GB2207703A - Rotary fluid flow machine - Google Patents
Rotary fluid flow machine Download PDFInfo
- Publication number
- GB2207703A GB2207703A GB08717072A GB8717072A GB2207703A GB 2207703 A GB2207703 A GB 2207703A GB 08717072 A GB08717072 A GB 08717072A GB 8717072 A GB8717072 A GB 8717072A GB 2207703 A GB2207703 A GB 2207703A
- Authority
- GB
- United Kingdom
- Prior art keywords
- sheave rail
- main shaft
- center
- eccentric cylinder
- eccentric
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01C—ROTARY-PISTON OR OSCILLATING-PISTON MACHINES OR ENGINES
- F01C11/00—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type
- F01C11/006—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of dissimilar working principle
- F01C11/008—Combinations of two or more machines or engines, each being of rotary-piston or oscillating-piston type of dissimilar working principle and of complementary function, e.g. internal combustion engine with supercharger
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Rotary Pumps (AREA)
Abstract
The machine comprises a compressor section 1 which includes a rotor 3 and a casing which is internally divided into a pair of working chambers by sealing vanes 4 slidably mounted in the casing and cooperating with the rotor periphery. The compressor discharges through outlet valves (13, Fig. 1) into ducts 14 which discharge tangentially into vanes 21 of a vaned wheel which is also provided with fan vanes 22. <IMAGE>
Description
DUALISTIC SYNCHRONOUS INDUCTION TYPE COMPRESSOR
This invention relates to a dualistic synchronous induction type compressor.
Since industry revolution, people have never relaxed to research the machine which enable to improve living quality, increase efficiency and decrease productivity cost; after so many times international energy crisis had happened in the society of human being, learning how to create maximum effect with minimum energy is still approached by many research institutes; so people fancy to invent a machine can revolve forever without consuming any fuel, and had designed many kinds of machine to utilize some permanent energy resouces, such as wind, ocean tide, solar energy and ground heat to engage different kinds of work.
Compressor is one of the equipmentslçhich can improve living quality, increase efficiency and decrease productivity cost, it may be used in air condition and freezer, to drive automatic machine in factory, such as machine-cutter, robot, machine-arm etc. There are many kinds of conventional compressor like rotary, reciprocal, screwed..., these compresssors spend lots of energy during operation, and increase productivity cost indirectly.
With several years experience of researching and testing in compressor, and being endeavor to research, the inventor had been trying to find a way out that save energy most, after laboriously research over and over, he finally has designed present invention, a brand new design: Dualistic Synchronous Induction Type Compressor.
The main structure comprising a main shaft sleeved a eccentric cylinder rotor tightly is positioned in a external tube, one end of the main shaft sleeved a cone doubleply axial-flow vane-wheel; two presssure separators divide the innards of external tube into two compression cells; two sets of inhaled and exhausted units; two pieces of sealing plates; two pieces of round sheave rail disc, can. guide the pressure separators synchronous motion, enable the eccentric cylinder rotor revolves the present invention once and have compressed twice, the duct on exhaust port guide the air into the inner vanes of cone double-ply axial-flow vane-wheel.
The prime object of the said composition is related the whole design which using the principle of equivalence of equilibrium balance method in physics, by the special treatments of mass increased and decreased, the main power structure of the invention develop the function of quantity will be limited by selection of quality without changing its form, and put whole mass together on center of the main shaft and achieve effect of dynamic balance, the main shaft revolution utilize minimum energy, and no more depend on the restorable force by crank and spring as presssure separator, and eliminate friction of the pressure separator and eccentric cylinder rotor, and won't be limited by size of structure and quantity.
The second object of the present invention is related eccentric cylinder rotor and two pieces of round sheave rail disc on two ends, which are combined into one by sleeve tightly on main shaft, and become a round kinematic unit of balance power, gearing arm of pressure separator sleeved in the sheave rail of the round sheave rail disc, when the main shaft revolves, the eccentric cylinder rotor and the round sheave rail disc revolve synchronously and guide the pressure separator into the straight groove of external tube with sheave rail of the round sheave rail disc and move reciprocally, enable the external force capacity conform the gravitation effect of a spherical distribution of mass.
