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:
Sep. 19, 2017

Filed:

Jun. 03, 2014
Applicant:

Hamilton Sundstrand Corporation, Charlotte, NC (US);

Inventors:

Clifford G. Stevens, Rockton, IL (US);

Kenneth Kramer, Byron, IL (US);

Assignee:

Hamilton Sundstrand Corporation, Charlotte, NC (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64F 1/34 (2006.01); H02J 1/00 (2006.01); H02H 1/00 (2006.01); H02H 1/06 (2006.01); H02H 11/00 (2006.01);
U.S. Cl.
CPC ...
B64F 1/34 (2013.01); H02H 1/0007 (2013.01); H02H 1/06 (2013.01); H02H 11/006 (2013.01); H02J 1/00 (2013.01);
Abstract

An external power supply system for an aircraft includes a power receptacle configured to connect to an external power source to provide external power, a power switch operative to switch between a battery power source and the external power source, and a voltage check system configured to prevent at least one of under-voltage or over-voltage of an aircraft electrical system. The voltage check system includes a voltage relay sensor configured to determine if the external power is within a suitable voltage range and a check switch operatively connected to the voltage relay sensor, wherein if the external power is within a suitable voltage range, the voltage relay sensor activates the check switch to allow external power to the aircraft electrical system, and wherein if the external power is outside the suitable voltage range, then the voltage relay sensor does not allow power to the aircraft electrical system.


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