F02K   1/00  \	0	0	3G106	F02K   1/00	54	åȥѥפޤϥΥηޤ֤ħΤͭʥåȥѥפޤϥΥʥåȥΥƣˣ	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  \	1	1	3G106	F02K   1/04	33	åȥѥ˥åȥ֤	Mounting of an exhaust cone in the jet pipe
F02K   1/06  \	1	1	3G106	F02K   1/06	48	åȥѥפޤϥΥͭѤѤΡʥåή˱ƶͿήΤʮͤˤΣƣˣˡΣ	Varying effective area of jet pipe or nozzle (by using fluid jets to influence the jet flow F02K 1/30) [1, 3, 2006.01]
F02K   1/08  \	2	2	3G106	F02K   1/08	37	ࡤ㡥ӵ󡤤μؤΰưޤȾؤѷˤ	by axially moving or transversely deforming an internal member, e.g. the exhaust cone
F02K   1/09  \	2	2	3G106	F02K   1/09	20	ࡤ㡥饦ɡμؤΰưˤΡʣƣˣͥ	by axially moving an external member, e.g. a shroud (F02K 1/12 takes precedence) [3]
F02K   1/10  \	2	2	3G106	F02K   1/10	30	åȥѥפޤϥΥѷ뤳Ȥˤ	by distorting the jet pipe or nozzle
F02K   1/11  \	2	2	3G106	F02K   1/11	4	ǲžޤ֤ˤΡΣ	by means of pivoted eyelids [3]
F02K   1/12  \	2	2	3G106	F02K   1/12	186	ž˻ٻ줿եåפˤ	by means of pivoted flaps
F02K   1/15  \	2	2	3G106	F02K   1/15	36	ޤĴΣ	Control or regulation [3]
F02K   1/16  \	3	3	3G106	F02K   1/16	18	¾ȤηΣ	conjointly with another control [3]
F02K   1/17  \	4	4	3G106	F02K   1/17	13	ǳȤηΣ	with control of fuel supply [3]
F02K   1/18  \	3	3	3G106	F02K   1/18	10	ưŪʤΡΣ	automatic [3]
F02K   1/28  \	1	1	3G106	F02K   1/28	30	åή˱ƶͿ뤿ήΤʮͤΡΣ	using fluid jets to influence the jet flow [3]
F02K   1/30  \	2	2	3G106	F02K   1/30	14	åȥѥפޤϥΥͭѤѤ뤿ΤΡΣ	for varying effective area of jet pipe or nozzle [3]
F02K   1/32  \	2	2	3G106	F02K   1/32	9	Ϥž뤿ΤΡΣ	for reversing thrust [3]
F02K   1/34  \	2	2	3G106	F02K   1/34	50	򸺾뤿ΤΡΣ	for attenuating noise [3]
F02K   1/36  \	1	1	3G106	F02K   1/36	25	ĤΡΣ	having an ejector [3]
F02K   1/38  \	1	1	3G106	F02K   1/38	43	åȤ˶ƳΡʣƣˣͥˡΣ	Introducing air inside the jet (F02K 1/28 takes precedence) [3]
F02K   1/40  \	1	1	3G106	F02K   1/40	23	åȤʣʬŪʥåȤʬʤޤϺĹи̤ͭΥΣ	Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet [3]
F02K   1/42  \	2	2	3G106	F02K   1/42	2	ư֤زưʤΡΣ	the means being movable into an inoperative position [3]
F02K   1/44  \	1	1	3G106	F02K   1/44	54	ؤβͤ򸺾ʡ㡥ġĤΡʣƣˣͥˡΣ	Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction (F02K 1/40 takes precedence) [3]
F02K   1/46  \	1	1	3G106	F02K   1/46	65	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 (F02K 1/28, F02K 1/36, F02K 1/38 take precedence) [3]
F02K   1/48  \	2	2	3G106	F02K   1/48	59	ȷΥΥΣ	Corrugated nozzles [3]
F02K   1/50  \	2	2	3G106	F02K   1/50	1	åȤΰǼǽʥ׾ΥХåեˤ곰¦иΡΣ	Deflecting outwardly a portion of the jet by retractable scoop-like baffles [3]
F02K   1/52  \	1	1	3G106	F02K   1/52	12	¾ΥΥޤϸࡤ㡥ե󥰡ܤư֤뤿ä˹줿Υ	Nozzles specially constructed for positioning adjacent to another nozzle or to a fixed member, e.g. fairing [3, 2006.01]