The third object of the present invention is related both sheave rail of round sheave rail disc and eccentric cylinder surface on center of eccentric cylinder rotor, which are in the same sharp; and every point is on the same verticality to coordinate pressure separator, and air compressor power capacity has no friction, any special lubricating device is not.necessary.
The fourth object of the present invention is related to gearing arm of pressure separator, which is a structure of the rotor revolution, twin roller is positioned on front and reciprocate on the round sheave of the round sheave rail disc, enable the pressure separator reciprocate in the straight groove of external tube, instead of conventional structure, such as belt, chain, gear, crank, etc., the sheave rail is of overlapping stairs, just match the design of twin roller, each roller is positioned between inner and outer of the sheave rail with high speed, enable the motion carried out smoothly.
The fifth object of the present invention is related to two pieces of pressure separator and two sets of indenpendant inhaled and exhausted unit, which divide the innard of external tube into two compression cells, that look like a compressor, but have the function of two sets of compressor in fact.
The sixth object of the present invention is related one end of the main shaft1 which sleeved tightly with a cone double-ply axial-flow vane-wheel, the air exhausted by the compresssor send into the inner vane through the duct, and accelerate the main shaft, then jet whirlingly, agitate air by outer whirling vane, the air force and air pressure are higher than exhausted fan.
The seventh object -of the present invention is related the structure which is simple, the volume can be changed by the requirement of air force and air pressure, the space won't be wasted, easy to move and low noise.
The eighth object of the present invention is related to low energy capacity, with lHP power to achieve the air volume of 103 m/min., the air pressure almost the same as reciprocal compressor.
An embodiment of this invention is described by way of examples, with reference to the drawings in which:
FIG.1 is a prospective view of the preferred embodiment for the present invention.
FIG.2 is a prospective assembles of the present invention.
FIG.3 is a top view of cross section of FIG.1 for the present invention.
FIG.4 is a front view of the pressure separator of the preferred embodiment for the present invention.
FIG.5 is a sketch of the connections between the roller of pressure separator and the disc of round sheave rail of the preferred embodiment.
FIG.6 is a cross section of the front view of FIG.1 for the preferred embodiment.
FIG.7 is a the sketch of cross-section of front view for another preferred embodiment.
FIG.8 is a the sketch of cross-section of front view for the other preferred embodiment.
Please refer to FIG.1 which is perspective view of the preferred embodiment for the present invention, the external tube (1) is a sealing tube and contain two horizontal straight grooves (11), it also has two inlet air valves (12) and two outlet air valves (13), outlet air valves (13) connect the duct (14) and lead the wasted air into the tangential direction of the inner vane (21) of cone double-ply axial-flow vane-wheel (2), two ends of the external tube (1) is fixed by fixing plate (15) and also be sealed, cone double-ply axial-flow vanewheel (2) is divided into inner vane (21) and outer whirling vane (22), inner vane (21) enable the main shaft (31) increase the accelerative effect of two-cylinder engine by exhausted duct (14), enable external whirling vane (22) create the effect both of exhausted fan and compressor.
Please refer to FIG.2 which is detail assembles of the perspective view for the present invention, an eccentric cylinder rotor (3) with two disc ends and eccentric cylinder center is positioned in external tube (1), the rotor penetrated through by a main shaft (31), the pressure separator (4) moves reciprocally in the straight groove (11); two sealing covers enclose two ends of the external tube (1), enable the whole external tube to be sealed completely; two pieces of round sheave rail disc (32) on two ends of the external tube (1), there are eccentric cylinder sheave rails outside of every round sheave rail disc (33), and the form of the disc is just the same as the center eccentric cylinder of the eccentric cylinder (3), also homo-step, in other words, both eccentric cylinder rotor (3) and two pieces of round sheave rail disc (34) sleeved tightly on the main shaft, and any point of the center cylinder ofthe eccentric cylinder rotor (3) and sheave rails (34) of two disc are on the same vertical line; the eccentric cylinder sheave rail (34) may lead the pressure separator (4) and move reciprocally in the straight groove; two flat fixing plates (15) are fixed on two sides of the external tube (1), the cone double-ply axial-flow vanewheel (2) sleeved tightly on the main shaft (31).
