| Outline |
Indent Level
| |
| Color | Curly Brackets (indicating CPC extensions to IPC) | |
CPC | COOPERATIVE PATENT CLASSIFICATION | |||||
![]() | AEROPLANES ; HELICOPTERS ( air-cushion vehicles B60V ) NOTE -
WARNING -
|
![]() | Guide Heading: | Aircraft structures or fairings ( boundary-layer controls B64C 21/00 ) |
![]() | Fuselages ; Constructional features common to fuselages, wings, stabilising surfaces and the like ( aerodynamical features common to fuselages, wings, stabilising surfaces, and the like B64C 23/00 ; flight-deck installations B64D ) |
B64C 1/0009 | . | { Aerodynamic aspects } |
![]() | . | Frames ; Stringers ; Longerons; { Fuselage sections } |
![]() | . . | { Frames } |
B64C 1/062 | . . . | { specially adapted to absorb crash loads } |
B64C 1/063 | . . . | { Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms ( folding or collapsing wings B64C 3/56 ) } |
B64C 1/064 | . . | { Stringers; Longerons } |
B64C 1/065 | . . | { Spars } |
![]() | . . | { Interior liners } |
![]() | . . | { Fuselage sections } |
B64C 1/08 | . . | Geodetic or other open-frame structures |
B64C 1/10 | . . | Bulkheads |
B64C 1/12 | . . | Construction or attachment of skin panels |
![]() | . | Windows ; Doors ; Hatch covers or access panels ; Surrounding frame structures ; Canopies ; Windscreens { accessories therefor, e.g. pressure sensors, water deflectors, hinges, seals, handles, latches, windscreen wipers } ( fairings movable in conjunction with undercarriage elements B64C 25/16 ; bomb doors B64D 1/06 ) |
![]() | . . | { Doors; surrounding frames } |
B64C 1/1415 | . . . | { Cargo doors, e.g. incorporating ramps } |
![]() | B64C 1/1423 | . . . | { Passenger doors } |
B64C 1/1446 | . . . |
B64C 1/1453 | . . . | { Drain masts } |
B64C 1/1461 | . . . | { Structures of doors or surrounding frames } |
B64C 1/1469 | . . . | { Doors between cockpit and cabin } |
![]() | . . | { Canopies; Windscreens or similar transparent elements } |
B64C 1/16 | . | specially adapted for mounting power plant |
![]() | . | Floors |
B64C 1/22 | . | Other structures integral with fuselages to facilitate loading { e.g. cargo bays, cranes ( cargo door type ramps B64C 1/1415 ) } |
B64C 1/24 | . | Step mounted on an retractable within fuselages ( readily removable B64D 9/00 ) |
B64C 1/26 | . | Attaching the wing or tail units or stabilising surfaces |
B64C 1/28 | . | Parts of fuselage relatively movable to improve pilots view |
B64C 1/30 | . | Parts of fuselage relatively movable to reduce overall size for storage |
B64C 1/32 | . | Severable or jettisonable parts of fuselage facilitating emergency escape ( ejector seats B64D 25/10 ) |
B64C 1/34 | . | comprising inflatable structural components ( connection of valves to inflatable elastic bodies B60C 29/00 ) |
B64C 1/36 | . | adapted to receive aerials or radomes ( aerials or radomes per se H01Q ) |
B64C 1/38 | . | Constructions adapted to reduce effects of aerodynamic or other external heating { ( cooling structural parts of aircrafts with air flow B64D 13/006 ) } |
![]() | . | Sound or heat insulation, { e.g. using insulation blankets ( insulating elements for vehicles, in general B60R 13/08 ) } |
![]() | . . | { Arrangement of fasteners specially adapted therefor, e.g. of clips ( in vehicles in general B60R 13/0206 ) } |
B64C 1/406 | . . . | { in combination with supports for lines, e.g. for pipes or cables ( arrangement of elements of electric or fluid circuits specially adapted for vehicles, in general B60R 16/00 ; supports for pipes, cables or protective tubing F16L 3/00 ; installations of electric cables or lines in vehicles H02G 3/00 ) } |
![]() | Wings ( stabilising surfaces B64C 5/00 ; ornithopter wings B64C 33/02 ) |
![]() | B64C 3/10 | . | Shape of wings |
![]() | . | Spars ; Ribs ; Stringers ( attaching wing unit to fuselage B64C 1/26 ) |
B64C 3/20 | . | Integral or sandwich constructions ( layered products or sandwich constructions in general B32B ) |
B64C 3/22 | . | Geodetic or other open-frame structures |
B64C 3/24 | . | Moulded or cast structures |
B64C 3/26 | . | Construction, shape, or attachment of separate skins, e.g. panels |
B64C 3/28 | . | Leading or trailing edges attached to primary structures, e.g. forming fixed slots |
B64C 3/30 | . | comprising inflatable structural components ( connection of valves to inflatable elastic bodies B60C 29/00 ) |
B64C 3/32 | . | specially adapted for mounting power plant |
B64C 3/34 | . | Integrally-constructed tanks, e.g. for fuel ( other aircraft fuel tanks or fuel systems B64D ) |
