Vehicular propulsion gas turbine motor
US4213297A · kind A · utility
Assignee
Inventors
Key dates
| Filing date | Oct 3, 1978 |
| Grant date | Jul 22, 1980 |
| Priority date | — |
| Expiry date | Oct 3, 1998 |
Classification
- Technology area (CPC F)Mechanical Engineering; Lighting; Heating
- CPC primaryF28F2250/108
- WIPO fieldEngines, pumps, turbines
- WIPO sectorMechanical engineering
Abstract
Elongated ceramic heat exchange units are arranged with each such unit axly oriented and all arranged parallel to each other in a ring surrounding the compressor, gas turbine and combustion chamber of a gas turbine motor. Each heat exchange unit has a multiplicity of rectangular slot channels through alternate ones of which the hot exhaust gas and the compressed air supply flow in counter-current. The cross sections of these channels all have their long dimension disposed substantially radially with respect to the axis of symmetry common to the principal components. The respective inputs for the two sets of channels are both from the inside of the ring arrangement but at opposite ends of each heat exchanger element; whereas the exit openings are in the end faces of the heat exchanger elements. The outlets for the compressed gas that has been heated in the heat exchanger communicate with a space that not only leads the compressed air to the compressed chamber but also allows the compressed air to reach space between the outside of the heat exchanger and an external casing, so as to cause the compressed air to apply its pressure to the heat exchanger elements tightening the seals bet…
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.