| Document |
Document Title |
|
WO/2018/195631A1 |
The present invention relates to a combined cycle heat engine comprised of a unit that operates on the Otto cycle and is interconnected and integrated with another unit that operates on a binary cycle of three isobaric processes and four...
|
|
WO/2018/195629A1 |
The present invention relates to a combined cycle heat engine comprised of a unit that operates on the Diesel cycle and is interconnected and integrated with another unit that operates on a binary cycle of three isobaric processes and fo...
|
|
WO/2018/195626A1 |
The present invention relates to a heat engine containing a polytropic-process polytropic expansion heating chamber (22), a three-way proportional control valve (23), two turbine rotors (24) and (25) and two compressor rotors (26) and (2...
|
|
WO/2018/195632A1 |
The present invention relates to a combined cycle heat engine comprised of a unit that operates on the Otto cycle and is interconnected and integrated with another unit that operates on a binary cycle of three isothermal processes and fo...
|
|
WO/2018/195621A1 |
The present invention relates to a heat engine containing an isobaric expansion heating chamber (22), a three-way proportional control valve (23), two turbine rotors (24) and (25) and two compressor rotors (26) and (27), all connected to...
|
|
WO/2018/195628A1 |
The present invention relates to a turbine-type combined cycle heat engine comprised of a unit that operates on the Brayton cycle and is interconnected and integrated with another unit that operates on a binary cycle of three isothermal ...
|
|
WO/2018/195622A1 |
The present invention relates to a heat engine containing an isothermal expansion heating chamber (22), a three-way proportional control valve (23), two turbine rotors (24) and (25) and two compressor rotors (26) and (27), all connected ...
|
|
WO/2018/195633A1 |
The present invention relates to a combined cycle heat engine comprised of a unit that operates on the Atkinson or Miller cycle and is interconnected and integrated with another unit that operates on a binary cycle of three isobaric proc...
|
|
WO/2018/184078A2 |
Tesla's three-phase hybrid rotary internal combustion engine is based on theoretical essentials of Tesla's concept of internal combustion engines and the principles of transforming kinetic fluid energy into mechanical work applied on Tes...
|
|
WO/2018/182272A1 |
The purpose of the present invention is to minimize fluid leakage and pressure leakage, and a turbine apparatus of the present invention comprises: a turbine (510) rotating together with a turbine shaft (513) in response to an inflow of ...
|
|
WO/2018/131167A1 |
The present invention provides a turbine wheel comprising a plurality of long blades and a plurality of short blades, wherein the trailing edges of the short blades are positioned farther upstream than are the trailing edges of the long ...
|
|
WO/2018/127445A1 |
A reverse compression cycle machine (M) comprising an evaporator (9), a compressor (1) and a condenser (3) arranged in series along a path of a working fluid in the machine (M), further comprising a boundary layer turbine (7) placed betw...
|
|
WO/2018/112530A1 |
A turbine rotor assembly including a unitary body including at least one inlet for inlet of a fluid into the rotor assembly and a plurality of flow channels extending through the unitary body and terminating in an outlet portion, the at ...
|
|
WO/2018/111585A1 |
A wellbore pump (100) that includes a pump housing (114), a pump stage (126) positioned within the pump housing (114), the pump stage (126) including a stationary diffuser (112a, 112b) and a rotating impeller (118) positioned within the ...
|
|
WO/2018/106539A1 |
A separation assembly comprises a housing, a jet that expels a fluid within the housing, and a turbine positioned within the housing. The fluid causes the turbine to rotate about a center rotational axis within the housing. The turbine c...
|
|
WO/2018/094444A1 |
This disclosure relates to a fluid flow machine, and a rotor therefore. In one aspect, the rotor contains internal flow channels for a flow medium to travel through, which does work on or extracts work from a fluid. Examples of fluid flo...
|
|
WO/2018/094524A1 |
A rotary manifold for a rotor assembly of a cohesion-type drive includes a manifold body extending along a drive axis for rotation thereabout, a first ductwork internal the body for fluid communication with a plurality of first chambers ...
|
|
WO/2018/078671A1 |
The present invention provides a power generation device, a generator, a power generation method, and an electrical power generation method, with which power can be generated efficiently without deterioration over time due to friction. T...
|
|
WO/2018/076050A1 |
A multi-stage axial turbine (typically between 4 and 10 stages) designed to operate more efficiently with partial admission of low temperature steam in each stage except the last one or two stages. Each stage of the subject turbine opera...
|
|
WO/2018/074312A1 |
Provided is a method for bonding dissimilar metals to each other, the method comprising: dissimilar metal layer-forming steps (P2), (P3), (P4) for supplying, on the surface of a first material to be bonded that is formed of a first metal...
|
|
WO/2018/065840A1 |
The present invention relates to an assembly of turbines, comprising: a first counter rotating turbine (2) and a second counter rotating turbine (3); a first group of gears (13) and a second group of gears (14) arranged on opposite sides...
|
|
WO/2018/054811A1 |
The invention relates to an assembly (1) for feeding an additional mass flow into a main mass flow, wherein the main mass flow flows along an axis of rotation, the feed and the axis of rotation being inclined in relation to one another.
|
|
WO/2018/047018A2 |
A boundary layer turbomachine can include a housing (10) defining an interior space and having an inlet opening and an outlet opening to facilitate movement of a fluid through the housing (10). The boundary layer turbomachine can also in...
|
|
WO/2018/045116A1 |
An airfoil body may include a plurality of tubercles along a leading edge of the airfoil body and a plurality of crenulations along a trailing edge of the airfoil body, wherein at least one of a position, a size, and a shape of the plura...
|
|
WO/2018/043071A1 |
Provided is an air turbine drive spindle configured so that an increase in pressure within a through-hole can be prevented. This spindle is provided with a rotating shaft (1) and an outer peripheral member (housing assembly (2), cover (5...
|
|
WO/2018/009995A1 |
The present invention describes a pressure reducing system with energy re-use. More specifically, the present invention describes a prime mover (1) which is associated with a line of industrial fluids and is capable of causing a pressure...
|
|
WO/2018/002748A1 |
The present invention refers to a method for the assembly of a counter-rotating radial turbine, comprising: preparing a central case (9); pre-assembling a first turbine unit (33') and a second turbine unit (33"), each comprising: a half-...
|
|
WO/2017/217561A1 |
Disclosed is an air controller comprising: a housing having an inlet port through which air is introduced and a discharge port through which the introduced air is discharged; at least one disc laminated at a predetermined interval inside...
|
|
WO/2017/174828A1 |
The invention relates to a device for joining a modular blade, the joint being formed by a plurality of bolts (8) that are secured between inserts (3 and 4) housed in the composite material of two modules (1 and 2) to be joined. The devi...
|
|
WO/2017/168335A1 |
The present invention concerns a method for the construction of bladed discs for radial turbomachines, comprising: preparing a disc (6, 14) provided with a front face (7); preparing a plurality of reinforcement rings (23) with different ...
|
|
WO/2017/168334A1 |
The present invention relates to a radial turbomachine with axial thrust compensation, comprising: a fixed casing (3); a plurality of main concentric bladed rings (9',9",9"',9"") arranged in the fixed casing (3) around a central axis (X-...
|
|
WO/2017/171678A1 |
A turbine assembly for electric generation comprising a first rotor which is rotatable about a rotation axis by the action of a pressurized fluid and one or more magnets (13) arranged on the first rotor to rotate together therewith furth...
|
|
WO/2017/165631A1 |
This invention is directed to a centrifuge rotor, such as for use in a disc nozzle centrifuge, having a bowl including an improved positioning and orientation of discharge nozzles for facilitating tangential flow of fluid discharged ther...
|
|
WO/2017/162964A1 |
The invention relates to an aircraft turbomachine comprising at least one unducted propeller having a plurality of blades (6), each blade (6) comprising: a blade body (8) made of a composite material with a fibrous reinforcement densifie...
|
|
WO/2017/149303A1 |
An automotive powertrain (100) for driving an automobile is disclosed. In particular, an automotive powertrain (100) comprising: an engine (110) with a crankshaft (112); and an electric supercharger (120) for boosting the output torque o...
|
|
WO/2017/138035A1 |
A gas expander 1 is provided with: a casing 20 having formed therein a swirl chamber 21 through which process gas G flows; a turbine wheel 10 accommodated within the casing 20 and rotationally driven by the process gas G which has been e...
|
|
WO/2017/134481A1 |
Air is compressed by an electric motor in stages of Archimedes scroll spirals. Condensed air moisture is collected as potable water at the output of each stage of air compression. Heat of compression is used to produce hot water. The dri...
|
|
WO/2017/133294A1 |
A tapering exponential spiral for a gas expander (503) for work extraction or air cooling is used. This tapering exponential spiral could also be used for a gas compressor (501) to increase the pressure and temperature of air. The compre...
|
|
WO/2017/104916A1 |
The present invention relates to a reaction-type steam turbine. More specifically, the present invention relates to a reaction-type steam turbine that has guide blades mounted on a turbine shaft located between disk blades and a steam in...
|
|
WO/2017/099698A1 |
The invention relates to power engineering and motor engineering and can be used in electricity generating plants and serve as a propulsion unit in vehicles. The basis of the present turbine/engine is that a cold pressurized working flui...
|
|
WO/2017/090963A1 |
The present invention relates to a small-scale combined heat and power generator using a steam injector which employs a small-scale heat source and, more particularly, to a small-scale combined heat and power generator comprising a rotat...
|
|
WO/2017/054068A1 |
A utility model of solar energy generator with a parabolic trough collector and a turbine with 1-100 KW power associates a solar concentrator collector with parabolic troughs with the hybrid Tesla-Pelton wheel turbine or with the Tesla t...
|
|
WO/2017/046385A1 |
The invention relates to a spindle head (1) and a machine-tool, having a clutch (26) that is arranged between a first drive shaft (6) of the spindle head (1) and a second drive shaft (9) of a drive (10), wherein the clutch (26) comprises...
|
|
WO/2017/048149A1 |
The invention relates to the energy sector. A device for converting the energy of a drop in the pressure of a gaseous working fluid comprises a housing, a consumer of the mechanical energy generated, and an expansion turbine with a blade...
|
|
WO/2017/041182A1 |
A shear flow turbomachinery device includes a housing having housing walls defining a cavity, a shaft extending into the cavity though a shaft opening in the housing wall at an end of the cavity, a rotor coupled to the shaft within the c...
|
|
WO/2017/035657A1 |
A pneumatic motor assembly that includes a pneumatic motor, which is driven by a compressed gas. The pneumatic motor assembly has a magnet assembly that magnetically couples the pneumatic motor assembly to an implement. After having bein...
|
|
WO/2017/029131A1 |
A computer implemented method (100) for the prediction of the surge point of a compressor (14) comprises the following steps: - generating (110) a plurality of meshes: - a compressor inlet mesh (220), - at least a compressor rotor stage ...
|
|
WO/2017/021067A1 |
The invention relates to a turbomachine, in particular a steam turbine (2) having an overload inflow region (17) which is designed for the inflow of overload steam, wherein said overload steam is prevented from impinging on the rotor sur...
|
|
WO/2017/022400A1 |
An air turbine drive spindle (100) with which it is possible to suppress a deterioration in painting quality by suppressing the inflow of a driving gas into a through-hole in a rotating shaft is provided with a housing and a rotating sha...
|
|
WO/2017/023155A1 |
The invention relates to a spiral turbine designed to use the micro-forces from the drag caused by a fluid on the walls of the conduits thereof, i.e. the shear stress through the boundary layer. Unlike traditional turbines with various n...
|
