| タイトル | Solar energy receiver for a Stirling engine |
| 本文（外部サイト） | http://hdl.handle.net/2060/19810008996 |
| 著者（英） | Selcuk, M. K. |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech.|NASA Pasadena Office |
| 発行日 | 1980-12-02 |
| 言語 | eng |
| 内容記述 | A solar energy receiver includes a separable endless wall formed of a ceramic material in which a cavity of substantially cylindrical configuration is defined for entrapping solar flux. An acceptance aperture is adapted to admit to the cavity a concentrated beam of solar energy. The wall is characterized by at least one pair of contiguously related segments separated by lines of cleavage intercepting the aperture. At least one of the segments is supported for pivotal displacement. A thermal-responsive actuator is adapted to respond to excessive temperatures within the cavity for initiating pivoted displacement of one segment, whereby thermal flux is permitted to escape from the cavity. |
| NASA分類 | ENERGY PRODUCTION AND CONVERSION |
| レポートNO | 81N17518 |
| 権利 | No Copyright |
