WO1984001758A1

WO1984001758A1 - Turbo jet pump

Info

Publication number: WO1984001758A1
Application number: PCT/AU1982/000177
Authority: WO
Inventors: George Branko Skrinjar
Original assignee: Skrinjar Designers Constructor; Gbs Dita Pty Ltd; George Branko Skrinjar
Priority date: 1982-10-27
Filing date: 1982-10-27
Publication date: 1984-05-10
Also published as: EP0124512A1; AU9052682A

Abstract

A turbo jet pump comprising a driven shaft (6) having, attached impeller blades (13), rotor blades (17) rotatable freely rotatable on shaft (20), the pumped liquid being forced past diverter ribs (14 and 21) at increasing velocity.

Description

Turbo Jet Pump

D E S C R I P T I O N

Sheet 1/4 - 4/4 shows invention of the Turbo Jet Pump, invented, designed and constructed by George Branko Skrinjar for heavy liquids.

Sheet 1/4 - 4/4 shows invention of the Turbo Jet Pump, invented, designed and constructed by George Branko Skrinjar for light liquids. FIG. 1 - 2 is a longitudinal section of the Turbo Jet Pump showing the main elements. FIG. 1A- 2A is a cross section A - A, through the Suction stage of the Turbo Jet Pump, showing the Front of the Action Impeller. FIG. 1B- 2B is a cross section B - B, through the Diverter stage I showing the Front of the Diverter

Passages. FIG. 1C- 2C is a cross section C -C, through the Reactor stage showing the Front of the Reactor Turbine wheel. FIG. 1D- 2D is a cross section C - C, through the Diverter stage II, showing the Front of the Diverter

Passages.

Through the Turbo Jet Pump Body 1 , passes vertical drive shaft 2, which rotates in the Bearings 3 and 4., the Vertical drive Shaft 2, through helical Gears 5, in the gear Box 9, and horizontal Shaft 6, which is rotating in its Bearings 7 and 8 and 12, rotates the Impeller 10, assembled on the shaft with Keys 11., the Impeller 10, has blades 13.

The Diverter Core 15, is connected with Diverter Ribs 14, to the Diverter Body 16., the Reactor Blades 17, are fixed to the Reactor Wheel 18, which freely rotates in the slide Bearing 19, on the Shaft 20, casted in the Diverter Core 22, connected with Diverter Ribs 21, to the Diverter Body 23, which is bolted together with first Diverter stage Body 16, sheet 1/4, FIG. 1, to the Body 1, with Bolts 24., The Cap 25, is fixed with bolts to the gear box Body 9., the Flange 26, holds the Bearing 3, in position, and is bolted to the Turbo Jet Pump Body 1., the seal Ring 27, is positioned in the groove between Impeller Body 10, and first stage Diverter Core 15., the Desmophrene packers 28, are pressed into the gear Box 9., the Diverter Body 23, and the Diverter Eody 16, are fixed with Bolts 29,and 24, to each other, and together to the Turbo Jet Pump Body 1., the Thrust Bearing 30, is situated in the Flange 26, bolted to the Turbo Jet Pump Body 1.

FIG. 1E - 1L and 2E - 2L, show elevation, plan and contuor line of the Blades and Ribs.

Claims

C L A I M S

CLAIM 1 Principle of Operation

Suction of the Media direct from the Front into the

Turbo Jet Pump. Divertisation of molecules of the

Media streams flow, and transfer of Media flow by rotation of the Reactor turbine, through Diverters out to the back through jet nozzle.

CLAIM 2 The Contour line, outside and inside of the operation Stages elements of the Turbo Jet Pump. CLAIM 3 Stages of Operation

Action Impeller, Diverter I, Reactor, Diverter II. CLAIM 4 Driven direct or through transmission with flexible or solid vertical or horizontal shaft by combustion engines or electric motors.

CLAIM 5 Assembly of the Turbo Jet Pump direct into pipe line or in any degree elbow.

CLAIM 6 As a water bore Pump, direct into the casing. CLAIM 7 For Pumping the gases and light and heavy liquids. CLAIM 8 Impeller Blades from 55 -- 3311 Diverter I Ribs from 66 -- 3322 Reactor Blades from 33 -- 2299

Diverter II Ribs from 44 -- 3300

Inlet ϕ S from 50 mm -- 17 000 mm

Outlet ϕ O from 10 mm -- 10 000 mm

Length 0 from 100 mm -- 30000 mm

CLAIM 9 Operation in Reverse. CLAIM 10 The Turbo Jet Pump, is a Pump System Skrinjar.