WO2012117365A1 - Fluid machine - Google Patents
Fluid machine Download PDFInfo
- Publication number
- WO2012117365A1 WO2012117365A1 PCT/IB2012/050963 IB2012050963W WO2012117365A1 WO 2012117365 A1 WO2012117365 A1 WO 2012117365A1 IB 2012050963 W IB2012050963 W IB 2012050963W WO 2012117365 A1 WO2012117365 A1 WO 2012117365A1
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- WO
- WIPO (PCT)
- Prior art keywords
- blade wheel
- impeller
- fluid
- fluid machine
- extra blade
- Prior art date
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/08—Adaptations for driving, or combinations with, pumps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
- F03B3/02—Machines or engines of reaction type; Parts or details peculiar thereto with radial flow at high-pressure side and axial flow at low-pressure side of rotors, e.g. Francis turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
- F03B—MACHINES OR ENGINES FOR LIQUIDS
- F03B3/00—Machines or engines of reaction type; Parts or details peculiar thereto
- F03B3/04—Machines or engines of reaction type; Parts or details peculiar thereto with substantially axial flow throughout rotors, e.g. propeller turbines
- F03B3/06—Machines or engines of reaction type; Parts or details peculiar thereto with substantially axial flow throughout rotors, e.g. propeller turbines with adjustable blades, e.g. Kaplan turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2220/00—Application
- F05B2220/60—Application making use of surplus or waste energy
- F05B2220/602—Application making use of surplus or waste energy with energy recovery turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2220/00—Application
- F05B2220/60—Application making use of surplus or waste energy
- F05B2220/604—Application making use of surplus or waste energy for domestic central heating or production of electricity
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/20—Rotors
- F05B2240/33—Shrouds which are part of or which are rotating with the rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/60—Application making use of surplus or waste energy
- F05D2220/62—Application making use of surplus or waste energy with energy recovery turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/60—Application making use of surplus or waste energy
- F05D2220/64—Application making use of surplus or waste energy for domestic central heating or production of electricity
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02B—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS, e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USER APPLICATIONS
- Y02B10/00—Integration of renewable energy sources in buildings
- Y02B10/50—Hydropower in dwellings
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E10/00—Energy generation through renewable energy sources
- Y02E10/20—Hydro energy
Definitions
- the invention relates to a fluid machine having an impeller with a plurality of blades and including a fluid inlet room and a fluid outlet room.
- a whirling motion also called vortex
- the whirling motion consisting of a linear and rotational component is caused by rotation of the impeller blade wheel.
- This phenomena is common to the impeller of a turbine converting the kinetic or pressure water energy to mechanical energy as well as to, for example, a dynamic machine with a blade wheel such as turbo-compressor which compresses gas flowing through the impeller.
- the whirling motion of the fluid may also have an undesired effect, for example with a jet engine aircraft, where it causes a declination of the exhaust fumes stream from the aircraft longitudinal axis behind the outlet tube exit plane due to a lateral force component of the vortex, what may cause a reduction of the total axial effective engine thrust.
- US 5261787 describes a device for directing water stream behind a turbine impeller by means of a cone that may be even forcibly rotated in order to reduce water surges and vibration of the turbine.
- US 4175640 discloses a system for internal mixing of hot primary exhaust flow with cool fan flow for reducing jet noise in a turbofan engine.
- Another solutions for directing the exhaust flow used frequently with the jet engines represents a system of fixed blades placed in fan air passageway behind the fan impeller.
- the fixed blades shall avoid rotational motion of the air behind the fan impeller and enable to use the axial air flow for directing the nozzle outlet fumes straight forward to avoid the undesired divergence of the exhaust fumes stream.
- the primary object of the invention is to provide a fluid machine comprising means for exploiting the rotational energy of the whirling motion of the fluid generated behind the impeller.
- Another object of the invention is to use such means for directing the fluid flow behind the impeller.