F02K   1/54  \	1	1	3G106	F02K   1/54	25	Ϥž뤿μʤͭΡήʮήѤƿϤžΣƣˣˡΣ	Nozzles having means for reversing jet thrust (reversing jet thrust using fluid jets F02K 1/32) [3, 2006.01]
F02K   1/56  \	2	2	3G106	F02K   1/56	13	åȼήžΡΣ	Reversing jet main flow [3]
F02K   1/58  \	3	3	3G106	F02K   1/58	9	ž֤ޤϥΥϥ󥰤줿ΡΣ	Reversers mounted on the inner cone or the nozzle housing [3]
F02K   1/60  \	3	3	3G106	F02K   1/60	35	ǲžޤ֤ޤȺˤؤФ˸Ρ㡥åȷεž֡Σ	by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers [3]
F02K   1/62  \	3	3	3G106	F02K   1/62	28	եåפˤؤФ˸ΡΣ	by blocking the rearward discharge by means of flaps [3]
F02K   1/64  \	2	2	3G106	F02K   1/64	19	եήžΡΣ	Reversing fan flow [3]
F02K   1/66  \	3	3	3G106	F02K   1/66	8	žѥե󱩺ѤΡΣ	using reversing fan blades [3]
F02K   1/68  \	3	3	3G106	F02K   1/68	13	ž֤եӵήΥ󥸥ϥ󥰤줿ΡΣ	Reversers mounted on the engine housing downstream of the fan exhaust section [3]
F02K   1/70  \	3	3	3G106	F02K   1/70	77	եϥ󥰤줿ϵžѥեåפޤϥɥѤΡΣ	using thrust reverser flaps or doors mounted on the fan housing [3]
F02K   1/72  \	4	4	3G106	F02K   1/72	38	եϥ󥰤θüưƵž줿ή줬̤ϩեϥ󥰤˳ΡΣ	the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow [3]
F02K   1/74  \	2	2	3G106	F02K   1/74	5	ʣή󥸥ˤƾʤȤ¾ΤҤȤĤή˴ؤƾʤȤҤȤĤήžΡΣ	Reversing at least one flow in relation to at least one other flow in a plural-flow engine [3]
F02K   1/76  \	2	2	3G106	F02K   1/76	28	ϵž֤ޤĴΣ	Control or regulation of thrust reversers [3]
F02K   1/78  \	1	1	3G106	F02K   1/78	93	åȥѥפΤ¾ι¤Σ	Other construction of jet pipes [3]
F02K   1/78  A	1	0	3G106	F02K   1/78	71	ϤѹǤ	Thrust force direction changeable
F02K   1/78  B	1	1	3G106	F02K   1/78	38	ľΥΦԤΤ	for vertical take-off/landing
F02K   1/78  C	1	2	3G106	F02K   1/78	0	åȥѥפž	Entire jet pipe that rotates
F02K   1/78  D	1	2	3G106	F02K   1/78	26	åȥѥפΰž	Part of the jet pipe that rotates
F02K   1/78  Z	1	0	3G106	F02K   1/78	66	¾Τ	Others
F02K   1/80  \	2	2	3G106	F02K   1/80	36	Ϣޤ³Σ	Couplings or connections [3]
F02K   1/82  \	2	2	3G106	F02K   1/82	62	åȥѥɡ㡥饤ʡΣ	Jet pipe walls, e.g. liners [3]
F02K   3/00  \	0	0	3G106	F02K   3/00	153	̵ޤϥƥåɥեư륬ӥΤ	Plants including a gas turbine driving a compressor or a ducted fan [1, 2006.01]
F02K   3/02  \	1	1	3G106	F02K   3/02	84	ưήΤΰӥǳƼХѥ	in which part of the working fluid by-passes the turbine and combustion chamber
F02K   3/04  \	2	2	3G106	F02K   3/04	213	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 [1, 2006.01]
F02K   3/06  \	3	3	3G106	F02K   3/06	735	եȥեͭ	with front fan
F02K   3/062  \	3	3	3G106	F02K   3/062	37	եȥեͭΡΣ	with aft fan [3]
F02K   3/065  \	3	3	3G106	F02K   3/065	12	եȥեȥեȥեͭΡΣ	with front and aft fans [3]
F02K   3/068  \	3	3	3G106	F02K   3/068	4	ľ¤ФûĹˤäħŤ줿ΡΣ	being characterised by a short axial length relative to diameter [3]
