F02K   1/00		åȥѥפޤϥΥηޤ֤ħΤͭʥåȥѥפޤϥΥʥåȥΥƣˣ	Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto(rocket nozzles <b>F02K9/97</b>)	1838
F02K   1/04		åȥѥ˥åȥ֤	Mounting of an exhaust cone in the jet pipe	339
F02K   1/06		åȥѥפޤϥΥͭѤѤΡʥåή˱ƶͿήΤʮͤˤΣƣˣˡΣ	Varying effective area of jet pipe or nozzle (by using fluid jets to influence the jet flow <b>F02K1/30</b>)	596
F02K   1/08		ࡤ㡥ӵ󡤤μؤΰưޤȾؤѷˤ	by axially moving or transversely deforming an internal member, e.g. the exhaust cone	431
F02K   1/09		ࡤ㡥饦ɡμؤΰưˤΡʣƣˣͥ	by axially moving an external member, e.g. a shroud(<b>F02K1/12</b> takes precedence)	292
F02K   1/10		åȥѥפޤϥΥѷ뤳Ȥˤ	by distorting the jet pipe or nozzle	130
F02K   1/11		ǲžޤ֤ˤΡΣ	by means of pivoted eyelids	263
F02K   1/12		ž˻ٻ줿եåפˤ	by means of pivoted flaps	1181
F02K   1/15		ޤĴΣ	Control or regulation	619
F02K   1/16		¾ȤηΣ	conjointly with another control	263
F02K   1/17		ǳȤηΣ	with control of fuel supply	195
F02K   1/18		ưŪʤΡΣ	automatic	82
F02K   1/28		åή˱ƶͿ뤿ήΤʮͤΡΣ	using fluid jets to influence the jet flow	314
F02K   1/30		åȥѥפޤϥΥͭѤѤ뤿ΤΡΣ	for varying effective area of jet pipe or nozzle	163
F02K   1/32		Ϥž뤿ΤΡΣ	for reversing thrust	115
F02K   1/34		򸺾뤿ΤΡΣ	for attenuating noise	382
F02K   1/36		ĤΡΣ	having an ejector	343
F02K   1/38		åȤ˶ƳΡʣƣˣͥˡΣ	Introducing air inside the jet(<b>F02K1/28</b> takes precedence)	752
F02K   1/40		åȤʣʬŪʥåȤʬʤޤϺĹи̤ͭΥΣ	Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet	281
F02K   1/42		ư֤زưʤΡΣ	the means being movable into an inoperative position	106
F02K   1/44		ؤβͤ򸺾ʡ㡥ġĤΡʣƣˣͥˡΣ	Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction(<b>F02K1/40</b> takes precedence)	248
F02K   1/46		åȤ˶ä뤿ΤޤϥåȤȼϤζȤκμʤͭΥ롤㡥òΤΤΡʣƣˣƣˣƣˣͥˡΣ	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(<b>F02K1/28</b>, <b>F02K1/36</b>, <b>F02K1/38</b> take precedence)	457
F02K   1/48		ȷΥΥΣ	Corrugated nozzles	337
F02K   1/50		åȤΰǼǽʥ׾ΥХåեˤ곰¦иΡΣ	Deflecting outwardly a portion of the jet by retractable scoop-like baffles	33
F02K   1/52		¾ΥΥޤϸࡤ㡥ե󥰡ܤư֤뤿ä˹줿Υ	Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member, e.g. fairing	195
F02K   1/54		Ϥž뤿μʤͭΡήʮήѤƿϤžΣƣˣˡΣ	Nozzles having means for reversing jet thrust (reversing jet thrust using fluid jets <b>F02K1/32</b>)	326
F02K   1/56		åȼήžΡΣ	Reversing jet main flow	347
F02K   1/58		ž֤ޤϥΥϥ󥰤줿ΡΣ	Reversers mounted on the inner cone or the nozzle housing	73
F02K   1/60		ǲžޤ֤ޤȺˤؤФ˸Ρ㡥åȷεž֡Σ	by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers	432
