F23R - Definition fr

Definition statement

This subclass covers:

Combustion chambers that are specially adapted for generation of gaseous combustion products of high pressure or high velocity, and therefore suitable for use as a source of motive power rather than merely a source of heat. Examples of such special adaptations are:

Methods of combustion in combustion chambers that are specially adapted for generation of combustion products of high pressure or high velocity.

Relationship between large subject matter areas

This subclass is to be seen as an application place in relation to the function-oriented aspects covered by other subclasses of F23. If a method or apparatus is of general interest for combustion it should be classified in other subclasses of F23, for example subclasses F23C(Methods or apparatus for combustion using fluent fuel) and F23D(Burners). If a detail is of general interest for combustion apparatus it should also be classified in other subclasses of F23, for example subclasses F23K(Feeding fuel to combustion apparatus) or F23N(Regulating or controlling combustion). It is sometimes difficult to decide whether an apparatus or a detail is specially adapted or not. In doubtful situations classification should therefore be made in both this subclass and other subclasses of F23.

This subclass covers the configuration of single combustion chambers or flame tubes, or the mutual (for example annular) arrangement of several combustion chambers or flame tubes. The incorporation or arrangement of combustion chambers within a power plant is classified in the place for the power plant as a whole, for example in subclasses F02C(Gas-turbine plants) or F02K(Jet-propulsion plants).

When the control of the combustion is integrated in the control system of an entire power plant it is classified in the place for the control system as a whole, for example in groups F02C 9/00 or F02K 3/08.

References relevant to classification in this subclass

This subclass does not cover:

Fluidised bed combustion chambers specially adapted for operation at superatmospheric pressures

F23C 10/16

Examples of places where the subject matter of this subclass is covered when specially adapted, used for a particular purpose, or incorporated in a larger system:

Combined gas-turbine and steam-turbine plants

F01K 23/00

Gas-turbine plants

F02C

e.g.

F02C 3/14, F02C 5/02

Combustion-product positive-displacement engine plants

F02G

Jet-propulsion plants

F02K

e.g.

F02K 3/10

Combustion chambers for rocket engine plants, i.e. plants carrying both fuel and oxidant therefor

F02K 9/00

Starting of engines by supplying pressure fluid generated directly by combustion

F02N 9/02

Informative references

Attention is drawn to the following places, which may be of interest for search:

Generation of pressure gas by chemical means

C06D 5/00

Gas turbines

F01D

Combustion chambers for internal-combustion engines, combustion in internal-combustion engines

F02B

Cooling of gas turbine plants

F02C 7/12

Mounting or supporting of gas turbine plants, accommodating heat expansion or creep in gas turbine plants

F02C 7/20

Arrangement of seals in gas turbine plants

F02C 7/28

Cylinders for combustion engines

F02F 1/00

Supplying combustion engines in general with combustible mixtures or constituents thereof

F02M

Steam generation using combustion under pressure substantially exceeding atmospheric pressure

F22B 1/22

Methods or apparatus for combustion using fluent fuel in general

F23C

Air supply to combustion chambers in general

F23C 7/00, F23L

Burners in general

F23D

Feeding fuel to combustion apparatus in general

F23K

Details of combustion chambers in general

F23M

e.g. walls

F23M 5/00

Regulating or controlling combustion in general

F23N

Igniting

F23Q

Glossary of terms

In this subclass, the following terms or expressions are used with the meaning indicated:

Flame tube

The portion of a combustion chamber downstream of the zone where fuel and primary air are mixed.