F02K   3/072  \	3	3	3G106	F02K   3/072	79	ղžͭΡΣ	with counter-rotating rotors [3]
F02K   3/075  \	3	3	3G106	F02K   3/075	110	ʣήή椹ΡΣ	controlling flow ratio between flows [3]
F02K   3/077  \	3	3	3G106	F02K   3/077	9	¿ήǤΡʤʾήͭ	the plant being of the multiple flow type, i.e. having three or more flows [3, 2006.01]
F02K   3/08  \	1	1	3G106	F02K   3/08	19	ưήΤŪ˲ǮΡʤΤǳƣãˡΣ	with supplementary heating of the working fluid; Control thereof (control of fuel supply therefor F02C 9/26) [1, 3, 2006.01]
F02K   3/10  \	2	2	3G106	F02K   3/10	135	եСʤˤΡʣƣˣͥˡΣ	by after-burners (F02K 3/105 takes precedence) [3]
F02K   3/105  \	2	2	3G106	F02K   3/105	13	ХѥήǮΡΣ	Heating the by-pass flow [3]
F02K   3/11  \	3	3	3G106	F02K   3/11	29	СʤޤǳƼˤΡΣ	by means of burners or combustion chambers [3]
F02K   3/115  \	3	3	3G106	F02K   3/115	7	ŪǮ򴹤ˤΡΣ	by means of indirect heat exchange [3]
F02K   3/12  \	1	1	3G106	F02K   3/12	146	ʣΥӥΤ뤳ȤħȤ	characterised by having more than one gas turbine
F02K   5/00  \	0	0	3G106	F02K   5/00	86	̵ޤϥƥåɥեư륬ӥʳεؤΤ	Plants including an engine, other than a gas turbine, driving a compressor or a ducted fan [1, 2006.01]
F02K   5/02  \	1	1	3G106	F02K   5/02	11	εؤԥȥǤ	the engine being of the reciprocating-piston type
F02K   7/00  \	0	0	3G106	F02K   7/00	45	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 F02K 9/00)
F02K   7/02  \	1	1	3G106	F02K   7/02	62	ʮַͤŪʤΡʤѥ륹å	the jet being intermittent, i.e. pulse jet
F02K   7/04  \	2	2	3G106	F02K   7/04	16	ǳƼΤ	with resonant combustion chambers
F02K   7/06  \	2	2	3G106	F02K   7/06	44	ǳƼۤĤ	with combustion chambers having valves
F02K   7/067  \	3	3	3G106	F02K   7/067	4	ϳŪۤĤΡΣ	having aerodynamic valves [3]
F02K   7/075  \	2	2	3G106	F02K   7/075	5	¿Υѥ륹åȥ󥸥ͭΡΣ	with multiple pulse-jet engines [3]
F02K   7/08  \	1	1	3G106	F02K   7/08	32	ʮͤϢ³Ūʤ	the jet being continuous
F02K   7/10  \	1	1	3G106	F02K   7/10	225	వˤ밵̤ˤäħŤ줿ΡʤϳǮϳŪƳɤޤϥॸåȥ󥸥	characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
F02K   7/12  \	2	2	3G106	F02K   7/12	13	󥸥󥤥󥸥åȥ󥸥Σ	Injection-induction jet engines [3]
F02K   7/14  \	2	2	3G106	F02K   7/14	102	ǳƤΡ㡥ॸåȥ󥸥Σ	with external combustion, e.g. scram-jet engines [3]
F02K   7/16  \	2	2	3G106	F02K   7/16	86	ॸåȡܥåȤʣ票󥸥Σ	Composite ram-jet/turbo-jet engines [3]
F02K   7/18  \	2	2	3G106	F02K   7/18	143	ॸåȡåȤʣ票󥸥Σ	Composite ram-jet/rocket engines [3]
F02K   7/20  \	2	2	3G106	F02K   7/20	5	ॸåȡѥ륹åȤʣ票󥸥Σ	Composite ram-jet/pulse-jet engines [3]
F02K   9/00  \	0	0	3G106	F02K   9/00	57	åȥ󥸥󡤤ʤǳȤλޤξܤΣ	Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof [1, 3, 2006.01]