Please refer to FIG.3 which showing top view of cross section for FIG.1, from which we can see parts combination of the present invention, the pressure separator (4) is convex, the contact surface with the eccentric cylinder rotor (3) is a sealing rod (41) enable the contact to be sealed and rolling smoothly by several weak springs; the main shaft (31) is fixed on the fixing plate (15) by two roller and enable the roll be smooth by supporting the weight of the eccentric cylinder rotor (3); two ends of the pressure separator (4) compsed by every two roller axis (43) positioned in the sheave rail (34) of the round sheave rail disc (33). Every point inside of the sheave rail (34a)(34b) and the cylinder side surface (35) of the eccentric cylinder rotor (3) are kept on the same straight line, in other words is its homo-step motion.
Please refer to FIG.4 showing the front view of the pressure separator for the present invention, inside of the pressure separator (4) contains sealing rod (41) and several weak springs (42), the twin roller (43) is positioned inside of two ends, the connecting rod (44) outside connect two homo-step arm (45). Several rolls (46) are positioned on the arm to achieve rational non-friction when the pressure separators (4) roll in the straight sheave rail (11).
Please refer to FIG.5 showing assembling of the pressure separator roll and round sheave rial disc of the present invention, the sheave of the sheave rail (34) on tie round sheave rail disc (33) is of stairs, every set contains two rolls (43) of the pressure separator (4), the under rolls lean on the right side of the sheave rail, the upper rolls lean to the left side of the sheave rail, two rolls (43) balance each other, the balance roll of the pressure separator (4) never get loose.
Please refer to Fig. 6 showing the crosssection of the front view of Fig.l for the present invention, from which we can understand the operations and inhal and exhaust operations for the present invention, it divide into two compression cells up and down (a,b), the main shaft (31) guide the eccentric cylinder rotor (3) revolves clockwise, the air have finished the first compression stroke with inhale by inlet air valve (12a) and exhaust by 'outlet air valve (13a); then the second compression stroke have finished with inhale by fllt-air valve (12b) and exhaust by outlet air valve (13b), so the eccentric cylinder rotor (3) revolves once, but compresses twice in face.
inner vane (21) of the cone double-ply axial-flow vanewheel (2) through the duct to accelerate the main shaft, simultaneously lead the external whirling vanes (21) and get strong .whirlpool to oreate air of high force and high pressure, so the invention have not only the effect of compressor, but also have adventage of exhausted fan.
Consequently as described above, the present invention applicate the principle of equilibrium in the balance method, ans with mass increased or decreased special treatment among the structures, develop the functions to limit quantity by selection of quality, and put whole mass together on the center of the main shaft, and achieve the effect of dynamic balance. By tests, the inventor has achieved 1720 rpm high speed revolution with HP motor in nil capacity and 20-50 kg loading on the main shaft, the air volume is over 103 m/min., created the great revolution momentum, utilize energy minimum.
On the design of the invention, the homostep arm (45! and the twin roller (43) instead of conventional structure, such as belt, chain, gear, crank etc., without movement and friction, can keep the structure stable and increase using time. The inner of external tube (1) divide into two compression cells with pressure separator (4), two compression is finished when the eccentric cylinder rotor (3) revolves once, then the exhaust air of compression stroke send into the inner vanes of the cone double-ply axial-flow vane-wheel through the duct, the main shaft is accelerated and creating power, and lead the external whirling vanes creating the air of high force and high pressure, to have the maximum effect with minimum energy, is the first invention of the inventor, and also have preferred embodiment to test the functions thus prove to be a breakthrough design.
The invention is not restricted by all said example, any one who familiar such skill can do any kind of variation, finish and application, all of them is included in the patent cortent of the invention.
