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  • F02B75/00
    		•  Other engines, e.g. single-cylinder engines HB CC 3G011
  • F02B75/00@A
    		•  characterized by the measures against exhaust gas HB CC 3G011
  • F02B75/00@B
    		•  .Multi-cylinder engines HB CC 3G011
  • F02B75/00@Z
    		•  Others HB CC 3G011
  • F02B75/02
    		•  .Engines characterised by their cycles, e.g. six-stroke HB CC 3G011
  • F02B75/02@A
    		•  6-cycle engines HB CC 3G011
  • F02B75/02@B
    		•  Regeneration cycle engines HB CC 3G011
  • F02B75/02@Z
    		•  Others HB CC 3G011
  • F02B75/04
    		•  .Engines with variable distances between pistons at top dead-centre positions and cylinder heads HB CC 3G011
  • F02B75/06
    		•  .Engines with means for equalisingtorque [1, 2006.01] HB CC 3G011
  • F02B75/08
    		•  .Engines with means for preventing corrosion in gas-swept spaces HB CC 3G011
  • F02B75/10
    		•  .Engines with means for rendering exhaust gases innocuous (apparatus per se F01N 3/00) [1, 2006.01] HB CC 3G011
  • F02B75/10@A
    		•  Multi-cylinder engines HB CC 3G011
  • F02B75/10@B
    		•  .Lean-rich combustion engines HB CC 3G011
  • F02B75/10@C
    		•  having an EGR means HB CC 3G011
  • F02B75/10@D
    		•  having a secondary air supply means HB CC 3G011
  • F02B75/10@E
    		•  Co-use of the EGR means and secondary air supply means HB CC 3G011
  • F02B75/10@Z
    		•  Others (catalyst R F 01 N 3/28) HB CC 3G011
  • F02B75/12
    		•  .Other methods of operation HB CC 3G011
  • F02B75/16
    		•  .Engines characterised by number of cylinders, e.g. single-cylinder engines (F02B 75/26 takes precedence) HB CC 3G011
  • F02B75/18
    		•  ..Multi-cylinder engines (scavenging aspects F02B 25/00) HB CC 3G011
  • F02B75/18@C
    		•  Different configurations or operations among cylinders HB CC 3G011
  • F02B75/18@D
    		•  .Different ignition types or cycles HB CC 3G011
  • F02B75/18@E
    		•  .Different cylinder shapes HB CC 3G011
  • F02B75/18@F
    		•  .Different compression ratios HB CC 3G011
  • F02B75/18@G
    		•  .Different air-fuel ratios HB CC 3G011
  • F02B75/18@H
    		•  Cylinder shape or layout HB CC 3G011
  • F02B75/18@J
    		•  having multiple crank shafts HB CC 3G011
  • F02B75/18@K
    		•  Air inlet/exhaust system HB CC 3G011
  • F02B75/18@L
    		•  .Drive or layout of the air inlet/exhaust valve HB CC 3G011
  • F02B75/18@M
    		•  Vibration prevention HB CC 3G011
  • F02B75/18@N
    		•  Pressure reduction operation allowed (control R F 02 D 17/02) HB CC 3G011
  • F02B75/18@P
    		•  having a communication channel between cylinders HB CC 3G011
  • F02B75/18@Z
    		•  Others HB CC 3G011
  • F02B75/20
    		•  ...with cylinders all in one line HB CC 3G011
  • F02B75/22
    		•  ...with cylinders in V-, fan-, or star-arrangement HB CC 3G011
  • F02B75/22@A
    		•  V type engines HB CC 3G011
  • F02B75/22@B
    		•  .Cylinder or crank case (including layout) HB CC 3G011
  • F02B75/22@C
    		•  .Air inlet/exhaust system HB CC 3G011
  • F02B75/22@D
    		•  .Valve motion mechanism HB CC 3G011
  • F02B75/22@E
    		•  .Cooling HB CC 3G011
  • F02B75/22@F
    		•  .Layout or drive of an auxiliary machine (general R F 02 B 67/00) HB CC 3G011
  • F02B75/22@G
    		•  .Vibration prevention (components R F 02 B 77/00 B) HB CC 3G011
  • F02B75/22@H
    		•  .Installation to a vehicle HB CC 3G011
  • F02B75/22@J
    		•  Star type engines HB CC 3G011
  • F02B75/22@Z
    		•  Others HB CC 3G011
  • F02B75/24
    		•  ...with cylinders arranged oppositely relative to main shaft and of "flat" type HB CC 3G011
  • F02B75/26
    		•  .Engines with cylinder axes coaxial with, or parallel or inclined to, main-shaft axis; Engines with cylinder axes arranged substantially tangentially to a circle centred on main-shaft axis HB CC 3G011
  • F02B75/28
    		•  .Engines with two or more pistons reciprocating within same cylinder or within essentially coaxial cylinders (arranged oppositely relative to main shaft F02B 75/24) HB CC 3G011
  • F02B75/28@A
    		•  Individual pistons that perform different motions HB CC 3G011
  • F02B75/28@B
    		•  characterized by the linkage between pistons HB CC 3G011
  • F02B75/28@C
    		•  .Link mechanism HB CC 3G011
  • F02B75/28@D
    		•  .directly connected HB CC 3G011
  • F02B75/28@E
    		•  2-cycle engines HB CC 3G011
  • F02B75/28@F
    		•  having at least three pistons for a combustion chamber HB CC 3G011
  • F02B75/28@Z
    		•  Others HB CC 3G011
  • F02B75/30
    		•  ..with one working piston sliding inside another HB CC 3G011
  • F02B75/32
    		•  .Engines characterised by connections between pistons and main shafts and not specific to preceding main groups HB CC 3G011
  • F02B75/32@A
    		•  Crank shaft provided (general R F 01 B 9/02) HB CC 3G011
  • F02B75/32@B
    		•  .Connection via a single connection rod HB CC 3G011
  • F02B75/32@C
    		•  .Multiple connection rods provided in parallel HB CC 3G011
  • F02B75/32@D
    		•  .having no connection rod HB CC 3G011
  • F02B75/32@E
    		•  using a diagonal plate or curved surface (general R F 01 B 9/04) HB CC 3G011
  • F02B75/32@Z
    		•  Others HB CC 3G011
  • F02B75/34
    		•  .Ultra-small engines, e.g. for driving models HB CC 3G011
  • F02B75/34@A
    		•  Multi-cylinder engines HB CC 3G011
  • F02B75/34@B
    		•  Starting device HB CC 3G011
  • F02B75/34@C
    		•  Exhaust device HB CC 3G011
  • F02B75/34@Z
    		•  Others HB CC 3G011
  • F02B75/36
    		•  .Engines with parts of combustion- or working-chamber walls resiliently yielding under pressure HB CC 3G011
  • F02B75/38
    		•  ..Reciprocating-piston engines (F02B 75/04 takes precedence; with resiliently-urged auxiliary piston in pre-combustion chamber F02B 19/06) HB CC 3G011
  • F02B75/40
    		•  .Other reciprocating-piston engines HB CC 3G011
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