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| SECTION B PERFORMING OPERATIONS; TRANSPORTING |
| B 64 | AIRCRAFT; AVIATION; COSMONAUTICS |
| B 64 C | AEROPLANES; HELICOPTERS (air-cushion vehicles B60V) |
13/ | 00 | Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers |
13/ | 02 | . | Initiating means |
13/ | 04 | . | . | actuated personally |
13/ | 06 | . | . | . | adjustable to suit individual persons |
13/ | 08 | . | . | . | Trimming zero positions |
13/ | 10 | . | . | . | comprising warning devices |
13/ | 12 | . | . | . | Dual control apparatus |
13/ | 14 | . | . | . | lockable (locking in position to suit individual persons B64C 13/06) |
13/ | 16 | . | . | actuated automatically, e.g. responsive to gust detectors |
13/ | 18 | . | . | . | using automatic pilot (automatic pilots per se G05D 1/00) |
13/ | 20 | . | . | . | using radiated signals |
13/ | 22 | . | . | . | readily revertible to personal control |
13/ | 24 | . | Transmitting means |
13/ | 26 | . | . | without power amplification or where power amplification is irrelevant |
13/ | 28 | . | . | . | mechanical |
13/ | 30 | . | . | . | . | using cable, chain, or rod mechanisms |
13/ | 32 | . | . | . | . | using cam mechanisms |
13/ | 34 | . | . | . | . | using toothed gearing |
13/ | 36 | . | . | . | fluid |
13/ | 38 | . | . | with power amplification |
13/ | 40 | . | . | . | using fluid pressure |
13/ | 42 | . | . | . | . | having duplication or stand-by provisions |
13/ | 44 | . | . | . | . | overriding of personal controls; with automatic return to inoperative position |
13/ | 46 | . | . | . | . | with artificial feel |
13/ | 48 | . | . | . | . | characterised by the fluid being gaseous |
13/ | 50 | . | . | . | using electrical energy |
15/ | 00 | Attitude, flight direction, or altitude control by jet reaction (details of jet-engine plants, e.g. of nozzles or jet pipes, F02K) [3] |
15/ | 02 | . | the jets being propulsion jets |
15/ | 12 | . | . | the power plant being tiltable |
15/ | 14 | . | the jets being other than main propulsion jets (jet flaps B64C 9/38) |
17/ | 00 | Aircraft stabilisation not otherwise provided for |
17/ | 02 | . | by gravity or inertia-actuated apparatus |
17/ | 04 | . | . | by pendular bodies |
17/ | 06 | . | . | by gyroscopic apparatus (automatic-pilot control B64C 13/18) |
17/ | 08 | . | by ballast supply or discharge (for lighter-than-air aircraft B64B) |
17/ | 10 | . | Transferring fuel to adjust trim |
19/ | 00 | Aircraft control not otherwise provided for |
19/ | 02 | . | Conjoint controls |
| Influencing air-flow over aircraft surfaces, not otherwise provided for |
21/ | 00 | Influencing air-flow over aircraft surfaces by affecting boundary-layer flow (boundary-layer control in general F15D) |
21/ | 02 | . | by use of slot, ducts, porous areas, or the like |
21/ | 04 | . | . | for blowing (B64C 21/08 takes precedence) |
21/ | 06 | . | . | for sucking (B64C 21/08 takes precedence) |
21/ | 08 | . | . | adjustable |
21/ | 10 | . | using other surface properties, e.g. roughness |
23/ | 00 | Influencing air-flow over aircraft surfaces, not otherwise provided for |
23/ | 02 | . | by means of rotating members of cylindrical or similar form |
23/ | 04 | . | by generating shock waves |
23/ | 06 | . | by generating vortices |
23/ | 08 | . | using Magnus effect |
25/ | 00 | Alighting gear (air-cushion alighting gear B60V 3/08) |
25/ | 02 | . | Undercarriages |
25/ | 04 | . | . | Arrangement or disposition on aircraft |
25/ | 06 | . | . | fixed |
25/ | 08 | . | . | non-fixed, e.g. jettisonable |
25/ | 10 | . | . | . | retractable, foldable, or the like |
25/ | 12 | . | . | . | . | sideways |
25/ | 14 | . | . | . | . | fore-and-aft |