Claims (7)
1. A dualistic synchronous induction type compressor com- prising:
A external tube which is instructed by a circular
tube shape comprising a both horizontal direction
straight groove that two inlet air valves and two
outlet air valves are positioned on it;
Two inlet air valves that a coarse filter mesh and
a stop valve are positioned in front of it;
Two outlet air valves that wasted air are sent -into
the tangential direction of the inner vanes of the
cone double-ply axial-flow vane-wheel;
An eccentric cylinder or ellipsoid roller that is
positioned in the external tube and shaped two ends
in disc, the center is eccentric cylinder, the rotor
center penetrate a main shaft among them;
Two sealing covers are positioned on the two ends
of the external tube to seal the external tube;;
Two round sheave rail discs are positioned outside
of the sealing cover and two ends of external tube,
there are eccentric or ellilpsoid sheave rails outside
of the disc; the sheave rail is of two-stairs, just
match the eccentric cylinder or ellipsoid on center
of the eccentric cylinder rotor or ellipsoid sheave
rail, it is vertical no matter any angles it revloves,
and achieve object of synchronous, both centers of
sealing cover and round sheave rail disc penetrate
the main shaft;
Two fixing plates are positioned outside of round
sheave rail disc and two ends of external tube;
A cone double-ply axial-flow vane-wheel is divided
into the inner vane and the external whirling vane,
sleeved on the main shaft tightly;;
Two pressure separators shaped in convex, there is
a set of twin rollers inside of two ends, the twin
rollers just install inside sheave rail of the round
sheave rail disc, the surface on the center convex
of the pressure separator and the eccentric cylinder
on the center of the eccentric cylinder rotor is a
sealing rod with several weak springs; and
All combination described above are characterized
by the eccentric cylinder rotor positioned in the
external tube, which match the pressure separator
and the inhaled and, exhausted unit to separate the
compression cell into two, the compressor capacity
become multiple increase, and the design transfer
the center of mass into center of the eccentric drived
the main shaft to balance the power, utilize energy
minimum and achieve multiple compression effect.
2. As described in Claim 1, a dualistic synchronous induc
tion type compressor of the claim for the present
invention, both the eccentric cylinder rotor and two
round sheave rail discs sleeve tightly on the main
shaft, and sheave rail of round sheave rail disc just
match the eccentric cylinder on the center of the
eccentric cylinder rotor, enable to keep vertical
wherever it may be, sheave rail positioned in twin
rollers of the pressure separator guide the pressure
separator, to be characterized by homo-step motion
non-friction capacity.
3. As described in Claim 1, a dualistic synchronous induc
tion type compressor of the claim for the present
invention, the straight sheave rail and the sheave
rail of the eccentric or ellipsoid in disc change
circular motion into linear motion by the criven of
homo-step arm bearing, it is characterized by instead
of conventional driving structure such as belt, chain,
gear and crank.
4. As described in Claim 1, a dualistic synchronous induc
tion compressor of the claim for the present invention,
the main driving structure of compression such as
eccentric cylinder rotor, round sheave rail disc etc,
as a compositive structure, breakthrough balance method
in power of conventional mass equivalent, enlarge
the application in the principle of the equilibrium,
with special treatment to limit quantity by selection
of quality, transfer the mass center of the cylinder
of eccentric structure on the center of the main shaft,
it is characterized by creating high speed motion
with a little energy and creating great inertia momentum.
5. As described in Claim 1, a dualistic synchronous induc
tion type compressor of the claim for the present
invention, the other end of the main shaft sleeved
tightly a cone double-ply axial-flow vane-wheel, the
exhausted air send into inner vanes through the duct,
creating power of two cylinder engine to a accelerate
the main shaft, simultaneously guiding the external
whirling vanes agitate air and exhaust whirlingly,
it is characterized by high air force and high air
pressure just like blast fan.
6. As described in Claim 1, a dualistic synchronous induc
tion type compressor of the claim for the present
invention, it is characterized by simple structure,
not waste space, easy to move, low noise, no lubricating
device need and the volume can be changed in the same
scale.
