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Electrical System for an Aircraft Cross-reference to Related Applications
| Content Provider | Semantic Scholar |
|---|---|
| Copyright Year | 2017 |
| Abstract | (57) ABSTRACT (21) Appl. No.: 13/718,836 An electrical system for an aircraft is provided. The system 1-1. comprises an inverter for transforming a first alternating cur (22) Filed: Dec. 18, 2012 rent from an on-board network having a variable frequency O O into a second alternating current, and at least a first electrical Related U.S. Application Data load and at least a second electrical load, which are config (60) Provisional application No. 61/577,986, filed on Dec. ured to be operated simultaneously by the second alternating 20, 2011. Current. |
| File Format | PDF HTM / HTML |
| Alternate Webpage(s) | https://patentimages.storage.googleapis.com/af/bc/3e/acaf2c79d2df06/US20130154357A1.pdf |
| Language | English |
| Access Restriction | Open |
| Content Type | Text |
| Resource Type | Article |