# US 5,344,281 A · Rotary vortex machine

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- Number: US 5,344,281 A
- Document ID: US5344281A
- Status: Granted
- Kind: A
- Application number: 07/949,642
- Filed: 1992-12-02
- Granted: 1994-09-06
- Earliest claimed: 1992-12-02
- Assignees: Osoboe Konstruktorskoe Bjuro Po Konstruirovaniju, Issledovaniju I Vnedreniju Glubinnykh Besshtangovykh Nasosov
- Inventors: Vladimir D. Anokhin; Anatoly I. Lepekha; Viktor N. Filippov; Sharifzhan R. Ageev; Anatoly F. Vinokurov; Jury V. Gusev; Sergei J. Ermakov
- Web page: https://patentgrep.com/patent/US5344281A

## CPC

- F01D 1/34: characterised by non-bladed rotor, e.g. with drilled holes (F01D1/32 takes precedence; sirens G10K7/00 {; impact turbines with buckets F01D1/026; hand-held tools with a non-bladed rotor F01D15/067})
- F04D 5/002: {Regenerative pumps (for elastic fluids F04D23/008)}
- F04D 23/008: {Regenerative pumps (for liquids or for liquids and elastic fluids F04D5/002)}
- F04D 29/161: {especially adapted for elastic fluid pumps}
- F04D 29/165: {especially adapted for liquid pumps}
- F04D 29/188: {specially for regenerative pumps}
- Y02T 50/60: Efficient propulsion technologies, e.g. for aircraft
- F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D)
- F04D: NON-POSITIVE-DISPLACEMENT PUMPS (engine fuel-injection pumps F02M; ion pumps H01J41/12; electrodynamic pumps H02K44/02)
- Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION

## Abstract

A rotary vortex machine having a stator (1) with an internal annular space (4) accommodating vanes (9) and a rotor (6) with an external annular space (7) accommodating a bridge (10) dividing the external annular space (7) into suction and delivery volumes. The rotor (6) has a curvilinear inlet passage (11) and a curvilinear outlet passage (12) to provide a flow of a service fluid essentially in one and the same direction in the suction and delivery volumes of the external annular space (7).

## Claims

### Claim 1

A rotary vortex machine comprising a stator (1) with an internal annular space (4) accommodating vanes (9), an inlet passage (2) and an outlet passage (3) for a service fluid, and a fluid energy converting stage installed in the stator (1) on a drive shaft (5) and comprising a rotor (6) having an external annular space (7) combined with the annular space (4) of the stator (1) and forming, together with said annular space (4), a working annular chamber (8), and a bridge (10) disposed in the annular space (7) of the rotor (6) and dividing said annular space (7) of the rotor into suction and delivery volumes communicating with the inlet passage (2) and the outlet passage (3) of the stator (1), said rotor (6) having a curvilinear inlet passage (11) and a curvilinear outlet passage (12) which connect the suction and delivery volumes of the annular space (7) of the rotor (6) with the inlet passage (2) and the outlet passage (3) of the stator (1), said curvilinear inlet and outlet passages being arranged on both sides of the bridge (10) in such a manner that the flow of the service fluid moves through said curvilinear passages (11, 12), essentially, in one and the same direction, the bridge (10) in the zone of said curvilinear passages (11, 12) having a variable cross section and being positioned at an angle relative to a radial plane passing through said bridge (10).

### Claim 2 (depends on 1)

A rotary machine as claimed in claim 1, further comprising at least one additional stage (17) for conversion of fluid energy installed so that its curvilinear inlet passage (18) communicates with the curvilinear outlet passage (12) of the preceding stage, the rotors (6 and 19) of the stages being mounted on the drive shaft (5) with a provision for axial movement and installed on supporting end seals (22) located between the stators and rotors at the side of the curvilinear inlet passages (11, 18).

### Claim 3 (depends on 1)

A rotary machine as claimed in claim 1, wherein end surfaces of said annular spaces (31 and 32) of said stator (30) and said rotor (29) are provided with a spiral-shaped curvilinear inlet passage (35) and a spiral-shaped curvilinear outlet passage (36), said outlet passage (37) of the stator (30) being in the form of a volute-shaped diffuser (38) having a winding direction opposite a winding direction of said curvilinear inlet and outlet passages (35, 36) of the rotor (29).

### Claim 4 (depends on 1)

A rotary machine as claimed in claim 1, wherein said inlet passage (38) of the stator (30) is arranged along an axis of rotation of the rotor (29).

### Claim 5 (depends on 3)

A rotary machine as claimed in claim 3, wherein said inlet passage (38) of the stator (30) is arranged along an axis of rotation of the rotor (29).