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Symbol IPC-Stellen auswählen Titel
A
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HUMAN NECESSITIES
B
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PERFORMING OPERATIONSTRANSPORTING
C
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CHEMISTRYMETALLURGY
D
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TEXTILESPAPER
E
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FIXED CONSTRUCTIONS
F
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MECHANICAL ENGINEERINGLIGHTINGHEATINGWEAPONSBLASTING
F01
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ENGINES OR PUMPS
F01
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MACHINES OR ENGINES IN GENERALENGINE PLANTS IN GENERALSTEAM ENGINES
F02
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COMBUSTION ENGINESHOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
F02B
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INTERNAL-COMBUSTION PISTON ENGINESCOMBUSTION ENGINES IN GENERAL (cyclically operating valves therefor F01L; lubricating internal-combustion engines F01M; gas-flow silencers or exhaust apparatus therefor F01N; cooling of internal-combustion engines F01P; internal-combustion turbines F02C; plants in which engines use combustion products F02C, F02G)
F02C
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GAS-TURBINE PLANTSAIR INTAKES FOR JET-PROPULSION PLANTSCONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; combustion apparatus in which combustion takes place in a fluidised bed of fuel or other particles F23C 10/00; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B 11/00; using gas-turbine plants in vehicles, see the relevant vehicle classes)
F02D
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CONTROLLING COMBUSTION ENGINES (vehicle fittings, acting on a single sub-unit only, for automatically controlling vehicle speed B60K 31/00; conjoint control of vehicle sub-units of different type or different function, road vehicle drive control systems for purposes other than the control of a single sub-unit B60W; cyclically operating valves for combustion engines F01L; controlling combustion engine lubrication F01M; cooling internal-combustion engines F01P; supplying combustion engines with combustible mixtures or constituents thereof, e.g. carburettors, injection pumps, F02M; starting of combustion engines F02N; controlling of ignition F02P; controlling gas-turbine plants, jet-propulsion plants, or combustion-product engine plants, see the relevant subclasses for these plants) [4, 2006.01]
F02F
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CYLINDERS, PISTONS, OR CASINGS FOR COMBUSTION ENGINESARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES (specially adapted for rotary-piston or oscillating-piston internal-combustion engines F02B; specially adapted for gas-turbine plants F02C; specially adapted for jet-propulsion plants F02K) [2]
F02G
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HOT-GAS OR COMBUSTION-PRODUCT POSITIVE-DISPLACEMENT ENGINE PLANTS (steam engine plants, special vapour plants, plants operating on either hot gas or combustion-product gases together with other fluid F01K; gas-turbine plants F02C; jet-propulsion plants F02K)USE OF WASTE HEAT OF COMBUSTION ENGINES, NOT OTHERWISE PROVIDED FOR
F02K
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JET-PROPULSION PLANTS (arrangement or mounting of jet-propulsion plants in land vehicles or vehicles in general B60K; arrangement or mounting of jet-propulsion plants in waterborne vessels B63H; controlling aircraft attitude, flight direction, or altitude by jet reaction B64C; arrangement or mounting of jet-propulsion plants in aircraft B64D; plants characterised by the power of the working fluid being divided between jet propulsion and another form of propulsion, e.g. propeller, F02B, F02C; features of jet-propulsion plants common to gas-turbine plants, air intakes or fuel supply control of air-breathing jet-propulsion plants F02C)
F02K 1/00
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Plants characterised by the form or arrangement of the jet pipe or nozzleJet pipes or nozzles peculiar thereto (rocket nozzles F02K 9/97) [1, 2006.01]
F02K 3/00
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Plants including a gas turbine driving a compressor or a ducted fan [1, 2006.01]
F02K 5/00
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Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan [1, 2006.01]
F02K 7/00
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Plants in which the working-fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fanControl thereof (rocket-engine plants F02K 9/00) [1, 2006.01]
F02K 9/00
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Rocket-engine plants, i.e. plants carrying both fuel and oxidant thereforControl thereof (chemical composition of propellants C06B, C06D) [1, 3, 2006.01]
F02K 9/08
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using solid propellants (F02K 9/72 takes precedence; using semi-solid or pulverulent propellants F02K 9/70) [3, 2006.01]
F02K 9/10
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. . Shape or structure of solid propellant charges [3, 2006.01]
F02K 9/12
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. . . made of two or more portions burning at different rates [3, 2006.01]
F02K 9/14
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. . . made from sheet-like materials, e.g. of carpet-roll type, of layered structure [3, 2006.01]
F02K 9/16
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. . . of honeycomb structure [3, 2006.01]
F02K 9/18
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. . . of the internal-burning type having a star or like shaped internal cavity [3, 2006.01]
F02K 9/20
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. . . of the external-burning type [3, 2006.01]
F02K 9/22
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. . . of the front-burning type [3, 2006.01]
F02K 9/24
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. . Charging rocket engines with solid propellantsMethods or apparatus specially adapted for working solid propellant charges [3, 2006.01]
F02K 9/26
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. . Burning control [3, 2006.01]
F02K 9/28
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. . having two or more propellant charges with the propulsion gases exhausting through a common nozzle [3, 2006.01]
F02K 9/30
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. . with the propulsion gases exhausting through a plurality of nozzles [3, 2006.01]
F02K 9/32
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. . Constructional partsDetails (shape or structure of solid propellant charges F02K 9/10; starting or ignition means or arrangements F02K 9/95; rocket nozzles F02K 9/97) [3, 2006.01]
F02K 9/34
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. . . CasingsCombustion chambersLiners thereof [3, 2006.01]
F02K 9/36
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. . . Propellant charge supports [3, 2006.01]
F02K 9/38
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. . . Safety devices, e.g. to prevent accidental ignition [3, 2006.01]