B64C 3/36 | . | Structures adapted to reduce effects of aerodynamic or other external heating { ( cooling structural parts of aircrafts with air flow B64D 13/006 ) } |
![]() | B64C 3/38 | . | Adjustment of complete wings or parts thereof |
B64C 3/385 | . . | { Variable incidence wings } |
B64C 3/40 | . . | Varying angle of sweep |
B64C 3/42 | . . | Adjusting about chordwise axes |
![]() | B64C 3/44 | . . | Varying camber |
B64C 3/46 | . . . | by inflatable elements ( connection of valves to inflatable elastic bodies B60C 29/00 ) |
B64C 3/48 | . . . | by relatively-movable parts of wing structures |
B64C 3/50 | . . . | by leading or trailing edge flaps ( ailerons B64C 9/00 ) |
B64C 3/52 | . . | Warping |
![]() | . . | Varying in area ( flaps extendable to increase camber B64C 3/44 ) |
B64C 3/56 | . . | Folding or collapsing to reduce overall dimensions of aircraft |
B64C 3/58 | . | provided with fences or spoilers ( adjustable for control purposes B64C 9/00 ) |
![]() | Stabilising surfaces ( attaching stabilising surfaces to fuselage B64C 1/26 ) |
B64C 5/02 | . | Tailplanes ( fins B64C 5/06 ) |
B64C 5/04 | . | Noseplanes |
B64C 5/06 | . | Fins ( specially for wings B64C 5/08 ) |
B64C 5/08 | . | mounted on or supported by wings |
![]() | . | adjustable |
B64C 5/12 | . . | for retraction against or within fuselage or nacelle |
B64C 5/14 | . . | Varying angle of sweep |
B64C 5/16 | . . | about spanwise axes |
B64C 5/18 | . . | in area ( attaching stabilising surfaces to fuselage B64C 1/26 ) |
![]() | Structures or fairings not otherwise provided for |
![]() | Adjustable control surfaces or members, e.g. rudders ( trimming stabilising surfaces B64C 5/10 ) |
B64C 9/02 | . | Mounting or supporting thereof |
B64C 9/04 | . | with compound dependent movements |
B64C 9/06 | . | with two or more independent movements |
B64C 9/08 | . | bodily displaceable ( varying camber of wings B64C 3/44 ) |
B64C 9/10 | . |
B64C 9/12 | . | surfaces of different type or function being simultaneously adjusted |
![]() | . | forming slots ( boundary-layer control B64C 21/00 ) |
B64C 9/146 | . . | { at an other wing location than the rear or the front ( wings provided with fixed fences or spoilers B64C 3/58 ) } |
![]() | . . | at the rear of the wing |
![]() | . . | at the front of the wing |
B64C 9/28 | . . | by flaps at both the front and rear of the wing operating in unison |
B64C 9/30 | . | Balancing hinged surfaces, e.g. dynamically |
![]() | . | Air braking surfaces ( braking by parachutes B64D 17/80 ) |
![]() | . | collapsing or retracting against or within other surfaces or other members |
B64C 9/38 | . | Jet flaps |
![]() | Propellers, e.g. of ducted type ; Features common to propellers and rotors for rotorcraft ( rotors specially adapted for rotorcraft B64C 27/32 ) NOTE -
|
B64C 11/001 | . | { Shrouded propellers } |
B64C 11/002 | . | { Braking propellers, e.g. for measuring the power output of an engine } |
B64C 11/003 | . | { Variable-diameter propellers; Mechanisms therefor } |
B64C 11/005 | . | { Spiral-shaped propellers } |
B64C 11/006 | . | { Paddle wheels } |
B64C 11/007 | . | { Propulsive discs, i.e. discs having the surface specially adapted for propulsion purposes } |
B64C 11/008 | . |
![]() | B64C 11/02 | . | Hub construction |
![]() | B64C 11/04 | . . | Blade mountings |
B64C 11/14 | . . | Spinners |
![]() | B64C 11/16 | . | Blades |
![]() | B64C 11/30 | . | Blade pitch-changing mechanisms NOTE -
|
B64C 11/301 | . . | { characterised by blade position indicating means } |
B64C 11/303 | . . | { characterised by comprising a governor } |
B64C 11/305 | . . | { characterised by being influenced by other control systems, e.g. fuel supply } |
![]() | B64C 11/306 | . . | { specially adapted for contrarotating propellers } |
![]() | B64C 11/32 | . . | mechanical |
B64C 11/325 | . . . | { comprising feathering, braking or stopping systems } |
![]() | B64C 11/34 | . . . | automatic |
B64C 11/343 | . . . . | { actuated by the centrifugal force or the aerodynamic drag acting on the blades } |
B64C 11/346 | . . . . | { actuated by the centrifugal force or the aerodynamic drag acting on auxiliary masses or surfaces } |
B64C 11/36 | . . . | non-automatic |
![]() | B64C 11/38 | . . | fluid, e.g. hydraulic |
B64C 11/385 | . . . | { comprising feathering, braking or stopping systems } |
B64C 11/40 | . . . | automatic |
B64C 11/42 | . . . | non-automatic |
B64C 11/44 | . . | electric |
