Power plants – Reaction motor – Particular exhaust nozzle feature
Reexamination Certificate
2005-09-27
2011-11-22
Rodriguez, William H (Department: 3741)
Power plants
Reaction motor
Particular exhaust nozzle feature
C060S226100, C239S265110
Reexamination Certificate
active
08061145
ABSTRACT:
The invention relates to an arrangement for propelling an aircraft comprising a jet engine and an outlet nozzle arranged downstream of the jet engine. The jet engine is of a type which generates an internal core flow and an external fan flow. A part of the outlet nozzle has an internal surface which defines a gas duct for the fan flow. The aforementioned part of the outlet nozzle includes a wall structure that is arranged at a distance from the internal surface such that it separates the gas duct for the fan flow from an internal gas duct for the core flow.
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International Search Report for corresponding International Application PCT/SE2005/001430.
International Preliminary Report on Patentability for corresponding International Application PCT/SE2005/001430.
Rodriguez William H
Volvo Aero Corporation
WRB-IP LLP
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