Combustion apparatus
US4315405A · kind A · utility
20Cited by
3References
4Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Nov 28, 1979 |
| Grant date | Feb 16, 1982 |
| Priority date | — |
| Expiry date | Nov 28, 1999 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF23R3/04
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
The airflow into a gas turbine engine combustion chamber e.g. through the primary air inlet and the dilution air inlets is directionally controlled by airflow directing inserts located in the air inlets. The inserts preferably comprise an open-ended cellular honeycomb structure.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.