Power plants – Internal combustion engine with treatment or handling of... – Material from exhaust structure fed to engine intake
Patent
1991-10-22
1992-11-24
Bertsch, Richard A.
Power plants
Internal combustion engine with treatment or handling of...
Material from exhaust structure fed to engine intake
60223, 60259, 60 39091, F02K 996, B65D 3912
Patent
active
051652293
ABSTRACT:
A thruster nozzle sealing system and apparatus is provided for protection of spacecraft thruster motors. The system includes a sealing plug, a sealing plug insertion tool, an outer cover, an outer cover attachment, a ferry flight attachment, and a test stand. The sealing plug provents moisture from entering the thruster engine so as to prevent valve failure. The attachments are interchangeably connectable with the sealing plug. The ferry flight attachment is used during air transportation of the spacecraft, and the outer cover attachment is used during storage and service of the spacecraft. The outer cover provides protection to the thruster nozzle from mechanical damage. The test stand provides a means for testing and certifying the operating condition of each component of the system.
REFERENCES:
patent: 3372548 (1968-03-01), Mathis et al.
patent: 3693831 (1972-09-01), West
patent: 3946557 (1976-03-01), Macbeth
patent: 4773474 (1988-09-01), Stay
patent: 5007236 (1991-04-01), Myers et al.
Barr Hardie R.
Bertsch Richard A.
Fein Edward K.
Jalali L.
Miller Guy M.
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