This invention relates to means and a method for cooling the walls of combustion chambers or of other highly heated cylinders or containers. The invention is designed to replace or supplement the usual means of cooling by water jackets or by other cooling applications externally of the cylinder, as such external applications have been found impractical under very high temperature conditions and particularly when used in continuous combustion apparatus. It is the object of my invention to provide means for cooling a combustion chamber or similar container by injecting a cooling fluid directly into the container and adjacent a wall or walls thereof. A further object is to inject the cooling fluid at such angles and in such manner that it will...
All over the world, rocket engine design engineers are faced with an ever increasing demand for high...
In the combustion chamber, temperatures up to 2000K are reached, which exceeds by far the melting po...
Apparatus for controlled low NO.sub.x combustion. First and second combustion zones are provided, ea...
This invention relates to the cooling of the outer wall of a combustion chamber or other highly heat...
This invention relates to apparatus for use in effecting the combustion of a mixture of a liquid fue...
This invention relates to a combustion chamber particularly designed for use in rockets, rocket plan...
This invention relates to a combustion chamber particularly adapted for use in the propulsion of roc...
The peak cold-wall heating rate generated in a combustion chamber of a scram-jet engine can exceed 2...
A heat transfer method and apparatus are disclosed for transferring heat across a cylinder surface, ...
HEATS is a lay-out tool for the determination of transient wall heat flux to a transpiration-cooled ...
Rotary combustion device (1) with rotary combustion chamber (4). Specific measures are taken to prov...
Rocket combustion chamber walls are exposed to the high-temperature environment caused by the combus...
HEATS is a lay-out tool for the determination of transient wall heat flux to a transpiration-cooled...
International audienceNumerical simulations in a gas turbine Swirl stabilized combustor were conduct...
The objective of this thesis is to compare various methods of combustor wall cooling and their effec...
All over the world, rocket engine design engineers are faced with an ever increasing demand for high...
In the combustion chamber, temperatures up to 2000K are reached, which exceeds by far the melting po...
Apparatus for controlled low NO.sub.x combustion. First and second combustion zones are provided, ea...
This invention relates to the cooling of the outer wall of a combustion chamber or other highly heat...
This invention relates to apparatus for use in effecting the combustion of a mixture of a liquid fue...
This invention relates to a combustion chamber particularly designed for use in rockets, rocket plan...
This invention relates to a combustion chamber particularly adapted for use in the propulsion of roc...
The peak cold-wall heating rate generated in a combustion chamber of a scram-jet engine can exceed 2...
A heat transfer method and apparatus are disclosed for transferring heat across a cylinder surface, ...
HEATS is a lay-out tool for the determination of transient wall heat flux to a transpiration-cooled ...
Rotary combustion device (1) with rotary combustion chamber (4). Specific measures are taken to prov...
Rocket combustion chamber walls are exposed to the high-temperature environment caused by the combus...
HEATS is a lay-out tool for the determination of transient wall heat flux to a transpiration-cooled...
International audienceNumerical simulations in a gas turbine Swirl stabilized combustor were conduct...
The objective of this thesis is to compare various methods of combustor wall cooling and their effec...
All over the world, rocket engine design engineers are faced with an ever increasing demand for high...
In the combustion chamber, temperatures up to 2000K are reached, which exceeds by far the melting po...
Apparatus for controlled low NO.sub.x combustion. First and second combustion zones are provided, ea...