- the object of this invention can be achieved by a fluid machine having an impeller with a plurality of blades and including a fluid inlet room and a fluid outlet room where an extra blade wheel rotatably mounted independent of the rotation of the impeller is located on the downstream side of the impeller and this extra blade wheel is associated with a device for conversion of the blade wheel kinetic energy into the electric or pressure energy.
- the extra blade wheel is located at the distance equal to 0.2 up to 2 multiple of the outside diameter of the impeller.
- the position of blades of the extra blade wheel with respect to the fluid stream is controlled by an adjusting mechanism.
- the device for conversion of the kinetic energy is an electric generator or a hydraulic pump.
- the impeller is a fan of an air bypass turbojet engine and the blade of the extra blade wheel are located in the air bypass channel.
- the extra blade wheel comprises a hub carrying a rotor of an electric generator and rotatably mounted on a hollow journal fixed to the engine body and including a stator of the electric generator.
- the impeller is a runner wheel of a water turbine.
- the outer ends of the blades of the extra blade wheel are attached to a watertight sealed ring for receiving a rotor of an electric generator carried in bearings incorporated in a turbine clothing together with a stator of the electric generator.
- the extra blade wheel arranged downstream the impeller enables to acquire additional usable source of kinetic energy, which is susceptible to conversion by conventional methods into electric or pressure energy.
- Another advantage of the fluid engine according to the invention resides in the possibility to set optimal characteristics of the fluid flow downstream the impeller. Still another advantage is that the flow characteristics may be adjusted interactively by application of a blade adjusting mechanism.
- Fig. 1 is a cross-sectional view of a bypass turbojet engine
- Fig. 2 is a cross-sectional view of the bypass turbojet engine taken along line A-A of Fig. 1;
- Fig. 3 is a cross-sectional perspective view of the bypass turbojet engine
- Fig. 4 is cross-sectional view of a horizontally situated axial flow turbine
- Fig. 5 is a cross-sectional view of vertically situated Kaplan turbine with an impeller and without a guide wheel;
- Fig. 6 is a partial cross-sectional view of the extra blade wheel taken along line B-B of Fig. 5.
- a bypass turbojet engine in a simple embodiment with one aerodynamically formed shaft 1 and one exhaust fluid driven turbine 15 is shown in a cross-sectional front view in Fig. 1 and in a perspective cross-sectional view in Fig. 3.
- the shaft 15 is rotatably mounted in an engine body 5 and its front part bears an impeller - in this example a fan 12 whose blades extend by their outer ends close to a clothing wall 4 surrounding the engine body 5. Downstream the fan, the shaft further carries blades of an axial multistage compressor 14.
- Combustion chambers 52 are disposed along the perimeter of the medium part of the shaft 1 while the rear engine part includes a blades of a turbine 15 also carried by the shaft 1 and followed by the outlet cone defining an annular space of an exit nozzle 51.
- An annular air bypass channel 41 is formed between the inner wall of the clothing 4 and the engine body 5. As shown in Fig. 2 and 3, blades of an extra blade wheel 2 extend into the bypass channel 41 at a distance of approximately 0.25 multiples of the diameter of the fan 12.
- a hub 21 of the extra blade wheel 2 is mounted on a bearing 32 fitted to a hollow journal 31, which is secured to the engine body 5.
- the hub 21 includes a rotor assembly of an electric generator and the hollow shaft 31 includes a corresponding stator assembly of this electric generator.
- a portion of air compressed by the fan 12 is directed into the axial compressor stage while the other portion of air flows through the bypass channel 41 so that in the exit nozzle both streams are mixed to generate the engine thrust.
- the blades of the extra blade wheel 2 are situated parallel to the engine longitudinal axis and are activated by a radial or rotational component of the stream vortex generated downstream the fan 12.
- the mechanical energy of the rotating extra blade wheel 2 is converted by the generator to electrical energy which may be used for feeding various electrical appliances of the engine powered machine, for example an aircraft.
- the above embodiment of the invention is described by way of example only and do not exclude another positioning of the blade wheel 2, for example in the area of the engine exit nozzle 51.