![]() | . | Arrangements of or constructional features peculiar to multiple propellers { ( B64C 11/306 takes precedence ) } |
![]() | Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers |
![]() | B64C 13/02 | . | Initiating means |
![]() | . . | actuated personally |
B64C 13/06 | . . . | adjustable to suit individual persons |
B64C 13/08 | . . . | Trimming zero positions |
B64C 13/10 | . . . | comprising warning devices |
B64C 13/12 | . . . | Dual control apparatus |
B64C 13/14 | . . . | lockable ( locking in position to suit individual persons B64C 13/06 ) |
![]() | . . | actuated automatically, e.g. responsive to gust detectors |
![]() | . | Transmitting means |
![]() | B64C 13/26 | . . | without power amplification or where power amplification is irrelevant |
![]() | B64C 13/28 | . . . | mechanical |
B64C 13/30 | . . . . | using cable, chain, or rod mechanisms |
B64C 13/32 | . . . . | using cam mechanisms |
B64C 13/34 | . . . . | using toothed gearing |
B64C 13/36 | . . . | fluid |
![]() | B64C 13/38 | . . | with power amplification |
![]() | . . . | using fluid pressure |
B64C 13/42 | . . . . | having duplication or stand-by provisions |
B64C 13/44 | . . . . | overriding of personal controls ; with automatic return to inoperative position |
B64C 13/46 | . . . . | with artificial feel |
B64C 13/48 | . . . . | characterised by the fluid being gaseous |
![]() | B64C 13/50 | . . . | using electrical energy |
![]() | Attitude, flight direction, or altitude control by jet reaction |
![]() | . | the jets being propulsion jets |
B64C 15/14 | . | the jets being other than main propulsion jets ( jet flaps B64C 9/38 ) |
![]() | Aircraft stabilisation not otherwise provided for |
![]() | . | by gravity or inertia-actuated apparatus |
B64C 17/04 | . . | by pendular bodies |
B64C 17/06 | . . | by gyroscopic apparatus ( automatic pilot control B64C 13/18 ) |
B64C 17/08 | . | by ballast supply or discharge ( for lighter-than-air aircraft B64B ) |
B64C 17/10 | . | Transferring fuel to adjust trim |
![]() | Aircraft control not otherwise provided for |
![]() | Guide Heading: | Influencing air-flow over aircraft surfaces, not otherwise provided for |
![]() | Influencing air-flow over aircraft surfaces by affecting boundary-layer flow ( boundary-layer control in general F15D ) |
![]() | . | by use of slot, ducts, porous areas, or the like |
B64C 21/025 | . . | { for simultaneous blowing and sucking } |
B64C 21/04 | . . | for blowing ( B64C 21/08 takes precedence ) |
B64C 21/06 | . . | for sucking ( B64C 21/08 takes precedence ) |
B64C 21/08 | . . | adjustable |
B64C 21/10 | . | using other surface properties, e.g. roughness |
![]() | Influencing air-flow over aircraft surfaces, not otherwise provided for |
B64C 23/005 | . | { by other means not covered by groups B64C 23/02 to B64C 23/08 , e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds } |
B64C 23/02 | . | by means of rotating members of cylindrical or similar form |
B64C 23/04 | . | by generating shock waves |
![]() | . | by generating vortices |
B64C 23/08 | . | using Magnus effect |
![]() | Alighting gear ( air-cushion alighting gear B60V 3/08 ) |
B64C 25/001 | . |
![]() | B64C 25/02 | . | Undercarriages |
B64C 25/04 | . . | Arrangement or disposition on aircraft |
B64C 25/06 | . . | fixed |
![]() | B64C 25/08 | . . | non-fixed, e.g. jettisonable |
![]() | B64C 25/10 | . . . | retractable, foldable, or the like |
![]() | . | characterised by the ground or like engaging elements ( arrester hooks B64C 25/68 ) |
![]() | B64C 25/34 | . . | wheeled type, e.g. multi-wheeled bogies |
B64C 25/38 | . . | Endless-track type |
![]() | . . | the elements being rotated before touch-down |
![]() | . . | Arrangements or adaptations 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 ) |
B64C 25/423 | . . . | { Braking devices acting by reaction of gaseous medium ( B64C 25/426 takes precedence; using rockets B64D 27/023 ) } |
B64C 25/426 | . . . | { Braking devices providing an automatic sequence of braking } |
![]() | . . . | Actuating mechanisms |
B64C 25/445 | . . . . | { Brake regulators for preventing somersaulting } |
B64C 25/46 | . . . . | Brake regulators for preventing skidding or aircraft somersaulting { ( anti-skidding regulators; electric or electronic controllers therefor B60T 8/1703 ) } |
B64C 25/48 | . . . . | differentially operated for steering purposes |
![]() | . . | Steerable undercarriages ; Shimmy damping ( steering devices applicable to land vehicles B62D ) |
