NOZZLE ARRANGEMENT FOR AN ENGINE

Number of patents in Portfolio can not be more than 2000

United States of America Patent

APP PUB NO 20150101337A1
SERIAL NO

14296628

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ATTORNEY / AGENT: (SPONSORED)

Importance

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Abstract

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A nozzle arrangement for an engine that is operable in both an air-breathing mode, in which the engine combusts air taken in from atmosphere with hydrogen from a store thereof, and in a rocket mode, in which the engine combusts oxygen from a store thereof with hydrogen from the store thereof. The nozzle arrangement may include a rocket combustion chamber fluidly coupled by a rocket throat to a rocket nozzle. The rocket nozzle includes a first portion adjacent the rocket throat and a second portion remote from the rocket throat and axially moveable relative to the first portion between a rocket position in which they form a substantially contiguous rocket nozzle and an air-breathing position in which they overlap to define an annular throat therebetween. The nozzle arrangement may also include at least one air-breathing combustion chamber arranged to be fluidly coupled to the annular throat when the first and second portions of the nozzle are in the air-breathing position.

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First Claim

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Patent Owner(s)

Patent OwnerAddress
REACTION ENGINES LTDINNOVATION CENTRE CULHAM SCIENCE CENTRE ABINGDON OXFORDSHIRE OX14 3DB

International Classification(s)

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Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bond, Alan Abingdon, GB 17 87
Webber, Helen Abingdon, GB 1 1

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