F02K   9/08  \	1	1	3G106	F02K   9/08	117	ΤοʺޤѤΡʣƣˣͥ表ȾΤޤʴοʺޤѤΣƣˣˡΣ	using solid propellants (F02K 9/72 takes precedence; using semi-solid or pulverulent propellants F02K 9/70) [3]
F02K   9/10  \	2	2	3G106	F02K   9/10	70	οηޤϹ¤Σ	Shape or structure of solid propellant charges [3]
F02K   9/12  \	3	3	3G106	F02K   9/12	31	ǳ®٤ΰۤʤ룲ʾʬΡΣ	made of two or more portions burning at different rates [3]
F02K   9/14  \	3	3	3G106	F02K   9/14	11	ȾκΡ㡥ڥåȥ뷿ع¤	made from sheet-like materials, e.g. of carpet-roll type, of layered structure [3]
F02K   9/16  \	3	3	3G106	F02K   9/16	2	ϥ˥๽¤ΤΡΣ	of honeycomb structure [3]
F02K   9/18  \	3	3	3G106	F02K   9/18	33	ޤ⹦ͭǳƷΤΡΣ	of the internal-burning type having a star or like shaped internal cavity [3]
F02K   9/20  \	3	3	3G106	F02K   9/20	6	ǳƷΤΡΣ	of the external-burning type [3]
F02K   9/22  \	3	3	3G106	F02K   9/22	21	üǳƷΤΡΣ	of the front-burning type [3]
F02K   9/24  \	2	2	3G106	F02K   9/24	62	οʺޤΥåȥ󥸥ؤŶοʺޤŶäŬ礷ˡޤ֡Σ	Charging rocket engines with solid propellants; Methods or apparatus specially adapted for working solid propellant charges [3]
F02K   9/26  \	2	2	3G106	F02K   9/26	43	ǳƤΣ	Burning control [3]
F02K   9/28  \	2	2	3G106	F02K   9/28	52	ʾοͭҤȤĤζ̤ΥΥʥӽФΡΣ	having two or more propellant charges with the propulsion gases exhausting through a common nozzle [3]
F02K   9/30  \	2	2	3G106	F02K   9/30	26	ʣΥΥʥӽФΡΣ	with the propulsion gases exhausting through a plurality of nozzles [3]
F02K   9/32  \	2	2	3G106	F02K   9/32	64	¤Ūʬ¾ʬवʤΣ	Constructional parts; Details not otherwise provided for [3, 2006.01]
F02K   9/34  \	3	3	3G106	F02K   9/34	160	󥰡ǳƼΥ饤ʡΣ	Casings; Combustion chambers; Liners thereof [3]
F02K   9/36  \	3	3	3G106	F02K   9/36	57	λٻΣ	Propellant charge supports [3]
F02K   9/38  \	3	3	3G106	F02K   9/38	48	֡㡥ȯŪФɻߡΣ	Safety devices, e.g. to prevent accidental ignition [3]
F02K   9/40  \	3	3	3G106	F02K   9/40	19	֡Σ	Cooling arrangements [3]
F02K   9/42  \	1	1	3G106	F02K   9/42	93	ΤޤϵΤοѤΡʣƣˣͥˡΣ	using liquid or gaseous propellants (F02K 9/72 takes precedence) [3]
F02K   9/44  \	2	2	3G106	F02K   9/44	114	ʺޤζΣ	Feeding propellants [3]
F02K   9/46  \	3	3	3G106	F02K   9/46	97	ݥפѤΡΣ	using pumps [3, 2006.01]
F02K   9/48  \	4	4	3G106	F02K   9/48	55	ʺޤǳƥ뤵륬ӥˤưΡΣ	driven by a gas turbine fed by propellant combustion gases [3]
F02K   9/50  \	3	3	3G106	F02K   9/50	77	ʺޤð뤿˹ⰵήΤѤΡΣ	using pressurised fluid to pressurize the propellants [3]
F02K   9/52  \	3	3	3G106	F02K   9/52	108	ʮʹΣ	Injectors [3, 2006.01]
F02K   9/54  \	3	3	3G106	F02K   9/54	5	ϳ̸дƥࡨ᥷ƥΣ	Leakage detectors; Purging systems; Filtration systems [3, 2006.01]
F02K   9/56  \	3	3	3G106	F02K   9/56	75	Σ	Control [3]
F02K   9/58  \	4	4	3G106	F02K   9/58	54	ʺ޶ۡΣ	Propellant feed valves [3, 2006.01]
