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:
Mar. 31, 2020

Filed:

Sep. 25, 2014
Applicant:

Patched Conics, Llc., Yamanashi, JP;

Inventor:

Junichiro Kawaguchi, Uenohara, JP;

Assignee:

PATCHED CONICS, LLC., Yamanashi, JP;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 9/46 (2006.01); F02K 9/50 (2006.01); F04F 13/00 (2009.01); B64G 1/26 (2006.01); B64G 1/40 (2006.01); F04B 27/00 (2006.01); F04B 39/00 (2006.01); F04B 39/06 (2006.01); F17C 7/04 (2006.01);
U.S. Cl.
CPC ...
F02K 9/46 (2013.01); B64G 1/26 (2013.01); B64G 1/402 (2013.01); F02K 9/50 (2013.01); F04B 27/00 (2013.01); F04B 39/0005 (2013.01); F04B 39/0027 (2013.01); F04B 39/06 (2013.01); F04F 13/00 (2013.01); F17C 7/04 (2013.01); F05D 2220/80 (2013.01); F17C 2201/018 (2013.01); F17C 2201/054 (2013.01); F17C 2221/011 (2013.01); F17C 2221/012 (2013.01); F17C 2221/013 (2013.01); F17C 2221/014 (2013.01); F17C 2221/033 (2013.01); F17C 2221/035 (2013.01); F17C 2221/08 (2013.01); F17C 2223/013 (2013.01); F17C 2223/0153 (2013.01); F17C 2223/0161 (2013.01); F17C 2223/035 (2013.01); F17C 2225/0123 (2013.01); F17C 2227/0142 (2013.01); F17C 2227/0302 (2013.01); F17C 2227/0309 (2013.01); F17C 2227/0376 (2013.01); F17C 2260/02 (2013.01); F17C 2270/0197 (2013.01);
Abstract

A heat exchanger generally employs a method for supplying liquid having critical pressure or higher or high pressure in order to suppress boiling. However, gas obtained by a evaporator behind the heat exchanger has relatively low pressure, and therefore supplying the liquid to the heat exchanger requires a system for converting an energy form of the obtained gas into kinetic energy or electrical energy, and increasing the pressure by a mechanical pump. Thus, the complicated system involving an efficiency loss is only solution, and it is difficult to achieve simplification of a system or reduction in the weight of a propellant supply device in a moving body, specifically, a flying object.


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