B64C 25/52 | . . | Skis or runners |
![]() | B64C 25/54 | . . | Floats |
B64C 25/56 | . . . | inflatable ( connection of valves to inflatable elastic bodies B60C 29/00 ) |
![]() | . . | Arrangements or adaptations of shock-absorbers or springs ( shimmy dampers B64C 25/50 ; vehicle suspension arrangements in general B60G ; shock absorber per se F16F ) |
B64C 25/66 | . . | Convertible alighting gear ; Combinations of different kinds of ground or like engaging elements |
B64C 25/68 | . | Arrester hooks ( arresting gear, e.g. on aircraft carriers B64F ) |
![]() | Guide Heading: | Aircraft kinds and components not otherwise provided for |
![]() | Rotorcraft ; Rotors peculiar thereto ( alighting gear B64C 25/00 ) |
B64C 27/001 | . | { Vibration damping devices } |
![]() | . | { Safety devices } |
B64C 27/008 | . | { Rotors tracking or balancing devices } |
![]() | B64C 27/02 | . | Gyroplanes |
![]() | . . |
B64C 27/022 | . . . | { Devices for folding or adjusting the blades } |
B64C 27/023 | . . . | { Construction of the blades; Coating of the blades } |
B64C 27/024 | . . . | { Devices for shifting the rotor axis } |
B64C 27/025 | . . . | { Rotor drives, in particular for taking off; Combination of autorotation rotors and driven rotors } |
B64C 27/026 | . . . | { Devices for converting a fixed wing into an autorotation rotor and viceversa } |
B64C 27/027 | . . | { Control devices using other means than the rotor } |
B64C 27/028 | . . | { Other constructional elements; Rotor balancing } |
![]() | . | Helicopters |
B64C 27/20 | . | Rotorcraft characterised by having shrouded rotors, e.g. flying platforms |
![]() | B64C 27/22 | . | Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft |
B64C 27/24 | . . | with rotor blades fixed in flight to act as lifting surfaces |
B64C 27/26 | . . | characterised by provision of fixed wings |
B64C 27/28 | . . | with forward-propulsion propellers pivotable to act as lifting rotors |
B64C 27/30 | . . | with provision for reducing drag of inoperative rotor |
![]() | . | Rotors ( features common to rotors and propellers B64C 11/00 ) |
B64C 27/322 | . . | { Blade travel limiting devices, e.g. droop stops } |
B64C 27/325 | . . | { Circulation-control rotors } |
B64C 27/327 | . . | { Retention means relieving the stress from the arm, e.g. tie-bars } |
B64C 27/33 | . . | having flexing arms |
B64C 27/35 | . . | having elastomeric joints |
![]() | . . | having articulated joints ( B64C 27/33 , B64C 27/35 take precedence ) |
B64C 27/39 | . . . | with individually articulated blades, i.e. with flapping or drag hinges |
![]() | B64C 27/41 | . . . | with flapping or universal joint, common to the blades |
B64C 27/45 | . . . | with a feathering hinge only |
![]() | B64C 27/46 | . . | Blades |
B64C 27/51 | . | { Damping of blade movements } |
B64C 27/52 | . | Tilting of rotor bodily relative to fuselage ( of see-saw type construction B64C 27/43 ) |
![]() | B64C 27/54 | . | Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement |
![]() | . . | Initiating means, e.g. actuated personally |
![]() | . . | Transmitting means |
![]() | B64C 27/59 | . . . | mechanical |
B64C 27/605 | . . . . | including swash plate, spider or cam mechanisms |
B64C 27/615 | . . . . | including flaps mounted on blades |
B64C 27/625 | . . . . | including rotating masses or servo rotors |
B64C 27/635 | . . . . | specially for controlling lag-lead movements of blades |
B64C 27/64 | . . . . | using fluid pressure |
B64C 27/68 | . . . . | using electrical energy |
B64C 27/72 | . . | Means acting on blades |
B64C 27/78 | . . | in association with pitch adjustment of blades of anti-torque rotor |
B64C 27/80 | . . | for differential adjustment of blade pitch between two or more lifting rotors |
B64C 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 |
![]() | 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 ) |
![]() | B64C 29/0008 | . | { having its flight directional axis horizontal when grounded } |
![]() | B64C 29/0016 | . . | { the lift during taking-off being created by free or ducted propellers or by blowers } |
B64C 29/0025 | . . . | { the propellers being fixed relative to the fuselage } |
B64C 29/0033 | . . . | { the propellers being tiltable relative to the fuselage } |
![]() | B64C 29/0041 | . . | { the lift during taking-off being created by jet motors } |
B64C 29/005 | . . . | { the motors being fixed relative to the fuselage } |
B64C 29/0058 | . . . | { with vertical jet } |
