Rocket motor
First Claim
7. IN A ROCKET MOTOR CASING MEANS, OUTLET NOZZLE MEANS AT ONE END OF THE CASING MEANS, SOLID FUEL IN THE CASING MEANS HAVING A PASSAGE THERETHROUGH DEFINING A CHAMBER, INJECTOR MEANS FOR INJECTING OXIDANT INTO THE COMBUSTION CHAMBER, PUMP MEANS HAVING AN OUTLET, A TURBINE DISC ROTATABLY MOUNTED IN THE SAID PASSAGE INTERMEDIATE THE LENGTH THEREOF AND COUPLED TO THE PUMP MEANS, THAT POSITION OF THE PASSAGE UPSTREAM OF THE TURBINE MEANS CONSTITUTING AN ANTE-CHAMBER AND THAT PORTION OF THE PASSAGE DOWNSTREAM OF THE TURBINE CONSTITUTING A COMBUSTION CHAMBER, A HOLLOW STATOR STRUCTURE SURROUNDING THE TURBINE DISC, COOLING MEANS IMMEDIATELY UPSTREAM OF SAID STATOR STRUCTURE, AND PIPE MEANS PROVIDING COMMUNICATION BETWEEN THE OUTLET OF THE PUMP MEANS, THE COOLING MEANS, AND THE INJECTOR MEANS.
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Accused Products
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Citations
7 Claims
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7. IN A ROCKET MOTOR CASING MEANS, OUTLET NOZZLE MEANS AT ONE END OF THE CASING MEANS, SOLID FUEL IN THE CASING MEANS HAVING A PASSAGE THERETHROUGH DEFINING A CHAMBER, INJECTOR MEANS FOR INJECTING OXIDANT INTO THE COMBUSTION CHAMBER, PUMP MEANS HAVING AN OUTLET, A TURBINE DISC ROTATABLY MOUNTED IN THE SAID PASSAGE INTERMEDIATE THE LENGTH THEREOF AND COUPLED TO THE PUMP MEANS, THAT POSITION OF THE PASSAGE UPSTREAM OF THE TURBINE MEANS CONSTITUTING AN ANTE-CHAMBER AND THAT PORTION OF THE PASSAGE DOWNSTREAM OF THE TURBINE CONSTITUTING A COMBUSTION CHAMBER, A HOLLOW STATOR STRUCTURE SURROUNDING THE TURBINE DISC, COOLING MEANS IMMEDIATELY UPSTREAM OF SAID STATOR STRUCTURE, AND PIPE MEANS PROVIDING COMMUNICATION BETWEEN THE OUTLET OF THE PUMP MEANS, THE COOLING MEANS, AND THE INJECTOR MEANS.
Specification
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Current AssigneeAndre Vilet
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Original AssigneeAndre Vilet
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InventorsANDRE VILET
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Application NumberUS04/460,691Time in Patent Office797 DaysField of SearchUS Class Current60/251CPC Class CodesF02K 9/72 using liquid and solid prop...