- the blades of the extra blade wheel may have an aerodynamic shape and further associated with a mechanism for adjusting their position with respect to the direction of the fluid stream.
- FIG. 4 Another example of the application of an extra blade wheel to a fluid engine in the form of water turbine is illustrated in a simplified view in absence of a guide wheel in Fig. 4.
- a horizontally situated impeller - water S- turbine runner wheel 61 coupled with an electric generator 62 is situated within the turbine clothing 8 in the entrance tube with the water flow direction denoted by arrow 82.
- an extra blade wheel 7 Downstream the runner wheel 61, an extra blade wheel 7 is located at a distance equal to a diameter of the runner wheel 61.
- the extra blade wheel 7 is mounted on a common shaft 75 together with an auxiliary generator 76.
- the distance between the runner wheel 61 and the extra blade wheel 7 is dependent inter alia on the density and the velocity of the liquid, cross-sections ratio etc.
- the extra blade wheel 7 for driving of the auxiliary generator 76 is actuated by a rotational power component of the vortex generated by the runner wheel 61.
- FIG. 5 and Fig. 6 A more detailed view of another, in this case vertical arrangement of a water turbine of a Kaplan turbine type is shown in Fig. 5 and Fig. 6.
- the turbine is also illustrated in a simplified form without a guide wheel.
- the impeller - runner wheel 61 of the turbine is born by a shaft 6 arranged in a vertical position inside a turbine clothing 8.
- am extra blade wheel 7 is situated under the turbine.
- the blades of the extra blade wheel are embedded by their outer ends in a peripheral ring 72 and by their inner ends in a central ring 78.
- the peripheral ring 72 is carried in a tapered roller bearing 73.
- a winding assembly of a rotor 71 of a generator is arranged along the perimeter of the peripheral ring 72.
- the winding of a corresponding stator 81 of the generator is built in opposite to it, in the turbine clothing 8.
- the generator is watertight sealed towards the internal room of the clothing 8 by a package 74.
- the blades are mounted on pivots 77 fixed in the peripheral ring 72 and are associated with a non-illustrated adjusting mechanism.
- the extra blade wheel 7 powering the rotor 71 of the generator is actuated by rotational force component of the vortex generated by the runner wheel 61.
- the blade adjusting mechanism enables optimal regulation of the speed of the extra blade wheel 7 and simultaneously adjusting the characteristics of water flow in the draft tube downstream the extra blade wheel 7.
- the foregoing examples of the embodiment of the invention do not limit the described process of conversion of the extra blade wheel kinetic energy to electric energy.
- the electric generator may be substituted by another device for conversion of the blade wheel kinetic energy.
- a hydraulic pump instead of an auxiliary generator 76 in Fig. 4 a hydraulic pump may be utilized as a source of pressure energy.
- the cross-sectional area of the clothing in the area of blade wheel may be enlarged to eliminate the change in the flow rate in the blade wheel due to a passive elements of the blade wheel supporting structure, etc.
- the extra blade wheel structure according to the invention may be applied to all fluid machines with a impeller actuated by kinetic or pressure fluid energy, such as water or gas turbines or fluid machines generating the kinetic energy by means of a power unit such blowers, suction or pressure fans etc.
- a impeller actuated by kinetic or pressure fluid energy such as water or gas turbines or fluid machines generating the kinetic energy by means of a power unit such blowers, suction or pressure fans etc.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
A fluid machine having an impeller (12; 61) with a plurality of blades and including a fluid inlet room and a fluid outlet room wherein an extra blade wheel (2; 7) rotatably mounted independent of the rotation of the impeller (12; 61) is located on the downstream side of the impeller (12; 61) and this extra blade wheel (2; 7) is associated with a device for conversion of the blade wheel kinetic energy into electric or pressure energy. T he impeller is a fan (12) of an air bypass turbojet engine or a runner wheel (61) of a water turbine and the device for conversion of the kinetic energy is an electric generator or a hydraulic pump.