25/ | 16 | . | . | . | . | Fairings movable in conjunction with undercarriage elements |
25/ | 18 | . | . | . | . | Operating mechanisms |
25/ | 20 | . | . | . | . | . | mechanical |
25/ | 22 | . | . | . | . | . | fluid |
25/ | 24 | . | . | . | . | . | electric |
25/ | 26 | . | . | . | . | . | Control or locking systems therefor |
25/ | 28 | . | . | . | . | . | . | with indicating or warning devices |
25/ | 30 | . | . | . | . | . | . | emergency actuated |
25/ | 32 | . | characterised by elements which contact the ground or similar surface (arrester hooks B64C 25/68) |
25/ | 34 | . | . | wheeled type, e.g. multi-wheeled bogies |
25/ | 36 | . | . | . | Arrangements or adaptations of wheels, tyres, or axles in general (construction of wheels or axles B60B; construction of tyres in general B60C) |
25/ | 38 | . | . | endless-track type |
25/ | 40 | . | . | the elements being rotated before touch-down |
25/ | 42 | . | . | Arrangement or adaptation of brakes (the ground braking force being regulated, at least in part, by a speed condition, e.g. acceleration or deceleration of the ground engaging alighting gear, B60T 8/32) [4] |
25/ | 44 | . | . | . | Actuating mechanisms |
25/ | 46 | . | . | . | . | Brake regulators for preventing skidding or aircraft somersaulting |
25/ | 48 | . | . | . | . | differentially operated for steering purposes |
25/ | 50 | . | . | Steerable undercarriages; Shimmy-damping (steering devices applicable to land vehicles B62D) |
25/ | 52 | . | . | Skis or runners |
25/ | 54 | . | . | Floats |
25/ | 56 | . | . | . | inflatable (connection of valves to inflatable elastic bodies B60C 29/00) |
25/ | 58 | . | . | Arrangements or adaptations of shock-absorbers or springs (shimmy-dampers B64C 25/50; vehicle suspension arrangements in general B60G; shock-absorbers per se F16F) |
25/ | 60 | . | . | . | Oleo legs |
25/ | 62 | . | . | . | Spring shock-absorbers; Springs |
25/ | 64 | . | . | . | . | using rubber or like elements |
25/ | 66 | . | . | Convertible alighting gear; Combinations of different kinds of ground or like engaging elements |
25/ | 68 | . | Arrester hooks (arresting gear, e.g. on aircraft carriers, B64F) |
| Aircraft kinds or components not otherwise provided for |
27/ | 00 | Rotorcraft; Rotors peculiar thereto (alighting gear B64C 25/00) |
27/ | 02 | . | Gyroplanes |
27/ | 04 | . | Helicopters |
27/ | 06 | . | . | with single rotor |
27/ | 08 | . | . | with two or more rotors |
27/ | 10 | . | . | . | arranged coaxially |
27/ | 12 | . | . | Rotor drives |
27/ | 14 | . | . | . | Direct drive between power plant and rotor hub |
27/ | 16 | . | . | . | Drive of rotors by means, e.g. propellers, mounted on rotor blades |
27/ | 18 | . | . | . | . | the means being jet-reaction apparatus |
27/ | 20 | . | Rotorcraft characterised by having shrouded rotors, e.g. flying platforms |
27/ | 22 | . | Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft |
27/ | 24 | . | . | with rotor blades fixed in flight to act as lifting surfaces |
27/ | 26 | . | . | characterised by provision of fixed wings |
27/ | 28 | . | . | with forward-propulsion propellers pivotable to act as lifting rotors |
27/ | 30 | . | . | with provision for reducing drag of inoperative rotor |
27/ | 32 | . | Rotors (features common to rotors and propellers B64C 11/00) |
27/ | 33 | . | . | having flexing arms [3] |
27/ | 35 | . | . | having elastomeric joints [3] |
27/ | 37 | . | . | having articulated joints (B64C 27/33, B64C 27/35 take precedence) [3] |
27/ | 39 | . | . | . | with individually articulated blades, i.e. with flapping or drag hinges [3] |
27/ | 41 | . | . | . | with flapping hinge or universal joint, common to the blades [3] |
