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Patent Searching and Data


Matches 151 - 200 out of 420

Document Document Title
WO/1987/004494A1
A compound engine comprises a positive displacement engine (100), such as a reciprocating or rotary piston diesel engine, which is linked to a turbine/turbocompressor set in the form of a gas turbine engine (102) with a free power turbin...  
WO/1987/004493A1
An operating cycle for a turbocompounded 2-stroke piston engine comprises a compression stroke, shown as B-A-G on the indicator diagram and an expansion stroke G-K-L-B. The expansion stroke expands the combustion gases to a pressure PB w...  
WO/1987/004492A1
A prime mover comprises a positive displacement engine (100), such as a reciprocating or rotary piston engine, which is linked to a turbine/turbocompressor set, such as the gas turbine engine (102). The exhaust gases of the positive disp...  
WO/1987/004491A1
The cylinder head (401) of a turbocompounded 2-stroke piston engine incorporates, for each cylinder (400), an indirect combustion chamber (402), which is connected to the cylinder clearance volume (413) by a passage (412). The indirect c...  
WO/1986/004956A1
The drive unit has intermittent combustion and at least two round discs (2a, 2b) which are installed rotating and concentric to a driven shaft (3) in a housing (1). Each disc (2a, 2b) includes at least one partial combustion chamber (5a,...  
WO/1983/001277A1
A power plant for operation substantially on an Atkinson type cycle comprising a compressor (10) for compressing a gaseous medium. A positive displacement mechanism (30) is provided for receiving the compressed gaseous medium from the co...  
WO/1983/000190A1
A method in operating an internal combustion engine (13) with an air compressor (10) driven thereby, which absorbs the total output of the engine. A first and a second part (15 and 16, respectively) of the pressurized air from the compre...  
WO/1982/003422A1
Method for transforming reaction heat into mechanical energy, wherein a plurality of bodies participating to the reaction are introduced in a reaction chamber where they are reacted between each other. The reaction heat of chemical react...  
WO/1982/001743A1
A hybrid gas turbine tow-phase internal combustion engine comprising a tuborotor (1) having blades (11) which extend radially from and rotate about a fixed axis. The turborotor is enclosed coaxially by an annular housing (2) which togeth...  
WO/1982/001744A1
This gas turbine apparatus contemplates to drive a turbine by compressing a combustible gas mixture with a reciprocating piston, introducing it into a combustion chamber, and igniting and exploding the gas in the combustion chamber. A wh...  
WO/1981/002912A1
A method of performing work and an apparatus for performing the method utilizing the following thermodynamic cycle. Ambient air is isothermally compressed to a predetermined degree (A-B) and then heat is added to the air at constant pres...  
WO/1981/000019A1
A machine with free pistons comprising a frame, an inner moving assembly comprising a central cross bar and translatingly guided so as to effect a reciprocating motion along the frame axis and an outer moving assembly comprising two oute...  
WO/1980/002444A1
Explosion turbine comprising a centrifugal or axial compressor (1) compressing the air across an induction distributor (8) in one or a plurality of combustion chambers (9) closed by an expension distributor (10); at the closing of the in...  
WO/1980/000990A1
Internal combustion engine combinating a two-cycle combustion chamber with a gas turbine. This invention makes it possible to overcome troubles caused by incomplete combustion of fuel in a known cylinder type engine and troubles caused b...  
JP2020045903A
[Subject] It is an engine using a piston and an engine which can control still more easily timing which supplies combustion gas, combustor efficiency, etc. is called for in an engine of a type supplied to a turbine etc. by making combust...  
JP6630024B2  
JP6615347B2  
JP6611653B2  
JPWO2018190156A1
An engine (5) which has a gas supply unit (10) which supplies combustion gas for a drive in connection with a both-way straight-line motion of a piston (12) is provided. The 1st combustion chamber (31) where a gas supply unit (10) was pr...  
JP2019508631A
The object of the present invention is to provide a system for enforcing a method and a method for reducing a reciprocation combustion engine at the time of power generation, and a fault of a gas turbine. The present invention is based o...  
JP6486668B2  
JP2019002393A
To solve such the social problems in which a number of inefficient internal combustion engines that use a large amount of fossil fuel are used despite that global warming becomes a serious social problem, existing internal combustion eng...  
JP2018535356A
[Subject] The object of the present invention is to provide a method and a system for enforcing a method of reducing a fault of a reciprocating combustion engine when generating power, and a gas turbine. [Solution] From a plurality of co...  
JP2018521259A
A fluid free passage is carried out including wings with a turbine constituted so that it might rotate around the axis of rotation, and a turbine, A flow guidance element constituted so that a turbine may be rotated around the axis of ro...  
JP2018521261A
The present invention mainly relates to a turbine engine combustion chamber module (4) provided with at least one constant-volume combustion chamber (7). The module is further provided with a pre-combustion room (6) which can generate hi...  
JP2018508694A
The present invention relates to a constant-volume combustion system (3) for a turbine engine. A plurality of combustion chambers (11*14) where the above-mentioned system was regularly distributed around an axis (AX) of a longitudinal di...  
JP2018031067A
To provide a generator of a mixture gas containing pressurized water vapor and HHO gas, to which attachment devices such as a liquid-gas separator, a flashback arrester or the like are conveniently connected, and by which a risk of leaka...  
JP2016107665A5  
JP6246988B2  
JPWO2017065285A1
An engine (10) which has a gas turbine unit and a plurality of combustion units (80) which supply combustion gas (51) to a gas turbine unit is provided. A combustion unit (80) moves the 1st wall surface (81a) that constitutes a part of c...  
JP6238997B2  
JP6220876B2  
JP2017184457A
To provide a thermoacoustic power generation system capable of continuing operation even if the temperature changes.A thermoacoustic power generation system 1 includes a thermoacoustic engine 2 having an annular loop tube 10 in which wor...  
JP2017180920A
To preferably suppress a decline in temperature difference between a heater and a cooler by an engine, amplify an acoustic wave appropriately by an engine, and to be preferably capable of generating electrical power by a power generator ...  
JP6207617B2  
JP6153163B2  
JP6132979B2  
JPWO2015159956A1
An engine (10) which spouts combustion gas as driving force is provided. A fueling way (13) where this engine (10) mixes and supplies fuel and air to a combustion chamber (11) and a combustion chamber (11), It has an igniter (42) which l...  
JP6103624B2  
JP2016538452A
Shell (11) which is a coupling guard (1) for a rotating member (15), and encloses a rotating member (15), An exhaust port (13) for carrying out discharge of a filling pipe (12) and coolant gas for pouring in coolant gas to plenum (25) ar...  
JP6038885B2  
JP6005061B2  
JP2016107665A
To provide a ship propulsion device having a simple structure where the number of friction parts is limited in a main driving mechanism, limited in generation of water contamination and noise, and easily handled.The ship propulsion devic...  
JP2016503482A
A pressure gain burner includes a detonation chamber, a pre-combustion chamber, an oxidizer whirlpool generator, an expansion * deviation (E*D) nozzle, and an ignition source. A detonation chamber has an upper inhalation end and a downst...  
JP2015531456A
The detonation engine (100) can work in a cylindrical shape detonation field (205) by carrying out detonation of the fuel-air mixture of an oxidizer to fuel. The detonation engine can have the 1st and 2nd entrances (135, 140) that have f...  
JP2015528082A
The present invention is provided with a compressed gas inhalation valve (22) with capability to take an open position and a closed position which intercepts an air intake of compressed gas into a combustion chamber, It is related with a...  
JP5734706B2  
JP2015031215A
To provide a reheating type ammonia gas turbine capable of curbing emission of unburnt ammonia and NOas much as possible.A reheating type ammonia gas turbine I comprises: a gas turbine 3 which is driven by combustion gas obtained by supp...  
JP5604075B2  
JP5576683B2  

Matches 151 - 200 out of 420