F02K   1/62		եåפˤؤФ˸ΡΣ	by blocking the rearward discharge by means of flaps	323
F02K   1/64		եήžΡΣ	Reversing fan flow	213
F02K   1/66		žѥե󱩺ѤΡΣ	using reversing fan blades	114
F02K   1/68		ž֤եӵήΥ󥸥ϥ󥰤줿ΡΣ	Reversers mounted on the engine housing downstream of the fan exhaust section	114
F02K   1/70		եϥ󥰤줿ϵžѥեåפޤϥɥѤΡΣ	using thrust reverser flaps or doors mounted on the fan housing	529
F02K   1/72		եϥ󥰤θüưƵž줿ή줬̤ϩեϥ󥰤˳ΡΣ	the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow	896
F02K   1/74		ʣή󥸥ˤƾʤȤ¾ΤҤȤĤή˴ؤƾʤȤҤȤĤήžΡΣ	Reversing at least one flow in relation to at least one other flow in a plural-flow engine	89
F02K   1/76		ϵž֤ޤĴΣ	Control or regulation of thrust reversers	943
F02K   1/78		åȥѥפΤ¾ι¤Σ	Other construction of jet pipes	991
F02K   1/80		Ϣޤ³Σ	Couplings or connections	707
F02K   1/82		åȥѥɡ㡥饤ʡΣ	Jet pipe walls, e.g. liners	1829
F02K   3/00		̵ޤϥƥåɥեư륬ӥΤ	Plants including a gas turbine driving a compressor or a ducted fan	1601
F02K   3/02		ưήΤΰӥǳƼХѥ	in which part of the working fluid by-passes the turbine and combustion chamber	1327
F02K   3/04		äΤ˥ƥåɥե󡤤ʤή㰵Υե󡤤ͭΡ㡥ήΤ	the plant including ducted fans, i.e. fans with high volume, low-pressure outputs, for augmenting jet thrust, e.g. of double-flow type	1216
F02K   3/06		եȥեͭ	with front fan	3964
F02K   3/062		եȥեͭΡΣ	with aft fan	213
F02K   3/065		եȥեȥեȥեͭΡΣ	with front and aft fans	117
F02K   3/068		ľ¤ФûĹˤäħŤ줿ΡΣ	being characterised by a short axial length relative to diameter	146
F02K   3/072		ղžͭΡΣ	with counter-rotating rotors	482
F02K   3/075		ʣήή椹ΡΣ	controlling flow ratio between flows	844
F02K   3/077		¿ήǤΡʤʾήͭ	the plant being of the multiple flow type, i.e. having three or more flows	342
F02K   3/08		ưήΤŪ˲ǮΡʤΤǳƣãˡΣ	with supplementary heating of the working fluid; Control thereof(control of fuel supply therefor <b>F02C9/26</b>)	176
F02K   3/10		եСʤˤΡʣƣˣͥˡΣ	by after-burners(<b>F02K3/105</b> takes precedence)	781
F02K   3/105		ХѥήǮΡΣ	Heating the by-pass flow	73
F02K   3/11		СʤޤǳƼˤΡΣ	by means of burners or combustion chambers	179
F02K   3/115		ŪǮ򴹤ˤΡΣ	by means of indirect heat exchange	275
F02K   3/12		ʣΥӥΤ뤳ȤħȤ	characterised by having more than one gas turbine	229
F02K   5/00		̵ޤϥƥåɥեư륬ӥʳεؤΤ	Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan	607
F02K   5/02		εؤԥȥǤ	the engine being of the reciprocating-piston type	247
F02K   7/00		ưήΤʮͤΤߤ˻Ѥʤ̵ޤϥƥåɥեư륿ӥޤϤ¾εؤΤʤʥåȥ󥸥ƣˣ	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 <b>F02K9/00</b>)	875