F02K 9/40
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. . . Cooling arrangements [3, 2006.01]
F02K 9/42
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using liquid or gaseous propellants (F02K 9/72 takes precedence) [3, 2006.01]
F02K 9/44
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. . Feeding propellants [3, 2006.01]
F02K 9/46
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. . . using pumps (pumps per seF04) [3, 2006.01]
F02K 9/48
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. . . . driven by a gas turbine fed by propellant combustion gases [3, 2006.01]
F02K 9/50
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. . . using pressurised fluid to pressurize the propellants [3, 2006.01]
F02K 9/52
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. . . Injectors (in general B05B) [3, 2006.01]
F02K 9/54
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. . . Leakage detectorsPurging systemsFiltration systems (filters per seB01D) [3, 2006.01]
F02K 9/56
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. . . Control [3, 2006.01]
F02K 9/58
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. . . . Propellant feed valves (valves in general F16K) [3, 2006.01]
F02K 9/60
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. . Constructional partsDetails (starting or ignition means or arrangements F02K 9/95; rocket nozzles F02K 9/97) [3, 2006.01]
F02K 9/62
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. . . Combustion or thrust chambers [3, 2006.01]
F02K 9/64
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. . . . having cooling arrangements [3, 2006.01]
F02K 9/66
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. . . . of the rotary type [3, 2006.01]
F02K 9/68
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. . . Decomposition chambers [3, 2006.01]
F02K 9/70
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using semi-solid or pulverulent propellants [3, 2006.01]
F02K 9/72
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using liquid and solid propellants, i.e. hybrid rocket-engine plants [3, 2006.01]
F02K 9/74
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combined with another jet-propulsion plant [3, 2006.01]
F02K 9/76
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. . with another rocket-engine plantMultistage rocket-engine plants [3, 2006.01]
F02K 9/78
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. . with an air-breathing jet-propulsion plant (with a ram-jet engine F02K 7/18) [3, 2006.01]
F02K 9/80
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characterised by thrust or thrust vector control (F02K 9/26, F02K 9/56, F02K 9/94 take precedence) [3, 2006.01]
F02K 9/82
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. . by injection of a secondary fluid into the rocket exhaust gases [3, 2006.01]
F02K 9/84
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. . using movable nozzles [3, 2006.01]
F02K 9/86
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. . using nozzle throats of adjustable cross-section [3, 2006.01]
F02K 9/88
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. . using auxiliary rocket nozzles [3, 2006.01]
F02K 9/90
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. . using deflectors (F02K 9/82 takes precedence) [3, 2006.01]
F02K 9/92
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. . incorporating means for reversing or terminating thrust [3, 2006.01]
F02K 9/94
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Re-ignitable or restartable rocket-engine plantsIntermittently operated rocket-engine plants [3, 2006.01]
F02K 9/95
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characterised by starting or ignition means or arrangements (safety devices F02K 9/38) [3, 2006.01]
F02K 9/96
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characterised by specially adapted arrangements for testing or measuring [3, 2006.01]
F02K 9/97
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Rocket nozzles (thrust or thrust vector control F02K 9/80) [3, 2006.01]
F02K 99/00
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Subject matter not provided for in other groups of this subclass [2009.01]
F02M
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SUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
F02N
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STARTING OF COMBUSTION ENGINES (starting of free-piston combustion-engines F02B 71/02; starting of gas-turbine plants F02C 7/26)STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
F02P
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IGNITION, OTHER THAN COMPRESSION IGNITION, FOR INTERNAL-COMBUSTION ENGINESTESTING OF IGNITION TIMING IN COMPRESSION-IGNITION ENGINES (specially adapted for rotary-piston or oscillating-piston engines F02B 53/12; ignition of combustion apparatus in general, glowing plugs F23Q; measuring of physical variables in general G01; controlling in general G05; data processing in general G06; electrical components in general, see section H; sparking plugs H01T)
F03
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MACHINES OR ENGINES FOR LIQUIDSWIND, SPRING, OR WEIGHT MOTORSPRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
F04
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POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDSPUMPS FOR LIQUIDS OR ELASTIC FLUIDS
F15
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ENGINEERING IN GENERAL
F15
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FLUID-PRESSURE ACTUATORSHYDRAULICS OR PNEUMATICS IN GENERAL
F16
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ENGINEERING ELEMENTS OR UNITSGENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONSTHERMAL INSULATION IN GENERAL
F17
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STORING OR DISTRIBUTING GASES OR LIQUIDS
F21
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LIGHTINGHEATING
F21
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LIGHTING
F22
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STEAM GENERATION
F23
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COMBUSTION APPARATUSCOMBUSTION PROCESSES
F24
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HEATINGRANGESVENTILATING
F25
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REFRIGERATION OR COOLINGCOMBINED HEATING AND REFRIGERATION SYSTEMSHEAT PUMP SYSTEMSMANUFACTURE OR STORAGE OF ICELIQUEFACTION OR SOLIDIFICATION OF GASES
F26
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DRYING
F27
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FURNACESKILNSOVENSRETORTS [4]
F28
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HEAT EXCHANGE IN GENERAL
F41
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WEAPONSBLASTING
F41
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WEAPONS
F42
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AMMUNITIONBLASTING
F99
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SUBJECT MATTER NOT OTHERWISE PROVIDED FOR IN THIS SECTION [2006.01]
G
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PHYSICS
H
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ELECTRICITY

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