F
SECTION F — MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
  
ENGINES OR PUMPS
 F01 - 
F04

Note(s)

Guide to the use of this subsection (classes F01-F04)

The following notes are meant to assist in the use of this part of the classification scheme.

  1. In this subsection, subclasses or groups designating "engines" or "pumps" cover methods of operating the same, unless otherwise specifically provided for.
  2. In this subsection, the following terms or expressions are used with the meanings indicated:
    • "engine" means a device for continuously converting fluid energy into mechanical power. Thus, this term includes, for example, steam piston engines or steam turbines, per se, or internal-combustion piston engines, but it excludes single-stroke devices. "Engine" also includes the fluid-motive portion of a meter unless such portion is particularly adapted for use in a meter;
    • "pump" means a device for continuously raising, forcing, compressing, or exhausting fluid by mechanical or other means; thus this term includes fans or blowers;
    • "machine" means a device which could equally be an engine and a pump, and not a device which is restricted to an engine or one which is restricted to a pump;
    • "positive displacement" means the way the energy of a working fluid is transformed into mechanical energy, in which variations of volume created by the working fluid in a working chamber produce equivalent displacements of the mechanical member transmitting the energy, the dynamic effect of the fluid being of minor importance; and vice versa;
    • "non-positive displacement" means the way the energy of a working fluid is transformed into mechanical energy, by transformation of the energy of the working fluid into kinetic energy; and vice versa;
    • "oscillating-piston machine" means a positive-displacement machine in which a fluid-engaging work-transmitting member oscillates. This definition applies also to engines and pumps;
    • "rotary-piston machine" means a positive-displacement machine in which a fluid-engaging work-transmitting member rotates about a fixed axis or about an axis moving along a circular or similar orbit. This definition applies also to engines and pumps;
    • "rotary piston" means the work-transmitting member of a rotary-piston machine and may be of any suitable form, e.g. like a toothed gear;
    • "cooperating members" means the "oscillating piston" or "rotary piston" and another member, e.g. the working-chamber wall, which assists in the driving or pumping action;
    • "movement of the co-operating members" is to be interpreted as relative, so that one of the "co-operating members" may be stationary, even though reference may be made to its rotational axis, or both may move;
    • "teeth or tooth equivalents" include lobes, projections or abutments;
    • "internal-axis type" means that the rotational axes of the inner and outer co-operating members remain at all times within the outer member, e.g., in a similar manner to that of a pinion meshing with the internal teeth of a ring gear;
    • "free piston" means a piston of which the length of stroke is not defined by any member driven thereby;
    • "cylinders" means positive-displacement working chambers in general and thus this term is not restricted to cylinders of circular cross-section;
    • "main shaft" means the shaft which converts reciprocating piston motion into rotary motion or vice versa;
    • "plant" means an engine together with such additional apparatus as is necessary to run the engine. For example, a steam engine plant includes a steam engine and means for generating the steam;
    • "working fluid" means the driven fluid in a pump and the driving fluid in an engine. The working fluid may be in a gaseous state, i.e. compressible, or liquid. In the former case coexistence of two states is possible;
    • "steam" includes condensable vapours in general, and "special vapour" is used when steam is excluded;
    • "reaction type" as applied to non-positive-displacement machines or engines means machines or engines in which pressure/velocity transformation takes place wholly or partly in the rotor; machines or engines with no, or only slight, pressure/velocity transformation in the rotor are called "impulse type".
  3. In this subsection:
  4. For use of this subsection with a good understanding, it is essential to remember, so far as subclasses F01B, F01C, F01D, F03B, and F04B, F04C, F04D, which form its skeleton, are concerned:

 F02
COMBUSTION ENGINES (cyclically operating valves therefor, lubricating, exhausting, or silencing engines F01); HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
 F02K
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

Note(s)