7. A dualistic synchronous induction type compressor,
and arranged substantially as herein described with
reference to any of the figures of the drawings.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB08717072A GB2207703A (en) | 1987-07-20 | 1987-07-20 | Rotary fluid flow machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB08717072A GB2207703A (en) | 1987-07-20 | 1987-07-20 | Rotary fluid flow machine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| GB8717072D0 GB8717072D0 (en) | 1987-08-26 |
| GB2207703A true GB2207703A (en) | 1989-02-08 |
Family
ID=10620958
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB08717072A Withdrawn GB2207703A (en) | 1987-07-20 | 1987-07-20 | Rotary fluid flow machine |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB2207703A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6347611B1 (en) * | 2000-07-17 | 2002-02-19 | Ellis F. Wright | Rotary engine with a plurality of stationary adjacent combustion chambers |
| FR2827006A1 (en) * | 2001-07-09 | 2003-01-10 | Roger Lafleur | Rotary engine comprises stator, housing containing rotor and shaft with surface forming sliding control cam for stator blades which delimit combustion chambers associated with fuel and oxidant compression circuits |
| GB2379482A (en) * | 2002-01-15 | 2003-03-12 | Alexander Orestovich Monfor | Hydraulic motor-generator |
| US20130259730A1 (en) * | 2010-11-29 | 2013-10-03 | Albert W. Patterson | Rotary pump with a vane provided in each pump outlet |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB307661A (en) * | 1928-05-18 | 1929-03-14 | Otto Schumann | Improvements in rotary internal combustion engines |
| GB440493A (en) * | 1934-07-02 | 1936-01-01 | Francis Donald Fisher | Improvements in and relating to internal-combustion turbines and compressor units |
| GB622608A (en) * | 1947-04-01 | 1949-05-04 | Alan Ferdinand Thompson Sellar | Improvements in rotary combustion engines |
| GB1100367A (en) * | 1966-02-25 | 1968-01-24 | Antonio Rodriguez Huerta | Internal combustion engine |
| GB1464323A (en) * | 1974-06-06 | 1977-02-09 | Kunoti M | Rotary positive-displacement pump or motor |
| GB2078304A (en) * | 1980-06-18 | 1982-01-06 | Ching Ho Tseng | Rotary positive-displacement fluid-machines |
| GB2133837A (en) * | 1983-01-19 | 1984-08-01 | Nissan Motor | Rotary fluid-pump |
-
1987
- 1987-07-20 GB GB08717072A patent/GB2207703A/en not_active Withdrawn
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB307661A (en) * | 1928-05-18 | 1929-03-14 | Otto Schumann | Improvements in rotary internal combustion engines |
| GB440493A (en) * | 1934-07-02 | 1936-01-01 | Francis Donald Fisher | Improvements in and relating to internal-combustion turbines and compressor units |
| GB622608A (en) * | 1947-04-01 | 1949-05-04 | Alan Ferdinand Thompson Sellar | Improvements in rotary combustion engines |
| GB1100367A (en) * | 1966-02-25 | 1968-01-24 | Antonio Rodriguez Huerta | Internal combustion engine |
| GB1464323A (en) * | 1974-06-06 | 1977-02-09 | Kunoti M | Rotary positive-displacement pump or motor |
| GB2078304A (en) * | 1980-06-18 | 1982-01-06 | Ching Ho Tseng | Rotary positive-displacement fluid-machines |
| GB2133837A (en) * | 1983-01-19 | 1984-08-01 | Nissan Motor | Rotary fluid-pump |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6347611B1 (en) * | 2000-07-17 | 2002-02-19 | Ellis F. Wright | Rotary engine with a plurality of stationary adjacent combustion chambers |
| FR2827006A1 (en) * | 2001-07-09 | 2003-01-10 | Roger Lafleur | Rotary engine comprises stator, housing containing rotor and shaft with surface forming sliding control cam for stator blades which delimit combustion chambers associated with fuel and oxidant compression circuits |
| GB2379482A (en) * | 2002-01-15 | 2003-03-12 | Alexander Orestovich Monfor | Hydraulic motor-generator |
| GB2379482B (en) * | 2002-01-15 | 2003-11-26 | Alexander Orestovich Monfor | Hydraulic motor-generator |
| US20130259730A1 (en) * | 2010-11-29 | 2013-10-03 | Albert W. Patterson | Rotary pump with a vane provided in each pump outlet |
| US8985982B2 (en) * | 2010-11-29 | 2015-03-24 | 1564330 Ontario Inc. | Rotary pump with a vane provided in each pump outlet |
Also Published As
| Publication number | Publication date |
|---|---|
| GB8717072D0 (en) | 1987-08-26 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |