The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Feb. 28, 2023

Filed:

Apr. 16, 2021
Applicant:

The Boeing Company, Chicago, IL (US);

Inventors:

John Behrens, Torrance, CA (US);

Craig Alan Christy, Seal Beach, CA (US);

Andrew Ian Mactavish, Palos Verdes Estates, CA (US);

Kevin Nemeth, Redondo Beach, CA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64G 1/10 (2006.01); B67D 7/36 (2010.01); B67D 7/02 (2010.01); B64G 1/64 (2006.01);
U.S. Cl.
CPC ...
B64G 1/1078 (2013.01); B67D 7/0294 (2013.01); B67D 7/36 (2013.01); B64G 1/646 (2013.01);
Abstract

A transfer system for supplying a receiving tank of a receiving spacecraft with a supply gas from a supply spacecraft. A transfer tank is disposed on the supply spacecraft and configured to retain a supply gas. A transfer line is coupled to the transfer tank, and one end thereof may be coupled to the receiving tank. A transfer valve is operatively coupled to the transfer line. A heating system is thermally coupled to the transfer tank. A control system is operatively coupled to the transfer valve and the heating system. The control system is operable to cause a transfer quantity of the supply gas to be heated, and to open the transfer valve, such that a difference between the increased pressure of the supply gas in the transfer tank and a pressure in the receiving tank causes the transfer quantity of the supply gas to flow to the receiving tank.


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