  1. In this subclass, the following expression is used with the meaning indicated:
    • "jet-propulsion plants" means plants using combustion to produce a fluid stream from which a propulsive thrust on the plants is obtained on the reaction principle.
  2. Attention is drawn to the Notes preceding class F01.
 F02K 1/00
Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto (rocket nozzles F02K 9/97)
 F02K 1/04
·  Mounting of an exhaust cone in the jet pipe
 F02K 1/06
·  Varying effective area of jet pipe or nozzle (F02K 1/30 takes precedence)  [3]
 F02K 1/08
·  ·  by axially moving or transversely deforming an internal member, e.g. the exhaust cone
 F02K 1/09
·  ·  by axially moving an external member, e.g. a shroud (F02K 1/12 takes precedence)  [3]
 F02K 1/10
·  ·  by distorting the jet pipe or nozzle
 F02K 1/11
·  ·  by means of pivoted eyelids  [3]
 F02K 1/12
·  ·  by means of pivoted flaps
 F02K 1/15
·  ·  Control or regulation  [3]
 F02K 1/16
·  ·  ·  conjointly with another control  [3]
 F02K 1/17
·  ·  ·  ·  with control of fuel supply  [3]
 F02K 1/18
·  ·  ·  automatic  [3]
 F02K 1/28
·  using fluid jets to influence the jet flow  [3]
 F02K 1/30
·  ·  for varying effective area of jet pipe or nozzle  [3]
 F02K 1/32
·  ·  for reversing thrust  [3]
 F02K 1/34
·  ·  for attenuating noise  [3]
 F02K 1/36
·  having an ejector  [3]
 F02K 1/38
·  Introducing air inside the jet (F02K 1/28 takes precedence)  [3]
 F02K 1/40
·  Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet  [3]
 F02K 1/42
·  ·  the means being movable into an inoperative position  [3]
 F02K 1/44
·  Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction (F02K 1/40 takes precedence)  [3]
 F02K 1/46
·  Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing (F02K 1/28, F02K 1/36, F02K 1/38 take precedence)  [3]
 F02K 1/48
·  ·  Corrugated nozzles  [3]
 F02K 1/50
·  ·  Deflecting outwardly a portion of the jet by retractable scoop-like baffles  [3]
 F02K 1/52
·  Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member, e.g. fairing  [3]
 F02K 1/54
·  Nozzles having means for reversing jet thrust (F02K 1/32 takes precedence)  [3]
 F02K 1/56
·  ·  Reversing jet main flow  [3]
 F02K 1/58
·  ·  ·  Reversers mounted on the inner cone or the nozzle housing  [3]
 F02K 1/60
·  ·  ·  by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers  [3]
 F02K 1/62
·  ·  ·  by blocking the rearward discharge by means of flaps  [3]
 F02K 1/64
·  ·  Reversing fan flow  [3]
 F02K 1/66
·  ·  ·  using reversing fan blades  [3]
 F02K 1/68
·  ·  ·  Reversers mounted on the engine housing downstream of the fan exhaust section  [3]
 F02K 1/70
·  ·  ·  using thrust reverser flaps or doors mounted on the fan housing  [3]
 F02K 1/72
·  ·  ·  ·  the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow  [3]
 F02K 1/74
·  ·  Reversing at least one flow in relation to at least one other flow in a plural-flow engine  [3]
 F02K 1/76
·  ·  Control or regulation of thrust reversers  [3]
 F02K 1/78
·  Other construction of jet pipes  [3]
 F02K 1/80
·  ·  Couplings or connections  [3]
 F02K 1/82
·  ·  Jet pipe walls, e.g. liners  [3]
 F02K 3/00
Plants including a gas turbine driving a compressor or a ducted fan
 F02K 3/02
·  in which part of the working fluid by-passes the turbine and combustion chamber
 F02K 3/04
·  ·  the plant including ducted fans, i.e. fans with high volume, low-pressure outputs, for augmenting jet thrust, e.g. of double-flow type
 F02K 3/06
·  ·  ·  with front fan
 F02K 3/062
·  ·  ·  with aft fan  [3]
 F02K 3/065
·  ·  ·  with front and aft fans  [3]
 F02K 3/068
·  ·  ·  being characterised by a short axial length relative to diameter  [3]
 F02K 3/072
·  ·  ·  with counter-rotating rotors  [3]
 F02K 3/075
·  ·  ·  controlling flow ratio between flows  [3]
 F02K 3/077
·  ·  ·  the plant being of the multiple flow type, i.e. having three or more flows  [3]
 F02K 3/08
·  with supplementary heating of the working fluid (after-burners, combustion chambers per se F23R); Control thereof (control of fuel supply therefor F02C 9/26)  [3]
 F02K 3/10
·  ·  by after-burners (F02K 3/105 takes precedence)  [3]
 F02K 3/105
·  ·  Heating the by-pass flow  [3]
 F02K 3/11
·  ·  ·  by means of burners or combustion chambers  [3]
 F02K 3/115
·  ·  ·  by means of indirect heat exchange  [3]
 F02K 3/12
·  characterised by having more than one gas turbine
 F02K 5/00
Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan
 F02K 5/02
·  the engine being of the reciprocating-piston type
 F02K 7/00