B64C 29/0066 | . . . | { with horizontal jet and jet deflector } |
B64C 29/0075 | . . . | { the motors being tiltable relative to the fuselage } |
B64C 29/0083 | . . | { the lift during taking-off being created by several motors of different type } |
B64C 29/0091 | . | { Accessories not provided for elsewhere } |
![]() | B64C 29/02 | . | having its flight directional axis vertical when grounded |
B64C 30/00 | Supersonic-type aircraft |
![]() | Aircraft intended to be sustained without power plant ; Powered hang-glider-type aircraft ; Microlight-type aircraft |
![]() | . | Gliders, e.g. sailplanes ( hang-gliders B64C 31/028 ) |
![]() | . | Hang-glider-type aircraft ; Microlight-type aircraft |
B64C 31/0285 | . . | { Safety devices } |
B64C 31/032 | . . | having delta shaped wing |
B64C 31/036 | . . | having parachute-type wing ( parachutes B64D 17/00 ) |
B64C 31/04 | . | Man-powered aircraft ( ornithopters B64C 33/00 ) |
B64C 31/06 | . | Kites ( hang-gliders B64C 31/028 ; toy aspects A63H 27/08 ; towed targets F41J { for propelling boats B63H 9/0685 ; for propelling wind driven boards, control means and harnesses therefor B63B 35/7976 } ) |
![]() | Ornithopters |
![]() | Flying-boats ; Seaplanes ( alighting gear B64C 25/00 ) |
![]() | B64C 35/001 | . | { with means for increasing stability on the water } |
B64C 35/002 | . . | { using adjustable auxiliary floats } |
B64C 35/003 | . . | { using auxiliary floats at the wing tips } |
B64C 35/005 | . | { with propellers, rudders or brakes acting in the water } |
B64C 35/006 | . | { with lift generating devices } |
B64C 35/007 | . | { Specific control surfaces therefor } |
B64C 35/008 | . | { Amphibious sea planes } |
![]() | Convertible aircraft ( vehicles capable of travelling in or on different media B60F ) |
B64C 37/02 | . | Flying units formed by separate aircraft ( towing, air-refuelling, or aircraft-carrying aircraft B64D ) |
![]() | Aircraft not otherwise provided for |
B64C 39/001 | . | { Flying saucers } |
![]() | . | { with wings, paddle wheels, bladed wheels, moving or rotating in relation to the fuselage ( rotorcraft B64C 27/00 , ornithopters B64C 33/00 ) } |
B64C 39/005 | . . | { about a horizontal transversal axis } |
B64C 39/006 | . . | { about a vertical axis } |
B64C 39/008 | . . | { about a longitudinal axis } |
![]() | B64C 39/02 | . | characterised by special use |
B64C 39/022 | . . | { Tethered aircraft } |
B64C 39/024 | . . | { of the remote controlled vehicle type, i.e. RPV } |
B64C 39/026 | . . | { for use as personal propulsion unit } |
B64C 39/028 | . . | { Micro-sized aircraft } |
B64C 39/04 | . | having multiple fuselages or tail booms |
![]() | . |
![]() | B64C 39/062 | . . | { having annular wings } |
B64C 39/066 | . . | { having channel wings } |
B64C 39/068 | . . | { having multiple wings joined at the tips } |
B64C 39/08 | . |
B64C 39/10 | . |
B64C 39/12 | . | Canard-type aircraft |
![]() | B64C 2001/00 | Fuselages ; Constructional features common to fuselages, wings, stabilising surfaces and the like ( aerodynamical features common to fuselages, wings, stabilising surfaces, and the like B64C 23/00 ; flight-deck installations B64D ) |
![]() | B64C 2001/0018 | . | comprising two decks adapted for carrying passengers only |
B64C 2001/0027 | . . | arranged one above the other |
B64C 2001/0036 | . . | arranged side by side at the same level |
B64C 2001/0045 | . | Fuselages characterised by special shapes |
![]() | B64C 2001/0054 | . | Fuselage structures substantially made from particular materials |
B64C 2001/0063 | . . | from wood |
B64C 2001/0072 | . . | from composite materials |
B64C 2001/0081 | . . | from metallic materials |
B64C 2001/009 | . | comprising decompression panels or valves for pressure equalisation in fuselages or floors |
![]() | B64C 2003/00 | Wings ( stabilising surfaces B64C 5/00 ; ornithopter wings B64C 33/02 ) |
![]() | B64C 2003/10 | . | Shape of wings |
![]() | B64C 2003/14 | . . | Aerofoil profile |
B64C 2003/142 | . . . | with variable camber along the airfoil chord |
B64C 2003/143 | . . . | comprising interior channels |
B64C 2003/144 | . . . | including a flat surface on either the extrados or intrados |
B64C 2003/145 | . . . | comprising 'Gurney' flaps |
B64C 2003/146 | . . . | comprising leading edges of particular shape |
B64C 2003/147 | . . . | comprising trailing edges of particular shape |
B64C 2003/148 | . . . | comprising protuberances, e.g. for modifying boundary layer flow |
B64C 2003/149 | . . . | for supercritical or transonic flow |
