COMBINED CYCLE PROPULSION SYSTEM

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20160010485A1
SERIAL NO

14790445

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Abstract

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A combined cycle propulsion system includes a low-speed propulsion engine and a high-speed propulsion engine that has a compression zone. A non-propulsion turbine is connected with the compression zone. An accessory drive gearbox is mechanically coupled with the low-speed engine and mechanically coupled with the non-propulsion turbine. For example, the low-speed propulsion engine is a turbine engine and the high-speed propulsion engine is a ramjet or scramjet engine.

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Patent Owner(s)

Patent OwnerAddress
AEROJET ROCKETDYNE INCP O BOX 13222 SACRAMENTO CA 95813-6000

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bulman, Melvin J Fair Oaks, US 34 300
Siebenhaar, Adam Shingle Springs, US 2 18
Volkmann, Jon Simi Valley, US 1 2

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