Ceramic-encased hot surface igniter system for jet engines
US8434292B2 · kind B2 · utility
Assignee
Inventors
Key dates
| Filing date | Dec 17, 2007 |
| Grant date | May 7, 2013 |
| Priority date | — |
| Expiry date | Aug 27, 2031 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
A ceramic-encased hot surface igniter system for jet engines is presented. The advanced ceramic-encased hot surface igniter system comprises at least one electrical resistance heated element encased in a durable, thermal and mechanical shock resistant, high temperature advanced ceramic compound such as silicon nitride. The one or more advanced ceramic-encased hot surface igniter elements are mounted proximally upstream or within a combustion chamber of a jet engine enclosure or within the afterburner section of a jet propulsion engine's exhaust. The surface temperature of each ignition element's encasement being of sufficient temperature to cause the ignition of a gaseous, atomized, or liquid fuel.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.