27/ | 43 | . | . | . | . | see-saw type, i.e. two-bladed rotor [3] |
27/ | 45 | . | . | . | with a feathering hinge only [3] |
27/ | 46 | . | . | Blades |
27/ | 467 | . | . | . | Aerodynamic features [6] |
27/ | 473 | . | . | . | Constructional features [6] |
27/ | 48 | . | . | . | . | Root attachment to rotor head |
27/ | 50 | . | . | . | . | Blades foldable to facilitate stowage of aircraft |
27/ | 51 | . | Damping of blade movements [3] |
27/ | 52 | . | Tilting of rotor bodily relative to fuselage (of see-saw type construction B64C 27/43) |
27/ | 54 | . | Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement |
27/ | 56 | . | . | characterised by the control initiating means, e.g. manually actuated (B64C 27/58 takes precedence) |
27/ | 57 | . | . | . | automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust [3] |
27/ | 58 | . | . | Transmitting means, e.g. interrelated with initiating means or means acting on blades (initiating means B64C 27/56; means acting on blades B64C 27/72) |
27/ | 59 | . | . | . | mechanical [3] |
27/ | 605 | . | . | . | . | including swash plate, spider or cam mechanisms [3] |
27/ | 615 | . | . | . | . | including flaps mounted on blades [3] |
27/ | 625 | . | . | . | . | including rotating masses or servo rotors [3] |
27/ | 635 | . | . | . | . | specially for controlling lag-lead movements of blades [3] |
27/ | 64 | . | . | . | using fluid pressure, e.g. having fluid power amplification [3] |
27/ | 68 | . | . | . | using electrical energy, e.g. having electrical power amplification [3] |
27/ | 72 | . | . | Means acting on blades |
27/ | 78 | . | . | in association with pitch adjustment of blades of anti-torque rotor |
27/ | 80 | . | . | for differential adjustment of blade pitch between two or more lifting rotors |
27/ | 82 | . | characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting-rotor torque or changing direction of rotorcraft |
29/ | 00 | Aircraft capable of landing or taking-off vertically (attitude, flight direction, or altitude control by jet reaction B64C 15/00; rotorcraft B64C 27/00; air-cushion vehicles B60V; details of jet-engine plants, e.g. of nozzles or jet pipes, F02K) |
29/ | 02 | . | having its flight directional axis vertical when grounded |
29/ | 04 | . | . | characterised by jet-reaction propulsion |
30/ | 00 | Supersonic type aircraft [3] |
31/ | 00 | Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft |
31/ | 02 | . | Gliders, e.g. sailplanes (hang-gliders B64C 31/028) [6] |
31/ | 024 | . | . | with auxiliary power plant [6] |
31/ | 028 | . | Hang-glider-type aircraft; Microlight-type aircraft [6] |
31/ | 032 | . | . | having delta shaped wing [6] |
31/ | 036 | . | . | having parachute-type wing (parachutes B64D 17/00) [6] |
31/ | 04 | . | Man-powered aircraft (ornithopters B64C 33/00) |
31/ | 06 | . | Kites (hang-gliders B64C 31/028; toy aspects A63H 27/08; towed targets F41J) |
33/ | 00 | Ornithopters |
33/ | 02 | . | Wings; Actuating mechanisms therefor |
35/ | 00 | Flying-boats; Seaplanes (alighting gear B64C 25/00) |
35/ | 02 | . | Flying-boat hulls [3] |
37/ | 00 | Convertible aircraft (vehicles capable of travelling in or on different media B60F) |
37/ | 02 | . | Flying units formed by separate aircraft (towing, air-refuelling, or aircraft-carrying aircraft B64D) |
39/ | 00 | Aircraft not otherwise provided for |
39/ | 02 | . | characterised by special use |
39/ | 04 | . | having multiple fuselages or tail booms [3] |
39/ | 06 | . | having disc- or ring-shaped wings [3] |
39/ | 08 | . | having multiple wings [3] |
39/ | 10 | . | All-wing aircraft [3] |
39/ | 12 | . | Canard-type aircraft [3] |
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