![]() | B64C 2003/38 | . | Adjustment of complete wings or parts thereof |
![]() | B64C 2003/44 | . . | Varying camber |
![]() | B64C 2003/54 | . . | Varying in area ( flaps extendable to increase camber B64C 3/44 ) |
![]() | B64C 2009/00 | Adjustable control surfaces or members, e.g. rudders ( trimming stabilising surfaces B64C 5/10 ) |
B64C 2009/005 | . | Ailerons |
![]() | B64C 2009/14 | . | forming slots ( boundary-layer control B64C 21/00 ) |
![]() | B64C 2013/00 | Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers |
![]() | B64C 2025/00 | Alighting gear ( air-cushion alighting gear B60V 3/08 ) |
![]() | B64C 2025/001 | . |
B64C 2025/003 | . . | Means for reducing landing gear noise, or turbulent flow around it, e.g. landing gear doors used as deflectors |
B64C 2025/005 | . . | Tail skids for fuselage tail strike protection on tricycle landing gear aircraft |
B64C 2025/006 | . . | Landing gear legs comprising torque arms |
B64C 2025/008 | . . | Comprising means for modifying their length, e.g. for kneeling, for jumping, or for leveling the aircraft |
![]() | B64C 2025/02 | . | Undercarriages |
![]() | B64C 2025/32 | . | characterised by the ground or like engaging elements ( arrester hooks B64C 25/68 ) |
![]() | B64C 2027/00 | Rotorcraft ; Rotors peculiar thereto ( alighting gear B64C 25/00 ) |
![]() | B64C 2027/001 | . | { Vibration damping devices } |
B64C 2027/002 | . . | mounted between the rotor drive and the fuselage |
B64C 2027/003 | . . | mounted on rotor hub, e.g. a rotary force generator |
B64C 2027/004 | . . | using actuators, e.g. active systems |
B64C 2027/005 | . . | using suspended masses |
![]() | B64C 2027/04 | . | Helicopters |
![]() | B64C 2027/32 | . | Rotors ( features common to rotors and propellers B64C 11/00 ) |
![]() | B64C 2027/54 | . | Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement |
![]() | B64C 2027/72 | . . | Means acting on blades |
![]() | B64C 2027/7205 | . . . | on each blade individually, e.g. individual blade control (IBC) |
![]() | B64C 2027/7211 | . . . . | without flaps |
B64C 2027/7216 | . . . . . | using one actuator per blade |
B64C 2027/7222 | . . . . . | using airfoil deformation |
B64C 2027/7227 | . . . . . | using blowing slots actuated by piezoelectric actuators |
![]() | B64C 2027/7233 | . . . . . | using higher-harmonic control (HHC) |
B64C 2027/7238 | . . . . . . | by controlling existing swash plate actuators |
B64C 2027/7244 | . . . . . . | by using dedicated actuators |
B64C 2027/725 | . . . . . | using jets controlled by piezoelectric actuators |
B64C 2027/7255 | . . . . . | using one or more swash plates |
![]() | B64C 2027/7261 | . . . . | with flaps |
![]() | B64C 2027/7266 | . . . . . | actuated by actuators |
B64C 2027/7272 | . . . . . . | of the electro-hydraulic type |
B64C 2027/7277 | . . . . . . | of the magnetostrictive type |
B64C 2027/7283 | . . . . . . | of the piezoelectric type |
B64C 2027/7288 | . . . . . . | of the memory shape type |
B64C 2027/7294 | . . . . . | actuated mechanically, e.g. by means of linkages |
![]() | B64C 2027/82 | . | characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting rotor torque or changing direction of rotorcraft |
B64C 2027/8209 | . . | Electrically driven tail rotors |
B64C 2027/8218 | . . | wherein the rotor or the jet axis is inclined with respect to the longitudinal horizontal or vertical plane of the helicopter |
B64C 2027/8227 | . . | comprising more than one rotor |
B64C 2027/8236 | . . | including pusher propellers |
B64C 2027/8245 | . . | using air jets |
B64C 2027/8254 | . . | Shrouded tail rotors, e.g. "Fenestron" fans |
![]() | B64C 2027/8263 | . . | comprising in addition rudders, tails, fins, or the like |
![]() | B64C 2031/00 | Aircraft intended to be sustained without power plant ; Powered hang-glider-type aircraft ; Microlight-type aircraft |
![]() | B64C 2031/06 | . | Kites ( hang-gliders B64C 31/028 ; toy aspects A63H 27/08 ; towed targets F41J { for propelling boats B63H 9/0685 ; for propelling wind driven boards, control means and harnesses therefor B63B 35/7976 } ) |
![]() | B64C 2039/00 | Aircraft not otherwise provided for |
![]() | B64C 2201/00 | Unmanned aerial vehicles ; Equipment therefor |
![]() | B64C 2201/02 | . | characterized by type of aircraft |
B64C 2201/021 | . . | Airplanes, i.e. having wings and tail planes |
B64C 2201/022 | . . | Balloons, blimps or airships |
B64C 2201/024 | . . | Helicopters, or autogiros |
