device // 2247912

FIELD: cooling equipment, particularly heat exchange apparatuses.

SUBSTANCE: device to remove heat from heat-generation component includes coolant stored in liquid coolant storage part, heat absorbing part including at least one the first microchannel and installed near heat-generation component. Heat absorbing part communicates with storage part. Liquid coolant partly fills microchannel due to surface tension force and evaporates into above microchannel with gaseous coolant generation during absorbing heat from heat generation component. Device has coolant condensing part including at least one the second microchannel connected to above coolant storage part separately from the first microchannel, gaseous coolant movement part located near heat-absorbing part and condensing part and used for gaseous coolant movement from the first microchannel to the second one. Device has case in which at least heat-absorbing part is placed and heat-insulation part adjoining heat absorbing part to prevent heat absorbed by above part from migration to another device parts.

EFFECT: reduced size, increased refrigeration capacity, prevention of gravity and equipment position influence on device operation.

22 cl, 4 dwg

Heat pipe // 2254533

FIELD: heat power engineering.

SUBSTANCE: heat pipe comprises vertical housing with evaporation and condensation zones and partially filled with heat-transfer agent and coaxial hollow insert in the evaporation zone which defines a ring space with the housing and is provided with outer fining. An additional hollow cylindrical insert of variable radius made of a non-heat-conducting material is interposed between the condensation zone and coaxial hollow insert. The outer side of the additional insert and inner side of the housing of the heat pipe define a closed space.

EFFECT: reduced metal consumption.

1 dwg

Heat exchanger // 2255284

FIELD: heat power engineering.

SUBSTANCE: heat exchanger comprises housing separated into chambers of evaporation and condensation with a baffle provided with heat pipes which are arranged in both of the chambers. The zones of evaporation of the pipes are positioned inside the evaporation chamber, and zones of the condensation of the pipes are positioned inside the condensation chamber. The heat pipes inside the evaporation chamber are made of wound pipes of oval cross-section. The zones of condensation of heat pipes are also made of wound pipes of oval cross-section .

EFFECT: enhanced efficiency.

1 cl, 6 dwg

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