Description
The invention relates to a fluid machine
having an impeller with a plurality of blades and
including a fluid inlet room and a fluid outlet room.
One of characteristic features of all
fluid machines with an impeller and fluid inlet and
outlet room is a whirling motion, also called vortex,
of the fluid such as liquid, air or another gas in the
outlet room of the machine and continuing downstream
the outlet tube exit plane. The whirling motion
consisting of a linear and rotational component is
caused by rotation of the impeller blade wheel. This
phenomena is common to the impeller of a turbine
converting the kinetic or pressure water energy to
mechanical energy as well as to, for example, a
dynamic machine with a blade wheel such as
turbo-compressor which compresses gas flowing through
the impeller. The whirling motion of the fluid may
also have an undesired effect, for example with a jet
engine aircraft, where it causes a declination of the
exhaust fumes stream from the aircraft longitudinal
axis behind the outlet tube exit plane due to a
lateral force component of the vortex, what may cause a
reduction of the total axial effective engine thrust.
In the prior art certain mechanisms for
directing the fluid stream are disclosed. For example
US 5261787 describes a device for directing water
stream behind a turbine impeller by means of a cone that
may be even forcibly rotated in order to reduce water
surges and vibration of the turbine.
US 4175640 discloses a system for
internal mixing of hot primary exhaust flow with cool
fan flow for reducing jet noise in a turbofan engine.
Another solutions for directing the
exhaust flow used frequently with the jet engines
represents a system of fixed blades placed in fan air
passageway behind the fan impeller. The fixed blades
shall avoid rotational motion of the air behind the
fan impeller and enable to use the axial air flow for
directing the nozzle outlet fumes straight forward to
avoid the undesired divergence of the exhaust fumes stream.
The primary object of the invention
is to provide a fluid machine comprising means
for exploiting the rotational energy of the
whirling motion of the fluid generated behind the impeller.
Another object of the invention is
to use such means for directing the fluid flow
behind the impeller.
The object of this invention can be
achieved by a fluid machine having an impeller
with a plurality of blades and including a fluid
inlet room and a fluid outlet room where an extra
blade wheel rotatably mounted independent of the
rotation of the impeller is located on the
downstream side of the impeller and this extra blade
wheel is associated with a device for conversion
of the blade wheel kinetic energy into the electric
or pressure energy.
Hereinafter, other advantageous
embodiments of the invention are described that
develop or specify in more details its essential
features but without limiting the scope of the invention.
The extra blade wheel is located at
the distance equal to 0.2 up to 2 multiple of
the outside diameter of the impeller.
The position of blades of the extra
blade wheel with respect to the fluid stream is
controlled by an adjusting mechanism.
The device for conversion of the
kinetic energy is an electric generator or a
hydraulic pump.
The impeller is a fan of an air
bypass turbojet engine and the blade of the
extra blade wheel are located in the air bypass channel.
The extra blade wheel comprises a
hub carrying a rotor of an electric generator
and rotatably mounted on a hollow journal fixed
to the engine body and including a stator of the
electric generator.
The impeller is a runner wheel of a
water turbine.
The outer ends of the blades of the
extra blade wheel are attached to a watertight
sealed ring for receiving a rotor of an electric
generator carried in bearings incorporated in a
turbine clothing together with a stator of the
electric generator.
The extra blade wheel arranged
downstream the impeller enables to acquire
additional usable source of kinetic energy, which
is susceptible to conversion by conventional methods
into electric or pressure energy. Another
advantage of the fluid engine according to the
invention resides in the possibility to set
optimal characteristics of the fluid flow
downstream the impeller. Still another advantage is
that the flow characteristics may be adjusted
interactively by application of a blade
adjusting mechanism.
