US 11,956,063 B2
Engine control system
Randall Benjamin King, West Chester, OH (US); and Matthew Krupnick, West Chester, OH (US)
Assigned to General Electric Company, Schenectady, NY (US)
Filed by General Electric Company, Schenectady, NY (US)
Filed on Nov. 16, 2020, as Appl. No. 17/098,955.
Claims priority of provisional application 62/935,433, filed on Nov. 14, 2019.
Prior Publication US 2021/0152237 A1, May 20, 2021
Int. Cl. H04B 7/185 (2006.01); H04W 88/06 (2009.01)
CPC H04B 7/18506 (2013.01) [H04W 88/06 (2013.01)] 21 Claims
OG exemplary drawing
 
1. An electronic engine control system comprising:
a first processor positioned at a first location in an aircraft engine under an engine cowl, in communication with an aircraft data loader, and programmable by the aircraft data loader according to a file;
a second processor positioned at a second location apart from the first location in the aircraft engine under the engine cowl and programmable by the first processor according to the file; and
a wired connection between the first processor and the second processor, the wire connection to transfer the file between the first processor and the second processor without opening the engine cowl.