Engine exhaust gas test harness

Thermal measuring and testing – Temperature measurement – Combined with diverse art device

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Details

73116, 374115, 374143, F02B 7700, G01K 1300

Patent

active

045809100

ABSTRACT:
In the maintenance of turbine propeller aircraft and related engines, test method and apparatus to measure engine exhaust temperature and exhaust pressure, without pulling the engine. Test harness associated with instrumental Jet Calibrator is interposed between tailpipe and airframe exhaust pipe to establish the accuracy of interstage turbine temperature and exhaust gas temperature by graphic comparisons. Both engine exhaust gas temperature and exhaust pressure may also be obtained concurrently to effect "on wing" recompensation of interstage turbine temperature during test run maintenance of the engine.

REFERENCES:
patent: 3022668 (1962-02-01), Lawson et al.
patent: 3318151 (1967-05-01), Behrendt et al.
patent: 3618386 (1971-11-01), Black
patent: 3789665 (1974-02-01), Hohenberg
patent: 4115998 (1978-09-01), Gilbert et al.
patent: 4122720 (1978-10-01), Podl
patent: 4186605 (1980-02-01), Bourigault

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