IP Library Granted Patent US 10,626,726
Granted Patent B2
US 10,626,726 · App. 15/742,444 · Granted Apr 21, 2020

Tubular adhesion turbine or pump

Inventor: Darrell Ford (Spruce Grove, CA)
F01D1/36F04D5/001F04D17/161F04D29/0473F04D29/057F05D2220/31Y02T50/672
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Quick Facts
Patent No.
US 10,626,726
App. No.
15/742,444
Granted
Apr 21, 2020
Kind
B2
Abstract

A boundary layer turbine having a housing with an inlet that receives pressurized fluid, a rotatable shaft extending through the housing, nested cylindrical tubes of progressively wider diameter connected coaxially about the shaft wherein adjacent tubes define a cylindrical fluid passageway there-between that is in fluid communication with the inlet and an outlet, and at least one nozzle coupled to the inlet configured to direct the flow of fluid from the inlet into the plurality of passageways and against the plurality of tubes at an angle to a normal plane to the curvature of the plurality of tubes and at an angle to the longitudinal axis of the shaft, wherein the angled flow of fluid imparts rotation to the plurality of tubes and the shaft and flows towards the outlet where the fluid is discharged, and wherein the rotating shaft may be used to provide kinetic energy.

Claims (15)

1. A boundary layer or adhesion turbine comprising:

a. a housing having an inlet end with an inlet and an outlet end with an outlet, the inlet being suitable for receiving a flow of pressurized fluid into the housing;

b. a shaft extending longitudinally through the housing from the inlet end to the outlet end and journaled for rotation relative to the housing about a longitudinal axis of the shaft;

c. a plurality of nested cylindrical tubes of progressively wider diameter arranged coaxially about the shaft and connected to the shaft such that adjacent tubes define a cylindrical fluid passageway there-between that is in fluid communication with the inlet and the outlet, thereby the plurality of tubes define a plurality of passageways;

d. at least one nozzle coupled to the inlet configured to direct the flow of fluid from the inlet into the plurality of passageways and against the plurality of tubes at an angle to a normal plane to the curvature of the plurality of tubes and at an angle to the longitudinal axis of the shaft, wherein the angled flow of fluid imparts rotation to the plurality of tubes and the shaft and flows towards the outlet where the fluid is discharged, and wherein the rotating shaft may be used to provide kinetic energy, and

e. a disc member coaxially connected to the shaft and connected to the plurality of tubes at the outlet end, the disc member including a plurality of exhaust ports in fluid communication with the passageways to allow fluid flow from the passageways to the outlet.

2. The apparatus as claimed in claim 1 wherein each tube of the plurality of tubes is shorter than the adjacent tube more proximal to the shaft such that the ends of the plurality of tubes near the inlet end are stepped towards the outlet end such that the plurality of passageways are likewise stepped such that the longest passageway is adjacent the shaft and the shortest passageway is furthest coaxially from the shaft.

3. The apparatus as claimed in claim 2 wherein the inlet includes a stepped wall portion that is closely complementary to the plurality of tubes such that each step of the wall portion is in close proximity to a portion of the adjacent tube, and the stepped wall and the inlet define a pressure chamber there-between.

4. The apparatus as claimed in any one of claims 1 - 3 wherein the at least one nozzle comprises a plurality of fluid jets, each fluid jet is adjacent one passageway of the plurality of passageways and operable to direct a jet of fluid from the inlet into said one passageway to impart rotation to the plurality of tubes.

5. The apparatus as claimed in claim 4 further comprising a plurality of second jets, each second jet being on a step of the wall portion and in close proximity to an adjacent tube to direct a second jet of fluid directly against a portion of the adjacent tube to create a fluid bearing seal between that step and the portion of the adjacent tube.

6. The apparatus as claimed in claim 4 wherein each fluid jet is operable to direct the jet of fluid into said one passageway at an angle to a normal plane to the curvature of the plurality of tubes and at an angle to the longitudinal axis of the shaft.

7. The apparatus as claimed in claim 1 wherein each tube of the plurality of tubes is shorter than the adjacent tube such that the ends of the plurality of tubes are stepped in such that the plurality of passageways are likewise stepped.

8. The apparatus as claimed in claim 7 wherein the inlet port includes a stepped wall portion that is closely complementary to the plurality of tubes such that each step of the wall portion is in close proximity to a portion of the adjacent tube, and the stepped wall and the inlet define a pressure chamber there-between.

9. The apparatus as claimed in any one of claims 7 - 8 wherein the at least one nozzle comprises a plurality of fluid jets, each fluid jet is adjacent one passageway of the plurality of passageways and operable to direct a jet of fluid from the inlet into said one passageway to impart rotation to the plurality of tubes.

10. The apparatus as claimed in claim 9 further comprising a plurality of second jets, each second jet being on a step of the wall portion and in close proximity to an adjacent tube to direct a second jet of fluid directly against a portion of the adjacent tube to create a fluid bearing seal between that step and the portion of the adjacent tube.

Assignments (1)
CHANGE OF NAME Recorded Aug 15, 2019
From: BOUNDARY TURBINES INC.
To: BOUNDARY ENERGY INC.
Reel/Frame 050064/0324 →
Continuity (2)
Provisional Application 62190352 · Jul 9, 2015
Related Publication 20180216463A1 · Aug 2, 2018