Marcus Jovon Richardson

US Patent:

20230012539, Jan 19, 2023

Filed:

Aug 25, 2022

Appl. No.:

17/895725

Inventors:

- Chicago IL, US
Marcus K. Richardson - Bothell WA, US
Chao-Hsin Lin - Redmond WA, US

International Classification:

B64D 11/04
A47B 31/02
B64D 11/00
F25D 3/12

Abstract:

A galley cart system employs a dry ice compartment and a refrigeration compartment in a galley cart in flow communication with the dry ice compartment. A ventilation system is in interruptible flow communication with at least the refrigeration compartment and configured to receive gas discharged from at least the refrigeration compartment.

US Patent:

20210302216, Sep 30, 2021

Filed:

Mar 30, 2020

Appl. No.:

16/834203

Inventors:

- Chicago IL, US
Marcus Karel Richardson - Everett WA, US

International Classification:

G01F 17/00
G01N 33/00

Abstract:

A test cage and method for testing a gap formed between a wall and an insulation layer in a vehicle. The test cage includes first and second end walls and a sidewall to form an interior space. Openings extend through one or more of the first and second end walls and the sidewall. The openings are configured to allow air flow through the interior space. Two or more ports extend through the first end wall and are in communication with the interior space. Each of the ports comprises an inner end at the interior space with the inner ends spaced apart within the interior space and also spaced away from the second end wall. Hoses can be connected to the ports to provide for inputting a gas and/or testing the air within the gap.

US Patent:

20210122478, Apr 29, 2021

Filed:

Oct 28, 2019

Appl. No.:

16/665893

Inventors:

- Chicago IL, US
Marcus K. Richardson - Everett WA, US
Jacob Bevan McWhirter - Lake Stevens WA, US

International Classification:

B64D 13/08
F02C 7/32

Abstract:

Aircraft cooling and heating systems and related methods are disclosed. An example apparatus includes an air compressor operatively coupled to a turbine engine. The air compressor is configured to generate compressed air at a first temperature. A vapor cycle system configured to reduce the first temperature of the compressed air provided by the air compressor to a second temperature that is less than the first temperature.

US Patent:

20200140093, May 7, 2020

Filed:

Nov 5, 2018

Appl. No.:

16/181197

Inventors:

- Chicago IL, US
Marcus Karel Richardson - Everett WA, US
Brian Tatsuo Imada - Fruitland ID, US
Myles Brown - Bothell WA, US
Steven Michael Loukusa - Bothell WA, US

Assignee:

The Boeing Company - Chicago IL

International Classification:

B64D 13/04
F24F 9/00

Abstract:

Systems and methods for limiting infiltration of cabin air into the flight deck of an aircraft, where the systems include at least one upper nozzle disposed adjacent to and above an outer upper edge of a flight deck doorway and directed downwardly, and at least one lower nozzle disposed adjacent to and below an outer lower edge of the flight deck doorway and directed upwardly; a conduit system to deliver air from a flight deck air supply to the upper and lower nozzles; and an airflow controller configured to provide sufficient air flow from the flight deck air supply to the upper and lower nozzles to create directional airstreams across the gaps between the closed flight deck door and the upper and lower edges of the flight deck doorway, so that the airstreams limit infiltration of cabin air into the flight deck via the gaps.

US Patent:

20190344893, Nov 14, 2019

Filed:

Jul 23, 2019

Appl. No.:

16/519658

Inventors:

- Chicago IL, US
Marcus K. Richardson - Bothell WA, US
Chao-Hsin Lin - Redmond WA, US

International Classification:

B64D 11/04
F25D 3/12
A47B 31/02
B64D 11/00

Abstract:

A galley cart system employs a dry ice compartment and a refrigeration compartment in a galley cart in flow communication with the dry ice compartment. A ventilation system is in interruptible flow communication with at least the refrigeration compartment and configured to receive gas discharged from at least the refrigeration compartment.

US Patent:

20190291873, Sep 26, 2019

Filed:

Mar 23, 2018

Appl. No.:

15/934233

Inventors:

- Chicago IL, US
Cameron Lindsay CARNEGIE - Everett WA, US
Marcus Karel RICHARDSON - Everett WA, US

International Classification:

B64D 13/06
B64C 1/06

Abstract:

An air drying system including a compressor coupled to a first air inlet through which moist air is received, a first turbine in fluid communication with the compressor and coupled to a first air outlet through which dry air is expelled, and a second turbine coupled to a second air inlet and a second air outlet and being driven, at least in part, by an air flow caused by a pressure differential between the second air inlet and the second air outlet, where the second turbine is operably coupled to the compressor and the first turbine by a drive mechanism so that rotation of the second turbine drives rotation of the compressor and the first turbine.

US Patent:

20160312809, Oct 27, 2016

Filed:

Apr 27, 2015

Appl. No.:

14/697570

Inventors:

- Chicago IL, US
Marcus K. Richardson - Bothell WA, US

International Classification:

F15D 1/00

Abstract:

An electrostatic bypass system and method as disclosed utilizes corona wires extending laterally across the flow path upstream of the section of the flow path of concern. The corona wires can be arranged to form a mesh across the flow path and can be powered by a power source to ionize the air surrounding the wires to thereby apply an electrostatic charge to the particulates as they pass through an ionized section of air proximate the wires.

US Patent:

20160270153, Sep 15, 2016

Filed:

Mar 14, 2016

Appl. No.:

15/069800

Inventors:

- Chicago IL, US
Marcus K. Richardson - Bothell WA, US
Myles E. Brown - Bothell WA, US

International Classification:

H05B 1/02
H05B 3/36
H05B 3/54

Abstract:

Described herein is a composite panel that includes a first layer made from an electrically non-conductive material. The composite panel also includes a resistance heater printed onto the first layer and a capacitive sensor applied onto the first layer. The capacitive sensor is operably coupled with the resistance heater. The composite panel additionally includes a second layer adjacent the resistance heater and the capacitive sensor. The resistance heater and the capacitive sensor are positioned between the first layer and the second layer. Furthermore, the second layer is made from an electrically non-conductive material. The resistance heater is configured to generate heat at least partially in response to input sensed by the capacitive sensor.