| AU412103B2 | 1968-05-23 | |||
| AU244364B | ||||
| GB1323872A | 1973-07-18 | |||
| GB1094169A | 1967-12-06 | |||
| DE2749698A1 | 1979-05-10 |
| 1. | CLAIM 1 Hydro Jet system Skrinjar contains three different types of blades; five compression o o blades equally spaced in circle at 72 and 24 positioned with axial line PIG. 6 Sheet 2/. |
| 2. | Five transfer blades equally spaced in circle at 72 and 30 positioned with axial line PIG. 5 Sheet 2/2. Ten reactor blades equally spaced in circle at 36° and 35° positioned with axial line PIG. 4 Sheet 2/2. CLAIM 2 Shape of the blades PIG. 1, PIG. 2 and PIG. 3 Sheet 2/2. CLAIK 3 Shape of the Rotor. CLAIM 4 Dimensions of the Jet as follows. IITLS'J. from <f> 70 mm i 7000 mm. OUTLET from ύ 50 mm ύ 6000 mm. LEITGTH from 250 mm to 30000 mm. CLAIM 5 Assembly of the Jet τ o water vehicles from underneath of the water vehicles body. CLAIM o Adaptable to all types cf inboard and outboard engines. CLAIM 7 Transferring of light and heavy liquids eg. water, oil, slurry for industrial purposes. CLAIM 8 Driven direct or through transmission with flexible or solid drive shaft. |
DESCRIPTION
On the Sheet 1/2 is shown invention of HYDRO JET invented, designed and constructed by George Branko Skrinjar. FIG. 1 is longitudinal section of the Hydro Jet, showing the -main elements. PIG. 2 is a fron elevation of the Hydro Jet. Through the Body 1 , is passing from the engine vertical Shaft 2, on which is assembled Gear 3, which with its rotation power rotates over Gear 4 assembled on the Shaft 9, Rotor 5.
The Rotor 5 contains five compression 31ades 6, which are compressing flow of the liquid to five transfer Blades 7, which increase power of the flow already com¬ pressed liquid, and transfer to ten reactor Blades 8.
Rotor is joint together with Shaft 9, rotating in-two bearing beds 10, positioned in front gear housing 11, and rear bearing housing 12, connected to the Jet Body 1, with support Ribs 13.
On the Sheet 2/2 are shown blades of the Hydro Jet, invented, designed and construc ed by George Branko Skrinjer.
PIG. 1 - 3 is side elevation of the blades, which shows the shape of each blade. PIG. 1 - 6 is horizontal section of the blades, which shows shape of the blade section and degree with axial line.