Russell E Randall

US Patent:

6601642, Aug 5, 2003

Filed:

Aug 9, 2002

Appl. No.:

10/064725

Inventors:

Russell E. Randall - Tarpon Springs FL

Assignee:

Future Flows, Inc. - Clearwater FL

International Classification:

F28F 500

US Classification:

165 86, 165185, 99483

Abstract:

A device for thawing frozen food requires no electrical energy consumption. A frozen food item is supported by a metallic bottom part and a metallic top part overlies the food item so that the food item is held in sandwiched relation between the top and bottom parts. The distance between the top part and the bottom part is vertically adjustable to accommodate frozen food items of differing sizes. A plurality of heat transfer fins are integrally formed in the top part and deliver heat from the ambient environment into the food item. A second embodiment includes fins on the bottom part as well. Moisture created by the thawing drains away from the food item under the influence of gravity.

US Patent:

20210253238, Aug 19, 2021

Filed:

Oct 26, 2020

Appl. No.:

17/080472

Inventors:

- BOCA RATON FL, US
RUSSELL RANDALL - LAND O LAKES FL, US

International Classification:

B64C 29/02
B64C 39/06

Abstract:

An aircraft capable of Vertical Take-Off and Landing (VTOL) and traverse flight. The aircraft generally includes a fixed outer structure including at least a generally cylindrical wing having an internal body situated within the fixed outer structure. A space is defined between the internal body and the fixed outer structure. Within this space are one or more rotatable ring impellers that create(s) thrust sufficient to achieve lift for the aircraft.

US Patent:

20200062385, Feb 27, 2020

Filed:

Oct 21, 2019

Appl. No.:

16/659265

Inventors:

- Boynton Beach FL, US
RUSSELL RANDALL - LAND O LAKES FL, US

International Classification:

B64C 29/02
B64C 39/06

Abstract:

An aircraft capable of Vertical Take-Off and Landing (VTOL) and traverse flight. The aircraft generally includes a fixed outer structure including at least a generally cylindrical wing having an internal body situated within the fixed outer structure. A space is defined between the internal body and the fixed outer structure. Within this space are one or more rotatable ring impellers that create(s) thrust sufficient to achieve lift for the aircraft.