The invention refers to a fluid energy machine with a circular or ellipsoid casing cylindrical in one direction, with one or several fluid inlets and one or several fluid outlets, in which a circular turning rotational body is placed coaxially (centred, central) and rotatable on a bearing.
The invention can be applied in the following areas of use.
The fluid energy machine according to the invention is able to cover nearly any area of application because it combines various other features in itself. A conventional pump or turbine requires a higher energy expenditure or throughput for liquid or gaseous media as compared to the invention. This is circumvented with the invention; the invention is independent of performance and speed.
Additionally, the fluid energy machine must have the highest possible efficiency. Furthermore, the invention of this fluid energy machine can be produced maintenance- and wear-free. The underlying principle should be applied in the above areas of applications.
The term of fluid energy machine comprises all machines where a fluid is involved in energy conversion in liquid or gaseous form.
For example, turbines, pumps, condensers, vacuum pump, force transmission (drives), and in the end also jet drives. A turbine converts the kinetic energy of fluids into turning or rotational energy; they therefore are continuous flow machines. Pumps, in contrast, are fluid energy machines in which the energy inherent to the fluid is increased by application of mechanic force. The pressure of the fluid medium is increased or kinetic energy is added, often for the purpose of changing position.
A conventional pump is usually only suitable specifically for a few areas of application. Generally, a great number of fluid energy machines are known; they are specifically used in different builds for a few areas of application. All fluid energy machines have in common that they should be constructed for the highest possible efficiency. This means that the highest possible share of the underlying input energy is converted into the desired output energy. This requires that the fluid energy machine has a low loss itself.
Common pumps in the form of a vane pump, for example, are known from the publications DE 691 25 372 T2, DE 10 2006 021 252 A1 and GB 319 467 A. Either of these publications describes a vane pump with vanes that are moved into and out of slots in a rotor with a forced guide.
The task of the present invention is to create a fluid energy machine that can be produced cost-efficiently and simply.
This task is solved by a fluid energy machine pursuant to patent claim 1.
The fluid energy machine according to the invention has the characteristics of pumping back and forth, achieving high displacement volumes, generating high pressure or vacuum and achieving best values at dry intake from large heights. Furthermore, the fluid energy machine requires only a low speed (energy savings) or much lower use of a fluid medium to achieve the comparable or better values of conventional fluid energy machines, turbines. Thus, the areas of application as fluid energy machine pump, turbine, condenser, vacuum pump, force transmission (drives), jet drive are widely spread.
The fluid energy machine according to the invention has the following characteristics:
The principle of the fluid energy machine is that the fluid in the chamber (gap) moves (is pumped) between the inner circular turning rotational body and the inner bore (recess) of the outer casing, with a lock provided between the fluid in- and outlets. Pressure is built against this lock in rotating direction, with a vacuum building behind the lock in rotating direction, independently of whether the fluid media are liquid or gaseous.
It is also essential that the blades are able to pass the lock. For this purpose, they must be retracted in the groove (recess) of the turning rotational body in the area of the lock so that they are lowered into the turning rotational body when passing the lock; after passing the lock and reaching the fluid inlet, they are extended again by forced control in the outer body bottom and lid, built as a circular and ellipsoid combined groove that retracts and extends the blade; the rotational motion of the turning rotational body converts the blade motion into linear motion.
The following figures explain the invention in more detail, with this only being example setups. They show:
An example principle presentation of the invention as fluid energy machine, pump, turbine, condenser, vacuum pump or jet drive.
An example principle presentation of the forced control in the bottom and lid of the outer casing.
An example principle presentation of the blade with ball bearing.
An example principle presentation of the lock.
An example principle presentation of the turning rotational body.
An example principle presentation of the pressure handover area, by duct or groove in the casing bottom and casing lid.
An example principle presentation of the pressure handover area by duct or groove in the outer casing.
An example principle presentation to move the fluid, behind the blades by duct or groove in the blade, down when retracting and in when extending.
An example principle presentation to move the fluid, behind the blades by duct or groove in the turning rotational body, down when retracting and in when extending.
Furthermore, the casing 21 has at least one fluid inlet 26 and at least one fluid outlet 27.
The casing 21 has an inner diameter D1 that is smaller than the outer diameter D2 of the casing 21, the circular turning rotational body 24 in turn has a smaller outer diameter D3 than the inner diameter D1 of the casing 21, so that a chamber (gap) 18 remains between the circular turning rotational body 24 and the casing 21 into which the fluid medium gets.
The fluid enters the chamber (gap) 28 through the fluid inlet 26 and leaves it again in rotational direction through the fluid outlet 27; the flow direction depends solely on the direction of the input energy, so that the fluid inlet 26 and the fluid outlet 27 only depends on the rotational direction and pumping forwards and backwards is possible. The fluid is either transported through the chamber (gap) 28 into the circular turning rotational direction by the blades 31, i.e. the circular turning rotational body 24 is driven as pump when in use, or the fluid itself affects the blades 31 and drives the circular turning rotational body 24 like a turbine. The blades 31 can be retracted completely into the turning rotational body in the grooves (recess) 32.
In the design example displayed, the blades 31 are attached with axles 33 on both sides to attach two differently sized bearings 34 above each other there that move the track of the staged forced control 35 in the casing bottom 36 and casing lid 36 (run along it), to completed retract or extend the blade 31.
With one of the two bearings 34 attached on top of each other at the blade 31 serving to extend blade 31 and the other bearing 34 to retract the blade 31; this is achieved by the staged forced control 35 in the casing bottom 36 and casing lid 36.
In the extended condition, the blades 31 close the chamber (gap) 28 so that the fluid cannot flow back; sealing should be as tight as possible and the blade 31 can pass lock 37 when retracted, so that a backpressure forms in rotational direction before lock 37 and is drained through fluid outlet 27 while the two other blades 31 close off the chamber (gap) 28 completely. Behind lock 37, a vacuum forms when extending the blade 31 in rotational direction independently of whether liquid of gaseous fluid media are used.
With lock 37 being provided between the radial outer surface of the turning rotational body 24 and the radial inner bore (recess) 23 of the outer casing 21, separating the chamber (gap) 28 between the fluid inlet 26 and the fluid outlet 27 to lock the chamber (gap) 28 for the fluid to prevent flowing of the fluid against the desired rotational direction of the circular turning rotational body 24. With the staged forced control 35 retracting even before the lock 37 reaches blade 31 in rotational direction, but extends again after passing of the lock 37; it is provided that the other blades 31 close off the chamber (gap) 28 completely at the same time.
The invention is not limited to the design examples displayed but also comprises other design forms like the staged forced control 35 blade control as tappet, sprocket at the top and bottom side or a grinding tappet, and the shape of the blades 31 should be adjusted to the demanded conditions according to the knowledge of flow mechanics and flow technology.
Number | Date | Country | Kind |
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PCT/DE2010/000018 | Jan 2010 | DE | national |