Login| Sign Up| Help| Contact|

Patent Searching and Data


Matches 201 - 250 out of 407

Document Document Title
JP2013044455A
To provide an internal combustion engine capable of using any kinds of fuels and generates rotational force by using blast produced by explosion of the fuel.An internal combustion engine 100 includes an impeller unit 10, a combustion uni...  
JP2013011381A
To provide a power generating system capable of generating power without generating CO2 or harmful gas.The power generating system has a combustion cylinder into which plant dust made of plants is supplied and in which dust explosion is ...  
JP5047367B2  
JP5000101B2  
JP5002721B1
[Subject] The gas generator of operation which supplies gas of operation to the power plant which makes gas of operation the source of power is provided. [Means for Solution] A gas generator of the present invention of operation is a dev...  
JP4993442B2  
JPWO2010073951A1
急激な主駆動機の負荷変化に対して船内の停 電を防止することができる排熱回収システム の制御方法及び制御装置を提供する。船の主 駆動機にて発生した排ガスの一部をガス...  
JPWO2010073951A
A control method of an exhaust heat collection system and a control device which can prevent an inboard power failure to a rapid load change of the main drive machine are provided. In a control method of an exhaust heat collection system...  
JP4938903B1
[Subject] CO 2 -- provide the power generation system which can be generated without generating harmful gas. [Means for Solution] A combustion pipe which is made to supply vegetable particulates which used a plant as a granular material,...  
JP2012500926A
The subject of the present invention is a combustion turbine (1) for intermittent combustion with at least one combustion chamber (3) having inlet valves (2) and an ignition device (18), the at least one combustion chamber (3) having no ...  
JP2007010308A5  
JP2011185268A
To improve the durability of a pulse detonation tube.In one embodiment, a pulse detonation system (10) includes the pulse detonation tube (36) including a base tube (78) and a thermally protective layer (82) disposed adjacent to an inner...  
JP2011185133A
To enhance working efficiency while lowering peaks of combustion temperature and pressure of a pulse detonation engine.An engine contains at least one pulse detonation combustor 103 provided with a combustion chamber 106 and an outlet no...  
JP4757263B2  
JP2011522993A
The engine (I) has a fuel supplying unit for supplying fuel to a combustion chamber (7) from a flame tube (2), and including a transferring chamber (9) with variable volume delimited by a lateral wall (6) of the tube, a transversal movab...  
JP2011518286A
The engine (I) has an outer envelope (3) defining a peripheral annular space (4) along a side wall (5) of a fire tube (2) that allows flow of air from an air inlet of the engine. Parallel fixed flow guides (11-14) define flow channels in...  
JP2011517741T
A rotating type and a mechanical round trip slide shuttlecock air pump are made into a pulse drive boundary layer gas turbine and one on a single shaft. A shaft is provided with a slot and alignment arrangement of the shaft is carried ou...  
JP2011117448A
To provide a method and an apparatus for modulating thrust during a flight envelope of a multiple combustion chamber pulse detonation engine, using cross-combustion chamber detonation initiation.A plurality of detonation combustion chamb...  
JP2011517741A
A rotating type and a mechanical round trip slide shuttlecock air pump are made into a pulse drive boundary layer gas turbine and one on a single shaft. A shaft is provided with a slot and alignment arrangement of the shaft is carried ou...  
JP2011080448A
To solve such a problem that startup of operation of a combustor may be difficult, particularly, in a low temperature environment, in use of a pulse detonation engine/combustor.A power generation system includes: a compressor stage; a pr...  
JP2011069346A
To provide an engine deemed to increase efficiency by improving a rotary engine.A rotary shaft 4 connected to a generator is arranged to be rotatably supported inside of a cylindrical engine outer wall 1. A hexagonal pyramid-shaped combu...  
JP4618612B2  
JP2010281208A
To provide a system which allows for accurate engine timing when a rotary or a cylindrical valve is used to distribute an air/fuel mixture for combustion according to subsonic speed or supersonic speed.This engine timing input system 400...  
JP2010261438A
To provide a method for removing hot gas deposits (18) from a system (10) by pressure pulses. The method includes steps of: adjusting flow of mixture of detonation fluid (36) and oxidant (38) to an expansion chamber (30), and generating ...  
JP4569951B2  
JP2010533259A
This invention presents a compact, light, efficient and high power output rotary internal combustion engine utilizing the waste heat. The engine has a rotor rotatable within a housing, but has no piston. The rotor has a plurality of comb...  
JP2010223221A
To provide an engine which tries to improve a method to fire PDC (pulse detonation combustion) such that any resonance (resonation) frequency is detuned.The engine (100) includes a compressor stage (101), a plurality of pulse detonation ...  
JP4497469B2  
JP2010138875A
To prevent pressure of compressed air supplied to a diesel engine from an exhaust turbine supercharger from exceeding a prescribed pressure when an electric power demand is decreased. This exhaust energy collection device includes: an ex...  
JP4478824B2  
JP4471644B2  
JP4411050B2  
JP2009293618A
To reduce NOx discharged from a gas turbine.A turbine system 2 includes a first compressor 6 configured so as to compress a gaseous matter, a first combustor 10 for mixing the compressed gaseous matter 9 with a fuel 12 and combusting the...  
JP4350128B2  
JP4332396B2  
JP2009162097A
To solve a problem that there are increase of weight and increase of noise since a rocket engine or the like is used and it must be used after acceleration since flowing-in of air of a constant speed or more is required when a convention...  
JP4256820B2  
JP2008309025A
To provide an electric power generation system using exhaust gas with little fluctuation of output frequency of a generator even when the flow rate of exhaust gas supplied from an internal combustion engine fluctuates or load fluctuates....  
JP2008520877A5  
JP2008520877T5  
JP4152894B2  
JP2008530450A
The pulse-jet engine of the millimeter scale is equipped with the main part of an engine which has specified the combustion chamber, the fuel entrance, the inspiratory port, and the exhaust port. The fuel entrance is 配設 (ed) so that ...  
JP2008520877A
The wind air engine about all the power-driven machinery which belongs to the machine field and carries out fixed speed operation of a jitney bus track and a passenger car, a railroad train, a vessel, aviation power, etc. Into size, i. E...  
JP2008133791A
To start a gas turbine generating system with a small number of devices and by simple control, and to provide the gas turbine generating system for improving re-use of energy of exhaust gas.As the gas turbine generating system driven by ...  
JP4032647B2  
JP2007535636A
[Subject] Conquest or the pulse-jet engine considerably reduced at least is offered for the disadvantageous point relevant to a well-known jet engine. [Solution means] They are whether it is the pulse-jet engine equipped with the 1/4-wav...  
JP3994284B2  
JP3981743B2  
JP3952202B2
To provide a pulse detonation engine of an air suction type that uses oxygen in open air for an oxidizer, in which high pressure and high density are achieved in a mixed gas charging process to a combustor. An outlet valve 20 that can be...  
JP3943094B2
To provide a pulse combustion device having several combustors. The pulse combustion device has a plurality of combustors having a body part 28 on the upstream side and a nozzle 30 on the downstream side. A plenum 50 is formed on an oute...  

Matches 201 - 250 out of 407