Apparatus for testing heat-insulating tubular member

Thermal measuring and testing – Thermal testing of a nonthermal quantity – Of susceptibility to thermally induced deteriouration – flaw,...

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731181, 738659, G01N 360, G01N 1700

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active

048345504

ABSTRACT:
An apparatus for testing a heat-insulating tubular member having at least one tubular portion comprising a combustion chamber connected to the tubular portion, a burner mounted in each combustion chamber, and an air line and a fuel supply line both connected to the burner. It may further comprise an air line for increasing exhaust gas pressure which opens on the inner wall of the combustion chamber near the burner.

REFERENCES:
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patent: 3478580 (1969-11-01), Siemietkowski et al.
patent: 3479882 (1969-11-01), Pospisil et al.
patent: 3534597 (1970-10-01), Webb
patent: 3667914 (1972-06-01), Penquite
patent: 3969932 (1976-07-01), Rieger et al.
patent: 4510807 (1985-04-01), Tokutake et al.
Drummond, "Simulated Rocket Engine Dynamic Force-Pressure Measurment System"; Proceedings of the 15th Int. ISA AeroSpace Insdrum. Symposium, Las Vegas, Nev., May 1969, pp. 10-17.

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