Certain of the possible embodiments of
the invention are further described by way of examples
with reference to the related schematic drawings. In
the drawings:
Fig. 1 is a cross-sectional view of a
bypass turbojet engine;
Fig. 2 is a cross-sectional view of the
bypass turbojet engine taken along line A-A of Fig. 1;
Fig. 3 is a cross-sectional perspective
view of the bypass turbojet engine;
Fig. 4 is cross-sectional view of a
horizontally situated axial flow turbine;
Fig. 5 is a cross-sectional view of
vertically situated Kaplan turbine with an impeller
and without a guide wheel;
Fig. 6 is a partial cross-sectional
view of the extra blade wheel taken along line B-B of
Fig. 5.
The following examples represent
various embodiments of the fluid machine according to
the invention, whereby the identical or nearly
identical components as for their function and purpose
may bear the same referring numerals.
A bypass turbojet engine in a simple
embodiment with one aerodynamically formed shaft 1 and
one exhaust fluid driven turbine 15 is shown in a
cross-sectional front view in Fig. 1 and in a
perspective cross-sectional view in Fig. 3. The shaft
15 is rotatably mounted in an engine body 5 and its
front part bears an impeller - in this example a fan 12
whose blades extend by their outer ends close to a
clothing wall 4 surrounding the engine body 5.
Downstream the fan, the shaft further carries blades of
an axial multistage compressor 14. Combustion chambers
52 are disposed along the perimeter of the medium part
of the shaft 1 while the rear engine part includes a
blades of a turbine 15 also carried by the shaft 1 and
followed by the outlet cone defining an annular space
of an exit nozzle 51. An annular air bypass channel 41
is formed between the inner wall of the clothing 4 and
the engine body 5. As shown in Fig. 2 and 3, blades of
an extra blade wheel 2 extend into the bypass channel
41 at a distance of approximately 0.25 multiples of the
diameter of the fan 12. A hub 21 of the extra blade
wheel 2 is mounted on a bearing 32 fitted to a hollow
journal 31, which is secured to the engine body 5. The
hub 21 includes a rotor assembly of an electric
generator and the hollow shaft 31 includes a
corresponding stator assembly of this electric generator.
A portion of air compressed by the fan
12 is directed into the axial compressor stage while
the other portion of air flows through the bypass
channel 41 so that in the exit nozzle both streams are
mixed to generate the engine thrust. The blades of the
extra blade wheel 2 are situated parallel to the
engine longitudinal axis and are activated by a radial
or rotational component of the stream vortex generated
downstream the fan 12. The mechanical energy of the
rotating extra blade wheel 2 is converted by the
generator to electrical energy which may be used for
feeding various electrical appliances of the engine
powered machine, for example an aircraft.
The above embodiment of the invention
is described by way of example only and do not exclude
another positioning of the blade wheel 2, for example
in the area of the engine exit nozzle 51. The blades of
the extra blade wheel may have an aerodynamic shape and
further associated with a mechanism for adjusting
their position with respect to the direction of the
fluid stream.
Another example of the application of
an extra blade wheel to a fluid engine in the form of
water turbine is illustrated in a simplified view in
absence of a guide wheel in Fig. 4. A horizontally
situated impeller - water S- turbine runner wheel 61
coupled with an electric generator 62 is situated
within the turbine clothing 8 in the entrance tube with
the water flow direction denoted by arrow 82.
Downstream the runner wheel 61, an extra blade wheel 7
is located at a distance equal to a diameter of the
runner wheel 61. The extra blade wheel 7 is mounted on
a common shaft 75 together with an auxiliary generator
76. The distance between the runner wheel 61 and the
extra blade wheel 7 is dependent inter alia on the
density and the velocity of the liquid, cross-sections
ratio etc. The extra blade wheel 7 for driving of the
auxiliary generator 76 is actuated by a rotational power
component of the vortex generated by the runner wheel 61.