F02K   7/02		ʮַͤŪʤΡʤѥ륹å	the jet being intermittent, i.e. pulse jet	590
F02K   7/04		ǳƼΤ	with resonant combustion chambers	219
F02K   7/06		ǳƼۤĤ	with combustion chambers having valves	322
F02K   7/067		ϳŪۤĤΡΣ	having aerodynamic valves	79
F02K   7/075		¿Υѥ륹åȥ󥸥ͭΡΣ	with multiple pulse-jet engines	94
F02K   7/08		ʮͤϢ³Ūʤ	the jet being continuous	307
F02K   7/10		వˤ밵̤ˤäħŤ줿ΡʤϳǮϳŪƳɤޤϥॸåȥ󥸥	characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines	1290
F02K   7/12		󥸥󥤥󥸥åȥ󥸥Σ	Injection-induction jet engines	207
F02K   7/14		ǳƤΡ㡥ॸåȥ󥸥Σ	with external combustion, e.g. scram-jet engines	353
F02K   7/16		ॸåȡܥåȤʣ票󥸥Σ	Composite ram-jet/turbo-jet engines	545
F02K   7/18		ॸåȡåȤʣ票󥸥Σ	Composite ram-jet/rocket engines	671
F02K   7/20		ॸåȡѥ륹åȤʣ票󥸥Σ	Composite ram-jet/pulse-jet engines	93
F02K   9/00		åȥ󥸥󡤤ʤǳȤλޤξܤΣ	Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof	958
F02K   9/08		ΤοʺޤѤΡʣƣˣͥ表ȾΤޤʴοʺޤѤΣƣˣˡΣ	using solid propellants(<b>F02K9/72</b> takes precedence; using semi-solid or pulverulent propellants <b>F02K9/70</b>)	741
F02K   9/10		οηޤϹ¤Σ	Shape or structure of solid propellant charges	573
F02K   9/12		ǳ®٤ΰۤʤ룲ʾʬΡΣ	made of two or more portions burning at different rates	234
F02K   9/14		ȾκΡ㡥ڥåȥ뷿ع¤	made from sheet-like materials, e.g. of carpet-roll type, of layered structure	134
F02K   9/16		ϥ˥๽¤ΤΡΣ	of honeycomb structure	23
F02K   9/18		ޤ⹦ͭǳƷΤΡΣ	of the internal-burning type having a star or like shaped internal cavity	235
F02K   9/20		ǳƷΤΡΣ	of the external-burning type	33
F02K   9/22		üǳƷΤΡΣ	of the front-burning type	65
F02K   9/24		οʺޤΥåȥ󥸥ؤŶοʺޤŶäŬ礷ˡޤ֡Σ	Charging rocket engines with solid propellants; Methods or apparatus specially adapted for working solid propellant charges	593
F02K   9/26		ǳƤΣ	Burning control	367
F02K   9/28		ʾοͭҤȤĤζ̤ΥΥʥӽФΡΣ	having two or more propellant charges with the propulsion gases exhausting through a common nozzle	259
F02K   9/30		ʣΥΥʥӽФΡΣ	with the propulsion gases exhausting through a plurality of nozzles	149
F02K   9/32		¤Ūʬ¾ʬवʤΣ	Constructional parts; Details not otherwise provided for	712
F02K   9/34		󥰡ǳƼΥ饤ʡΣ	Casings; Combustion chambers; Liners thereof	1453
F02K   9/36		λٻΣ	Propellant charge supports	364
F02K   9/38		֡㡥ȯŪФɻߡΣ	Safety devices, e.g. to prevent accidental ignition	313
F02K   9/40		֡Σ	Cooling arrangements	110
F02K   9/42		ΤޤϵΤοѤΡʣƣˣͥˡΣ	using liquid or gaseous propellants(<b>F02K9/72</b> takes precedence)	983
F02K   9/44		ʺޤζΣ	Feeding propellants	894