B64C 2201/025 | . . | Ornithopters, i.e. generating lift and propulsion by flapping wings or insect like means |
B64C 2201/027 | . . | Flying platforms |
B64C 2201/028 | . . | of all-wing types |
![]() | B64C 2201/04 | . | characterised by type of power plant |
B64C 2201/042 | . . | by electric motors ; Electric power sources therefor, e.g. fuel cells, solar panels or batteries |
B64C 2201/044 | . . | by internal combustion engines, e.g. oscillating piston or rotary piston engines |
B64C 2201/046 | . . | by rocket engines, ramjets, or pulse-reactors |
B64C 2201/048 | . . | by jet turbines, or turbofans |
![]() | B64C 2201/06 | . | characterised by in-flight supply of energy |
![]() | B64C 2201/08 | . | characterised by the launching method |
B64C 2201/082 | . . | Released from other aircraft |
B64C 2201/084 | . . | using catapults |
B64C 2201/086 | . . | by taking-off horizontally by own power, e.g. from a runway |
B64C 2201/088 | . . | Vertical take-off using special means ( for helicopters B64C 2201/024 ; for balloons B64C 2201/022 ) |
![]() | B64C 2201/10 | . | characterised by the lift producing means |
B64C 2201/101 | . . | Lifting aerostatically, e.g. using lighter-than-air gases in chambers |
B64C 2201/102 | . . | Deployable wings, e.g. foldable or morphing wings |
B64C 2201/104 | . . | Fixed wings |
B64C 2201/105 | . . | Inflatable wings |
B64C 2201/107 | . . | Parachutes ; Parasails ; Kites ; Membranes |
B64C 2201/108 | . . | using rotors, or propellers |
![]() | B64C 2201/12 | . | adapted for particular use |
B64C 2201/121 | . . | for dropping bombs ; for electronic warfare ; Flying bombs |
B64C 2201/122 | . . | as communication relays, e.g. high altitude platforms |
B64C 2201/123 | . . | for imaging, or topography |
B64C 2201/125 | . . | for meteorology |
B64C 2201/126 | . . | adapted for performing different kinds of missions, e.g. multipurpose use |
B64C 2201/127 | . . | for photography, or video recording, e.g. by using cameras |
B64C 2201/128 | . . | for transporting goods other than bombs |
![]() | B64C 2201/14 | . | characterised by flight control |
![]() | B64C 2201/141 | . . | autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems (INS) |
B64C 2201/143 | . . . | adapted for flying in formations |
B64C 2201/145 | . . . | using satellite radio beacon positioning systems, e.g. GPS |
![]() | B64C 2201/146 | . . | Remote controls |
![]() | B64C 2201/16 | . | characterised by type of propulsion unit |
B64C 2201/162 | . . | using ducted fans or propellers |
B64C 2201/165 | . . | using unducted propellers |
B64C 2201/167 | . . | using rockets, ramjets, pulse jets, plasma, or the like |
![]() | B64C 2201/18 | . | characterised by landing method |
B64C 2201/182 | . . | by being caught in mid-air, or next to the ground, e.g. using a net |
B64C 2201/185 | . . | by deploying parachutes, or the like |
B64C 2201/187 | . . | by landing horizontally, e.g. on a runway |
![]() | B64C 2201/20 | . | Methods for transport, or storage of unmanned aerial vehicles |
B64C 2201/201 | . . | in containers |
B64C 2201/203 | . . | in rucksacks, or bags to be carried by persons |
B64C 2201/205 | . . | by waterborne vehicles, e.g. ships or submarines or by hovercraft |
B64C 2201/206 | . . | by airborne vehicles, e.g. airplanes or helicopters |
B64C 2201/208 | . . | by landborne vehicles, e.g. trucks, lorries, tanks or cars |
B64C 2201/22 | . | having stealth characteristics |
![]() | B64C 2230/00 | Boundary layer controls |
B64C 2230/02 | . | by using acoustic waves generated by transducers |
B64C 2230/04 | . | by actively generating fluid flow |
B64C 2230/06 | . | by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure |
B64C 2230/08 | . | by influencing fluid flow by means of surface cavities, i.e. net fluid flow is null |
B64C 2230/10 | . | by influencing fluid flow by heating using other means than combustion |
B64C 2230/12 | . | by using electromagnetic tiles, fluid ionizers, static charges or plasma |
B64C 2230/14 | . | achieving noise reductions |
B64C 2230/16 | . | by blowing other fluids over the surface than air, e.g. He, H, O2 or exhaust gases |
B64C 2230/18 | . | by using small jets that make the fluid flow oscillate |
B64C 2230/20 | . | by passively inducing fluid flow, e.g. by means of a pressure difference between both ends of a slot or duct |
B64C 2230/22 | . | by using a surface having multiple apertures of relatively small openings other than slots |
B64C 2230/24 | . | by using passive resonance cavities, e.g. without transducers |