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 fan; Control thereof (rocket-engine plants F02K 9/00)
 F02K 7/02
·  the jet being intermittent, i.e. pulse jet
 F02K 7/04
·  ·  with resonant combustion chambers
 F02K 7/06
·  ·  with combustion chambers having valves
 F02K 7/067
·  ·  ·  having aerodynamic valves  [3]
 F02K 7/075
·  ·  with multiple pulse-jet engines  [3]
 F02K 7/08
·  the jet being continuous
 F02K 7/10
·  characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
 F02K 7/12
·  ·  Injection-induction jet engines  [3]
 F02K 7/14
·  ·  with external combustion, e.g. scram-jet engines  [3]
 F02K 7/16
·  ·  Composite ram-jet/turbo-jet engines  [3]
 F02K 7/18
·  ·  Composite ram-jet/rocket engines  [3]
 F02K 7/20
·  ·  Composite ram-jet/pulse-jet engines  [3]
 F02K 9/00
Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof (chemical composition of propellants C06B, C06D)  [3]
 F02K 9/08
·  using solid propellants (F02K 9/72 takes precedence; using semi-solid or pulverulent propellants F02K 9/70)  [3]
 F02K 9/10
·  ·  Shape or structure of solid propellant charges  [3]
 F02K 9/12
·  ·  ·  made of two or more portions burning at different rates  [3]
 F02K 9/14
·  ·  ·  made from sheet-like materials, e.g. of carpet-roll type, of layered structure  [3]
 F02K 9/16
·  ·  ·  of honeycomb structure  [3]
 F02K 9/18
·  ·  ·  of the internal-burning type having a star or like shaped internal cavity  [3]
 F02K 9/20
·  ·  ·  of the external-burning type  [3]
 F02K 9/22
·  ·  ·  of the front-burning type  [3]
 F02K 9/24
·  ·  Charging rocket engines with solid propellants; Methods or apparatus specially adapted for working solid propellant charges  [3]
 F02K 9/26
·  ·  Burning control  [3]
 F02K 9/28
·  ·  having two or more propellant charges with the propulsion gases exhausting through a common nozzle  [3]
 F02K 9/30
·  ·  with the propulsion gases exhausting through a plurality of nozzles  [3]
 F02K 9/32
·  ·  Constructional parts; Details (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]
 F02K 9/34
·  ·  ·  Casings; Combustion chambers; Liners thereof  [3]
 F02K 9/36
·  ·  ·  Propellant charge supports  [3]
 F02K 9/38
·  ·  ·  Safety devices, e.g. to prevent accidental ignition  [3]
 F02K 9/40
·  ·  ·  Cooling arrangements  [3]
 F02K 9/42
·  using liquid or gaseous propellants (F02K 9/72 takes precedence)  [3]
 F02K 9/44
·  ·  Feeding propellants  [3]
 F02K 9/46
·  ·  ·  using pumps (pumps per se F04)  [3]
 F02K 9/48
·  ·  ·  ·  driven by a gas turbine fed by propellant combustion gases  [3]
 F02K 9/50
·  ·  ·  using pressurised fluid to pressurize the propellants  [3]
 F02K 9/52
·  ·  ·  Injectors (in general B05B)  [3]
 F02K 9/54
·  ·  ·  Leakage detectors; Purging systems; Filtration systems (filters per se B01D)  [3]
 F02K 9/56
·  ·  ·  Control  [3]
 F02K 9/58
·  ·  ·  ·  Propellant feed valves (valves in general F16K)  [3]
 F02K 9/60
·  ·  Constructional parts; Details (starting or ignition means or arrangements F02K 9/95; rocket nozzles F02K 9/97)  [3]
 F02K 9/62
·  ·  ·  Combustion or thrust chambers  [3]
 F02K 9/64
·  ·  ·  ·  having cooling arrangements  [3]
 F02K 9/66
·  ·  ·  ·  of the rotary type  [3]
 F02K 9/68
·  ·  ·  Decomposition chambers  [3]
 F02K 9/70
·  using semi-solid or pulverulent propellants  [3]
 F02K 9/72
·  using liquid and solid propellants, i.e. hybrid rocket-engine plants  [3]
 F02K 9/74
·  combined with another jet-propulsion plant  [3]
 F02K 9/76
·  ·  with another rocket-engine plant; Multistage rocket-engine plants  [3]
 F02K 9/78
·  ·  with an air-breathing jet-propulsion plant (with a ram-jet engine F02K 7/18)  [3]
 F02K 9/80
·  characterised by thrust or thrust vector control (F02K 9/26, F02K 9/56, F02K 9/94 take precedence)  [3]
 F02K 9/82
·  ·  by injection of a secondary fluid into the rocket exhaust gases  [3]
 F02K 9/84
·  ·  using movable nozzles  [3]
 F02K 9/86
·  ·  using nozzle throats of adjustable cross-section  [3]
 F02K 9/88
·  ·  using auxiliary rocket nozzles  [3]
 F02K 9/90
·  ·  using deflectors (F02K 9/82 takes precedence)  [3]
 F02K 9/92
·  ·  incorporating means for reversing or terminating thrust  [3]
 F02K 9/94
·  Re-ignitable or restartable rocket-engine plants; Intermittently operated rocket-engine plants  [3]
 F02K 9/95
·  characterised by starting or ignition means or arrangements (safety devices F02K 9/38)  [3]
 F02K 9/96
·  characterised by specially adapted arrangements for testing or measuring  [3]
 F02K 9/97
·  Rocket nozzles (thrust or thrust vector control F02K 9/80)  [3]
 F02K 11/00
Plants not provided for in the preceding groups  [3]