F02K   9/46		ݥפѤΡΣ	using pumps	565
F02K   9/48		ʺޤǳƥ뤵륬ӥˤưΡΣ	driven by a gas turbine fed by propellant combustion gases	528
F02K   9/50		ʺޤð뤿˹ⰵήΤѤΡΣ	using pressurised fluid to pressurize the propellants	593
F02K   9/52		ʮʹΣ	Injectors	1377
F02K   9/54		ϳ̸дƥࡨ᥷ƥΣ	Leakage detectors; Purging systems; Filtration systems	99
F02K   9/56		Σ	Control	784
F02K   9/58		ʺ޶ۡΣ	Propellant feed valves	738
F02K   9/60		¤Ūʬ¾ʬवʤΣ	Constructional parts; Details not otherwise provided for	1570
F02K   9/62		ǳƼޤϿϼΣ	Combustion or thrust chambers	1024
F02K   9/64		֤ĤΡΣ	having cooling arrangements	1121
F02K   9/66		󷿤ΤΡΣ	of the rotary type	106
F02K   9/68		ʬ򼼡Σ	Decomposition chambers	365
F02K   9/70		ȾΤޤʴοʺޤѤΡΣ	using semi-solid or pulverulent propellants	198
F02K   9/72		ΤȸΤοʺޤѤΡʤϥ֥åɥåȥ󥸥	using liquid and solid propellants, i.e. hybrid rocket-engine plants	590
F02K   9/74		¾ΥåȿȤȤ߹碌Σ	combined with another jet-propulsion plant	57
F02K   9/76		¾Υåȥ󥸥ȤȤ߹碌¿ʥåȥ󥸥Σ	with another rocket-engine plant; Multistage rocket-engine plants	229
F02K   9/78		۹åȿȤȤ߹碌ʥॸåȥ󥸥ȤȤ߹碌ƣˣˡΣ	with an air-breathing jet-propulsion plant(with a ram-jet engine <b>F02K7/18</b>)	224
F02K   9/80		ϤޤϿϥ٥ȥħȤΡʸΤοʺޤǳƣˣΤޤϵΤοζƣˣСƻưǽʤޤϴַŪ˺ưåȥ󥸥ƣˣˡΣ	characterised by thrust or thrust vector control (burning control of solid propellants <b>F02K9/26</b>; feeding control of liquid or gaseous propellants <b>F02K9/56</b>; re-ignitable, restartable or intermittently operated rocket-engine plants <b>F02K9/94</b>)	705
F02K   9/82		åӵήΤʮͤΡΣ	by injection of a secondary fluid into the rocket exhaust gases	238
F02K   9/84		ưΥѤΡΣ	using movable nozzles	461
F02K   9/86		Υ륹ѤĴǽʤΡΣ	using nozzle throats of adjustable cross-section	327
F02K   9/88		åȥΥѤΡΣ	using auxiliary rocket nozzles	168
F02K   9/90		и֤ѤΡʣƣˣͥˡΣ	using deflectors(<b>F02K9/82</b> takes precedence)	200
F02K   9/92		ϤžޤϽ뤵뤿μʤȷ礷ΡΣ	incorporating means for reversing or terminating thrust	132
F02K   9/94		ФޤϺƻưǽʥåȥ󥸥ַŪ˺ưåȥ󥸥Σ	Re-ignitable or restartable rocket-engine plants; Intermittently operated rocket-engine plants	263
F02K   9/95		ưޤмʤޤ֤ˤäħŤ줿Ρʰ֣ƣˣˡΣ	characterised by starting or ignition means or arrangements(safety devices <b>F02K9/38</b>)	1723
F02K   9/96		ޤϷ¬ΤäŬ礷֤ˤäħŤ줿ΡΣ	characterised by specially adapted arrangements for testing or measuring	1685
F02K   9/97		åȥΥʿϤޤϿϥ٥ȥƣˣˡΣ	Rocket nozzles(thrust or thrust vector control <b>F02K9/80</b>)	2376
F02K  99/00		Υ֥饹¾Υ롼פʬवʤࡡΣ	Subject matter not provided for in other groups of this subclass	691
