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Empresa búlgara ofrece un turbomotor de combustión interna con turbina para transporte aéreo y por carretera

Resumen

Tipo:
Oferta Tecnológica
Referencia:
TOBG20171213001
Publicado:
08/01/2018
Caducidad:
08/01/2019
Resumen:
Una empresa búlgara ha desarrollado un turbomotor pequeño de combustión interna con turbina que ofrece un momento de rotación alto y una mayor eficiencia. Este turbomotor puede ponerse en marcha por un operador y/o controlador lógico programable (PLC). Para alcanzar el grado anticipado de grosor preliminar de la mezcla aire-combustible o del aire, las cámaras del motor son alimentadas a la fuerza con aire a alta presión. Este motor es más compacto, económico, potente y dinámico y tiene un número menor de piezas de baja inercia, además de poder fabricarse e instalarse de forma sencilla. La empresa busca un fabricante de motores para vehículos de transporte y turbinas empleadas en turbocompresores para establecer acuerdos de cooperación técnica y financiación.

Details

Tittle:
Bulgarian company offers invention relates to a turbine internal combustion turbo engine for air and road transport.
Summary:
The invention relates to a turbine internal combustion turbo engine,small- sized,with higher rotating moment and higher efficiency, which can be operated by an operator and/or by a programmable logical controller (PLC). The engine turbine is housed in the turbine vessel of the engine and rotates resting in its bearing hubs. To reach the anticipated degree of preliminary thickness of the air-fuel mixture or of the air, the working chambers of the engine are forcibly fed with high-pressure air.
Description:
A design company, specified in the field of innovative classic piston and innovative turbine engines with internal combustion: innovative turbine engines with external combustion - gas, air and steam turbines for low, high pressure: innovative gas and air mono-stage single and multi-stage compressors for low, medium and high compressed gases: classical systems for measurement and automation of technological processes in the sector of air and road transport.
The offered technology is an engine stationary turbine vessel, hereinafter called the vessel, has at its both ends coaxial, transverse, eccentric flanges through whose outer parallel face walls are made peripheral connecting openings and oil-leading channels which are in their lowest part and are joined to an oil carter which is hermetically connected to the vessel in whose walls are made liquid cooling chambers. In the vessel there is a longitudinal opening in which on both sides of the vessel and opposite each other are hermetically and coaxially placed: an immovable long T-shaped part and a movable short T-shaped part with a plastic spring on it movable on its axis; the two T-shaped parts of the vessel turbine sleeve have their external front bearing foot blocks, equal inside diameters and are internally and hermetically connected according to the compensating channel-tooth system. Passing hermetically, longitudinally and coaxially through the vessel wall and the wall of the turbine sleeve are made the engine reactive exhaust ports having parallel
axes and a common exhaust collector and connected with the atmosphere through the exhaust system. Passing hermetically, longitudinally and coaxially through the vessel and turbine sleeve walls and parallel to the reactive exhaust ports are made air-whirling blow ports of the engine connected with each other through their common longitudinal blow collectors and through it with the forced-filling system for high-pressure air. The injection openings of the engine are bored to pass longitudinally, transversely and coaxially through the vessel and turbine sleeve wall and are parallel to the air-whirling blow ports. The spark-ignition and fuel-injection openings of the engine are bored opposite the reactive exhaust ports and the air-whirling blow ports and pass hermetically, transversely, longitudinally and coaxially through the vessel and the turbine sleeve walls. Inside the turbine sleeve in a mobile position is placed the engine turbine with its liquid-cooled rotor, hereinafter called rotor, with outgoing front and rear power-leading shafts in which are drilled the front and rear internally blind liquid openings connected with openings bored transversely and symmetrically at both ends, in this case in the inner end of the shaft there are /6/ six of them. In the rotor are drilled several pairs of diametrically, longitudinally and radially symmetrical openings, in this case /3/ three pairs or /6/ openings, which do not cross each other. Several pairs of turbine driving lifting plates channels, hereinafter called driving lifting plates channels, in this case /3/ pairs or /6/ channels, are made coaxially and through pairs of openings in the rotor between its two side faces. The driving lifting plates channels have parallel walls with sloping outer edges. In the rotor sections formed between adjacent pairs of driving lifting plates channels are made longitudinal liquid chambers passing through the rotor sections and cooling their walls. Inside the pairs of openings are located movable pipe turbine plates barneys, in this case /6/ six, hereinafter called barneys, with central pivot connecting springs, in this case /12/ twelve, at the two ends of the barneys. To the outer ends of springs are fixed saucer washers by means of a pivot.
Advantages and Innovations:
The engine offered here with its volume or power will be more compact, more economical, more powerful, more dynamical, with a smaller number of low-inertia parts, simple to produce, install and centre. Its main advantage is that according to its constructive plan a hermetical sealing system is worked out /spring-mechanical, gas-pneumatic and inertia system/ for rotating combustion and working chambers of the engine; also for spring-mechanical, gaspneumatic and inertia compensation of physical, mechanical friction wear.
The second big advantage of this engine is that its design allows its being equipped with necessary standard external devices according to eccentricity of flanges of the vessel as a result of which it can run as a conventional engine using only spark-ignition fuels or only thermal ignition ones. The engine offered here will be more economical, many times smaller in size andweight, more compact; it will also have a smaller number of low-inertia rotating parts with limited forward-backward movement and smaller weight, they will be high-tech in their make, assembly and fitting; as a result the engine will have a simple and more reliable construction and will be easy to operate, maintain and repair. When the engine is equipped with programmable logical controllers (PLC) controlling its work and the work of its turbo-compressor and at the same time with standard outer devices for sparkignition and thermo-ignition fuels the degree of preliminary thickening of air-fuel mixture or of air in its working chambers can be changed manually by the operator or automatically by PLC during work when necessary.
Stage of Development:
Under development/lab tested
IPs:
Patents granted

Partner sought

Type and Role of Partner Sought:
Type of partner sought - manufacture of engines for transport vehicles, turbines used in the energetics and turbo -compressors; technical cooperation; looking for financial resources.
Specific area of activity of the partner: Transport and energetics
Task to be performed: Prototype creation and performance testing.

Client

Type and Size of Client:
Industry SME <= 10
Already Engaged in Trans-National Cooperation:
No
Languages Spoken:
Bulgarian
English

Keywords

Technology Keywords:
02009005 Construcción de barcos
02009001 Diseño de vehículos
04002 Energy production, transmission and conversion
02009002 Hybrid and Electric Vehicles
02008 Infraestructura de transporte