| 摘要 |
A total air temperature sensor probe (10) samples the air stream surrounding an aircraft in flight, and includes a duct (14) carrying a fluid flow a portion of which is diverted to a primary chamber (26) mounting a total air temperature sensor (28). A secondary chamber (48) has a secondary sensor (50) for sensing a different property of a sampled air stream. The secondary chamber (48) is open to receive air flow from passageways (44) in the total air temperature probe.
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