| 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...
|