A more detailed view of another, in
this case vertical arrangement of a water turbine of a
Kaplan turbine type is shown in Fig. 5 and Fig. 6. The
turbine is also illustrated in a simplified form without
a guide wheel. The impeller - runner wheel 61 of the
turbine is born by a shaft 6 arranged in a vertical
position inside a turbine clothing 8. Under the
turbine, am extra blade wheel 7 is situated. The blades
of the extra blade wheel are embedded by their outer
ends in a peripheral ring 72 and by their inner ends
in a central ring 78. The peripheral ring 72 is carried
in a tapered roller bearing 73. A winding assembly of
a rotor 71 of a generator is arranged along the
perimeter of the peripheral ring 72. The winding of a
corresponding stator 81 of the generator is built in
opposite to it, in the turbine clothing 8. The
generator is watertight sealed towards the internal room
of the clothing 8 by a package 74. The blades are
mounted on pivots 77 fixed in the peripheral ring 72
and are associated with a non-illustrated adjusting
mechanism. As in the preceding example, the extra
blade wheel 7 powering the rotor 71 of the generator
is actuated by rotational force component of the vortex
generated by the runner wheel 61. The blade adjusting
mechanism enables optimal regulation of the speed of
the extra blade wheel 7 and simultaneously adjusting the
characteristics of water flow in the draft tube
downstream the extra blade wheel 7.
The foregoing examples of the
embodiment of the invention do not limit the described
process of conversion of the extra blade wheel kinetic
energy to electric energy. The electric generator may be
substituted by another device for conversion of the
blade wheel kinetic energy. For example, instead of an
auxiliary generator 76 in Fig. 4 a hydraulic pump may
be utilized as a source of pressure energy. The
cross-sectional area of the clothing in the area of
blade wheel may be enlarged to eliminate the change in
the flow rate in the blade wheel due to a passive
elements of the blade wheel supporting structure, etc.
The extra blade wheel structure
according to the invention may be applied to all fluid
machines with a impeller actuated by kinetic or
pressure fluid energy, such as water or gas turbines or
fluid machines generating the kinetic energy by means
of a power unit such blowers, suction or pressure fans etc.
Claims (1)
1. A fluid machine having an impeller (12; 61)
with a plurality of blades and including a fluid
inlet room and a fluid outlet room characterized in
that an extra blade wheel (2; 7) rotatably mounted
independent of the rotation of the impeller (12; 61)
is located on the downstream side of the impeller
(12; 61) and this extra blade wheel (2; 7) is associated
with a device for conversion of the extra blade
wheel kinetic energy into electric or pressure energy.
2. The fluid machine of claim 1, wherein the
extra blade wheel (2; 7) is located at the distance
equal to 0.2 up to 2 multiple of the outside
diameter of the impeller (12; 61).
3. The fluid machine of claims 1 or 2, wherein t
he position of blades of the extra blade wheel with
respect to the fluid stream is controlled by an
adjusting mechanism.
4. The fluid machine of any of claims 1 to 3,
wherein the device for conversion of the kinetic
energy is an electric generator or a hydraulic pump.
5. The fluid machine of any of claims 1 to 4,
wherein t he impeller is a fan (12) of an air bypass
turbojet engine and the blades of the extra blade
wheel (2) are located in the air bypass channel (41).
6. The fluid machine of claim 5, wherein the
extra blade wheel (2) comprises a hub (21) carrying
a rotor of an electric generator and rotatably
mounted on a hollow journal (31) fixed to the engine
body (5) and including a stator of the electric generator.
7. The fluid machine of any of claims 1 to 5,
wherein t he impeller is a runner wheel (61) of a
water turbine.