F02K   9/60  \	2	2	3G106	F02K   9/60	83	¤Ūʬ¾ʬवʤΣ	Constructional parts; Details not otherwise provided for [3, 2006.01]
F02K   9/62  \	3	3	3G106	F02K   9/62	126	ǳƼޤϿϼΣ	Combustion or thrust chambers [3]
F02K   9/64  \	4	4	3G106	F02K   9/64	177	֤ĤΡΣ	having cooling arrangements [3]
F02K   9/66  \	4	4	3G106	F02K   9/66	5	󷿤ΤΡΣ	of the rotary type [3]
F02K   9/68  \	3	3	3G106	F02K   9/68	36	ʬ򼼡Σ	Decomposition chambers [3]
F02K   9/70  \	1	1	3G106	F02K   9/70	15	ȾΤޤʴοʺޤѤΡΣ	using semi-solid or pulverulent propellants [3]
F02K   9/72  \	1	1	3G106	F02K   9/72	85	ΤȸΤοʺޤѤΡʤϥ֥åɥåȥ󥸥	using liquid and solid propellants, i.e. hybrid rocketengine plants [3, 2006.01]
F02K   9/74  \	1	1	3G106	F02K   9/74	13	¾ΥåȿȤȤ߹碌Σ	combined with another jet-propulsion plant [3]
F02K   9/76  \	2	2	3G106	F02K   9/76	30	¾Υåȥ󥸥ȤȤ߹碌¿ʥåȥ󥸥Σ	combined with another jet-propulsion plant [3, 2006.01]
F02K   9/78  \	2	2	3G106	F02K   9/78	63	۹åȿȤȤ߹碌ʥॸåȥ󥸥ȤȤ߹碌ƣˣˡΣ	with an air-breathing jet-propulsion plant (with a ram-jet engine F02K 7/18) [3]
F02K   9/80  \	1	1	3G106	F02K   9/80	70	ϤޤϿϥ٥ȥħȤΡʸΤοʺޤǳƣˣΤޤϵΤοζƣˣСƻưǽʤޤϴַŪ˺ưåȥ󥸥ƣˣˡΣ	characterised by thrust or thrust vector control (burning control of solid propellants F02K 9/26; feeding control of liquid or gaseous propellants F02K 9/56; re-ignitable, restartable or intermittently operated rocket-engine plants F02K 9/94) [3, 2006.01]
F02K   9/82  \	2	2	3G106	F02K   9/82	19	åӵήΤʮͤΡΣ	by injection of a secondary fluid into the rocket exhaust gases [3]
F02K   9/84  \	2	2	3G106	F02K   9/84	79	ưΥѤΡΣ	using movable nozzles [3]
F02K   9/86  \	2	2	3G106	F02K   9/86	46	Υ륹ѤĴǽʤΡΣ	using nozzle throats of adjustable cross-section [3]
F02K   9/88  \	2	2	3G106	F02K   9/88	34	åȥΥѤΡΣ	using auxiliary rocket nozzles [3]
F02K   9/90  \	2	2	3G106	F02K   9/90	46	и֤ѤΡʣƣˣͥˡΣ	using deflectors (F02K 9/82 takes precedence) [3]
F02K   9/92  \	2	2	3G106	F02K   9/92	8	ϤžޤϽ뤵뤿μʤȷ礷ΡΣ	incorporating means for reversing or terminating thrust [3]
F02K   9/94  \	1	1	3G106	F02K   9/94	27	ФޤϺƻưǽʥåȥ󥸥ַŪ˺ưåȥ󥸥Σ	Re-ignitable or restartable rocket-engine plants; Intermittently operated rocket-engine plants [3, 2006.01]
F02K   9/95  \	1	1	3G106	F02K   9/95	222	ưޤмʤޤ֤ˤäħŤ줿Ρʰ֣ƣˣˡΣ	characterised by starting or ignition means or arrangements (safety devices F02K 9/38) [3]
F02K   9/96  \	1	1	3G106	F02K   9/96	127	ޤϷ¬ΤäŬ礷֤ˤäħŤ줿ΡΣ	characterised by specially adapted arrangements for testing or measuring [3]
F02K   9/97  \	1	1	3G106	F02K   9/97	255	åȥΥʿϤޤϿϥ٥ȥƣˣˡΣ	Rocket nozzles (thrust or thrust vector control F02K 9/80) [3]
F02K  99/00  \	0	0	3G106	F02K  99/00	107	Υ֥饹¾Υ롼פʬवʤࡡΣ	Subject matter not provided for in other groups of this subclass [2009.01]