B64C 2230/26 | . | by using rib lets or hydrophobic surfaces |
B64C 2230/28 | . | at propeller or rotor blades |
![]() | B64C 2700/00 | Codes corresponding to the former IdT classification |
![]() | B64C 2700/62 | . | Codes corresponding to the former IdT classification of class 62 |
![]() | B64C 2700/6201 | . . | Airplanes, helicopters, autogyros |
![]() | B64C 2700/6202 | . . . | Characteristics not limited to an aircraft type |
B64C 2700/6204 | . . . . | Materials |
B64C 2700/6205 | . . . . | Protection means, e.g. against rust, water, fire |
![]() | B64C 2700/6207 | . . . . | Stabilisation |
![]() | B64C 2700/6208 | . . . . . | Longitudinal and transversal stability |
![]() | B64C 2700/6209 | . . . . . . | automatically controlled |
B64C 2700/6211 | . . . . . . . | with movable weight not acting as pendulum |
![]() | B64C 2700/6212 | . . . . . . . | with weight acting as pendulum |
B64C 2700/6214 | . . . . . . . . | with parts of the aircraft acting as pendulum |
B64C 2700/6215 | . . . . . . . . | with fluid acting as pendulum |
B64C 2700/6216 | . . . . . . . | by gyroscopical effect ( also in combination with pendulum ) |
![]() | B64C 2700/6218 | . . . . . . . | by other pulse power source, e.g. aerodynamical effect, propellers |
![]() | B64C 2700/6221 | . . . . . . | manually controlled |
B64C 2700/6222 | . . . . . . . | with movable weight not acting as pendulum |
B64C 2700/6223 | . . . . . . . | with weight acting as pendulum |
B64C 2700/6225 | . . . . . . . | by gyroscopical effet ( also in combination with pendulum ) |
![]() | B64C 2700/6226 | . . . . . . . | by other pulse power source ; e.g. aerodymamical effet, popeller |
B64C 2700/6229 | . . . . . . | Special devices to stabilise or to compensate a helicoper rotor by other means than counter rotating rotor |
B64C 2700/623 | . . . . . . | Special devices to stabilise or to compensate a gyroplane pivoting torque |
![]() | B64C 2700/6232 | . . . | Airplanes with fixed or movable wings |
![]() | B64C 2700/6233 | . . . . | Design, structure or mounting of wings |
B64C 2700/6235 | . . . . . | Guy-wires assemblies ; Connections between wings and fuselage |
B64C 2700/6236 | . . . . . | Honeycomb stiffeners |
B64C 2700/6238 | . . . . . | Pressure equalising devices between the inside of the wing and the atmosphere |
B64C 2700/6239 | . . . . . | Ful wing structures |
![]() | B64C 2700/624 | . . . . . | Wings or parts thereof movable during flight |
![]() | B64C 2700/6243 | . . . . | Control systems |
B64C 2700/6245 | . . . . . | by warping of wings tips |
B64C 2700/6246 | . . . . . | by auxiliary surfaces at the wings tips |
B64C 2700/6247 | . . . . . | by auxiliary surfaces outside the wings tips |
B64C 2700/6249 | . . . . . | by propellers |
B64C 2700/625 | . . . . . | by jet flaps |
![]() | B64C 2700/6252 | . . . . . | Control systems assemblies |
![]() | B64C 2700/6254 | . . . . . | Control systems or transmitting systems for actuating control surfaces |
![]() | B64C 2700/6256 | . . . . . . | Control devices for fins or rudders |
![]() | B64C 2700/6259 | . . . . . . | Control devices for feed-back compensating and guiding surfaces |
![]() | B64C 2700/6261 | . . . . . . | Transmission systems |
B64C 2700/6264 | . . . . . . | Vibrations suppressing devices |
B64C 2700/6266 | . . . . . . | Safety devices |
B64C 2700/6267 | . . . . . | Control devices for a special position of the flying aircraft or a special position of the pilot |
B64C 2700/6269 | . . . . . | Control from outside the aircraft |
![]() | B64C 2700/627 | . . . . | Influencing airflow over aircraft surfaces |
![]() | B64C 2700/6276 | . . . | Rotorcraft |
![]() | B64C 2700/6277 | . . . . | with driven or windmilling propellers |
![]() | B64C 2700/6278 | . . . . . | Features common for any type of rotorcraft |
![]() | B64C 2700/6281 | . . . . . | Helicopters |
![]() | B64C 2700/6283 | . . . . . . | Rotor construction |
![]() | B64C 2700/6284 | . . . . . . . | Blades control devices |
![]() | B64C 2700/6287 | . . . . . . . | Rotor drives |
B64C 2700/629 | . . . . . . . | Rotors which can be used as propulsion means |
B64C 2700/6291 | . . . . . . . | Rotors stowable in the wings |
B64C 2700/6292 | . . . . . . | Control means using other devices than the rotor |
B64C 2700/6294 | . . . . . . | Construction parts, e.g. frames ; Balancing ; Flight control ; Brakes |
![]() | B64C 2700/6295 | . . . | Aircraft specially adapted for special uses |
B64C 2700/6298 | . . . | Gliders |