Jay Haskin

US Patent:

20180320543, Nov 8, 2018

Filed:

Jun 7, 2018

Appl. No.:

16/002620

Inventors:

Jay HASKIN - Bryan TX, US

International Classification:

F01D 15/12
F01D 5/22
F01D 25/16
F01D 25/24
F04D 25/02

Abstract:

A power transmission system for use with a turbine, a turbocharger, or a compressor has a housing, a first shaft mounted within the housing, a second shaft rotatably mounted within the housing and positioned exterior of the first shaft, a second set of blades affixed to the first shaft, and a second set of blades affixed to the second shaft. The first set of blades is positioned adjacent to the second set of blades. The first set of blades are rotatable in a direction opposite to the second shaft and the second set of blades. A shroud is affixed to an outer periphery of one of the sets of blades so as to have a portion overlying at least a portion of an outer periphery of the other of the first and second sets of blades. A power receiver is driven by the second shaft so as to convert rotational energy of the second shaft into energy or motion.

US Patent:

20180119562, May 3, 2018

Filed:

Aug 16, 2017

Appl. No.:

15/678769

Inventors:

Jay HASKIN - Bryan TX, US

International Classification:

F01D 15/12
F01D 5/02
F01D 25/16

Abstract:

A power transmission for a turbine or a compressor has a housing, a first shaft rotatably mounted so as to be rotatable in one direction in the housing, a barrel rotatably mounted so as to be rotatable in a direction opposite to that of the first shaft within the housing, a first plurality of blades affixed to the first shaft and extending radially outwardly therefrom, and a second plurality of blades affixed to the barrel and extending inwardly therefrom. Each blade of the second plurality of blades is interposed between adjacent blades of the first plurality of blades. A second shaft is mounted exterior of the housing so as to drive the barrel in rotation.

US Patent:

20150369250, Dec 24, 2015

Filed:

Jun 19, 2014

Appl. No.:

14/308899

Inventors:

Jay HASKIN - Bryan TX, US

International Classification:

F04D 19/02

Abstract:

A turbine apparatus has a main shaft, a first set of blades mounted to the main shaft, a second set of blades, and a barrel affixed to a periphery of the second set of blades. The barrel is rotatably mounted independent of a rotation of the main shaft. The barrel and the second set of blades rotates in a direction opposite to the direction of rotation of the first set of blades and the main shaft. A third set of blades is mounted to the main shaft such that the second set of blades is interposed between the first and third sets of blades. An outer shell extends over and an outer surface of the barrel such that the barrel is rotatable interior of the outer shell.