8. The fluid machine of claim 7, wherein t he
outer ends of the blades of the extra blade wheel
(7) are attached to a watertight sealed peripheral
ring (72) for receiving a rotor (71) of an electric
generator and carried in bearings (73) incorporated
in a turbine clothing (8) together with a stator
(81) of the electric generator.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CZ20110107A CZ2011107A3 (en) | 2011-03-02 | 2011-03-02 | Vane machine |
CZPV2011-107 | 2011-03-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2012117365A1 true WO2012117365A1 (en) | 2012-09-07 |
Family
ID=45998415
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/IB2012/050963 WO2012117365A1 (en) | 2011-03-02 | 2012-03-01 | Fluid machine |
Country Status (2)
Country | Link |
---|---|
CZ (1) | CZ2011107A3 (en) |
WO (1) | WO2012117365A1 (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107355314A (en) * | 2017-08-24 | 2017-11-17 | 刘雨棣 | It is segmented tandem electric rotor fanjet and its control method |
CN110107426A (en) * | 2019-05-08 | 2019-08-09 | 中国航空发动机研究院 | Across the medium flight device power device shared based on combustion chamber between grade and turbine water sky |
JP2019210922A (en) * | 2018-06-08 | 2019-12-12 | 株式会社東芝 | Energy recovery device for hydraulic machine, hydraulic machine, and operation method for hydraulic machine |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN113513801B (en) * | 2021-04-20 | 2022-09-27 | 深圳博强建设开发有限公司 | New energy-saving building with air conditioning function |
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CH316900A (en) * | 1953-04-15 | 1956-10-31 | Escher Wyss Ag | Hydroelectric machine system with counter-rotating impellers |
US4175640A (en) | 1975-03-31 | 1979-11-27 | Boeing Commercial Airplane Company | Vortex generators for internal mixing in a turbofan engine |
US5261787A (en) | 1992-01-17 | 1993-11-16 | Impsa International, Inc. | Water turbines and water flow transition members therefor |
DE4320180A1 (en) * | 1992-06-19 | 1993-12-23 | Antonio Artinano | Rotor unit for axial flow turbo-engine - with constant profile variation of fluid passage between rotor core and outer jacket |
US20070169462A1 (en) * | 2004-01-31 | 2007-07-26 | John Sharp | Gas turbine, especially an aircraft engine |
JP2008014202A (en) * | 2006-07-05 | 2008-01-24 | Kawasaki Heavy Ind Ltd | Hydraulic power generating device |
WO2009153124A2 (en) * | 2008-05-27 | 2009-12-23 | Siemens Aktiengesellschaft | Turbine motor with at least two rotors |
-
2011
- 2011-03-02 CZ CZ20110107A patent/CZ2011107A3/en unknown
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2012
- 2012-03-01 WO PCT/IB2012/050963 patent/WO2012117365A1/en active Application Filing
Patent Citations (7)
Publication number | Priority date | Publication date | Assignee | Title |
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CH316900A (en) * | 1953-04-15 | 1956-10-31 | Escher Wyss Ag | Hydroelectric machine system with counter-rotating impellers |
US4175640A (en) | 1975-03-31 | 1979-11-27 | Boeing Commercial Airplane Company | Vortex generators for internal mixing in a turbofan engine |
US5261787A (en) | 1992-01-17 | 1993-11-16 | Impsa International, Inc. | Water turbines and water flow transition members therefor |
DE4320180A1 (en) * | 1992-06-19 | 1993-12-23 | Antonio Artinano | Rotor unit for axial flow turbo-engine - with constant profile variation of fluid passage between rotor core and outer jacket |
US20070169462A1 (en) * | 2004-01-31 | 2007-07-26 | John Sharp | Gas turbine, especially an aircraft engine |
JP2008014202A (en) * | 2006-07-05 | 2008-01-24 | Kawasaki Heavy Ind Ltd | Hydraulic power generating device |
WO2009153124A2 (en) * | 2008-05-27 | 2009-12-23 | Siemens Aktiengesellschaft | Turbine motor with at least two rotors |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107355314A (en) * | 2017-08-24 | 2017-11-17 | 刘雨棣 | It is segmented tandem electric rotor fanjet and its control method |
JP2019210922A (en) * | 2018-06-08 | 2019-12-12 | 株式会社東芝 | Energy recovery device for hydraulic machine, hydraulic machine, and operation method for hydraulic machine |
CN110107426A (en) * | 2019-05-08 | 2019-08-09 | 中国航空发动机研究院 | Across the medium flight device power device shared based on combustion chamber between grade and turbine water sky |
Also Published As
Publication number | Publication date |
---|---|
CZ2011107A3 (en) | 2012-09-12 |
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