B64C 1/00
|
FuselagesConstructional features common to fuselages, wings, stabilising surfaces or the like |
B64C 1/06
|
FramesStringersLongerons |
B64C 1/08
|
Geodetic or other open-frame structures |
B64C 1/10
|
Bulkheads |
B64C 1/12
|
Construction or attachment of skin panels |
B64C 1/14
|
WindowsDoorsHatch covers or access panelsSurrounding frame structuresCanopiesWindscreens |
B64C 1/16
|
FuselagesConstructional features common to fuselages, wings, stabilising surfaces or the like specially adapted for mounting power plant |
B64C 1/18
|
Floors |
B64C 1/20
|
Floors specially adapted for freight |
B64C 1/22
|
Other structures integral with fuselages to facilitate loading |
B64C 1/24
|
Steps mounted on, and retractable within, fuselages |
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 dimensions of aircraft |
B64C 1/32
|
Severable or jettisonable parts of fuselage facilitating emergency escape |
B64C 1/34
|
FuselagesConstructional features common to fuselages, wings, stabilising surfaces or the like comprising inflatable structural components |
B64C 1/36
|
FuselagesConstructional features common to fuselages, wings, stabilising surfaces or the like adapted to receive antennas or radomes |
B64C 1/38
|
Constructions adapted to reduce effects of aerodynamic or other external heating |
B64C 1/40
|
Sound or heat insulation |
B64C 3/00
|
Wings |
B64C 3/10
|
Shape of wings |
B64C 3/14
|
Aerofoil profile |
B64C 3/16
|
Frontal aspect |
B64C 3/18
|
SparsRibsStringers |
B64C 3/20
|
Integral or sandwich constructions |
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
|
Wings comprising inflatable structural components |
B64C 3/32
|
Wings specially adapted for mounting power plant |
B64C 3/34
|
Tanks constructed integrally with wings, e.g. for fuel or water |
B64C 3/36
|
Structures adapted to reduce effects of aerodynamic or other external heating |
B64C 3/38
|
Adjustment of complete wings or parts thereof |
B64C 3/40
|
Varying angle of sweep |
B64C 3/42
|
Adjusting about chordwise axes |
B64C 3/44
|
Varying camber |
B64C 3/46
|
Varying camber by inflatable elements |
B64C 3/48
|
Varying camber by relatively-movable parts of wing structures |
B64C 3/50
|
Varying camber by leading or trailing edge flaps |
B64C 3/52
|
Warping |
B64C 3/54
|
Varying in area |
B64C 3/56
|
Folding or collapsing to reduce overall dimensions of aircraft |
B64C 3/58
|
Wings provided with fences or spoilers |
B64C 5/00
|
Stabilising surfaces |
B64C 5/02
|
Tailplanes |
B64C 5/04
|
Noseplanes |
B64C 5/06
|
Fins |
B64C 5/08
|
Stabilising surfaces mounted on, or supported by, wings |
B64C 5/10
|
Stabilising surfaces adjustable |
B64C 5/12
|
Stabilising surfaces adjustable for retraction against or within fuselage or nacelle |
B64C 5/14
|
Varying angle of sweep |
B64C 5/16
|
Stabilising surfaces adjustable about spanwise axes |
B64C 5/18
|
Stabilising surfaces adjustable in area |
B64C 7/00
|
Structures or fairings not otherwise provided for |
B64C 7/02
|
Nacelles |
B64C 9/00
|
Adjustable control surfaces or members, e.g. rudders |
B64C 9/02
|
Mounting or supporting thereof |
B64C 9/04
|
Adjustable control surfaces or members, e.g. rudders with compound dependent movements |
B64C 9/06
|
Adjustable control surfaces or members, e.g. rudders with two or more independent movements |
B64C 9/08
|
Adjustable control surfaces or members, e.g. rudders bodily displaceable |
B64C 9/10
|
Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs |
B64C 9/12
|
Adjustable control surfaces or members, e.g. rudders surfaces of different type or function being simultaneously adjusted |
B64C 9/14
|
Adjustable control surfaces or members, e.g. rudders forming slots |
B64C 9/16
|
Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing |
B64C 9/18
|
Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by single flaps |
B64C 9/20
|
Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing by multiple flaps |
B64C 9/22
|
Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing |
B64C 9/24
|
Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap |
B64C 9/26
|
Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by multiple flaps |
B64C 9/28
|
Adjustable control surfaces or members, e.g. rudders forming slots by flaps at both the front and rear of the wing operating in unison |
B64C 9/30
|
Balancing hinged surfaces, e.g. dynamically |
B64C 9/32
|
Air braking surfaces |
B64C 9/34
|
Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members |
B64C 9/36
|
Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members the members being fuselages or nacelles |
B64C 9/38
|
Jet flaps |
B64C 11/00
|
Propellers, e.g. of ducted typeFeatures common to propellers and rotors for rotorcraft |
B64C 11/02
|
Hub construction |
B64C 11/04
|
Blade mountings |
B64C 11/06
|
Blade mountings for variable-pitch blades |
B64C 11/08
|
Blade mountings for non-adjustable blades |
B64C 11/10
|
Blade mountings for non-adjustable blades rigid |
B64C 11/12
|
Blade mountings for non-adjustable blades flexible |
B64C 11/14
|
Spinners |
B64C 11/16
|
Blades |
B64C 11/18
|
Aerodynamic features |
B64C 11/20
|
Constructional features |
B64C 11/22
|
Solid blades |
B64C 11/24
|
Hollow blades |
B64C 11/26
|
Fabricated blades |
B64C 11/28
|
Collapsible or foldable blades |
B64C 11/30
|
Blade pitch-changing mechanisms |
B64C 11/32
|
Blade pitch-changing mechanisms mechanical |
B64C 11/34
|
Blade pitch-changing mechanisms mechanical automatic |
B64C 11/36
|
Blade pitch-changing mechanisms mechanical non-automatic |
B64C 11/38
|
Blade pitch-changing mechanisms fluid, e.g. hydraulic |
B64C 11/40
|
Blade pitch-changing mechanisms fluid, e.g. hydraulic automatic |
B64C 11/42
|
Blade pitch-changing mechanisms fluid, e.g. hydraulic non-automatic |
B64C 11/44
|
Blade pitch-changing mechanisms electric |
B64C 11/46
|
Arrangements of, or constructional features peculiar to, multiple propellers |
B64C 11/48
|
Units of two or more coaxial propellers |
B64C 11/50
|
Phase synchronisation between multiple propellers |
B64C 13/00
|
Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers |
B64C 13/02
|
Initiating means |
B64C 13/04
|
Initiating means actuated personally |
B64C 13/06
|
Initiating means actuated personally adjustable to suit individual persons |
B64C 13/08
|
Trimming zero positions |
B64C 13/10
|
Initiating means actuated personally comprising warning devices |
B64C 13/12
|
Dual control apparatus |
B64C 13/14
|
Initiating means actuated personally lockable |
B64C 13/16
|
Initiating means actuated automatically, e.g. responsive to gust detectors |
B64C 13/18
|
Initiating means actuated automatically, e.g. responsive to gust detectors using automatic pilot |
B64C 13/20
|
Initiating means actuated automatically, e.g. responsive to gust detectors using radiated signals |
B64C 13/22
|
Initiating means actuated automatically, e.g. responsive to gust detectors readily revertible to personal control |
B64C 13/24
|
Transmitting means |
B64C 13/26
|
Transmitting means without power amplification or where power amplification is irrelevant |
B64C 13/28
|
Transmitting means without power amplification or where power amplification is irrelevant mechanical |
B64C 13/30
|
Transmitting means without power amplification or where power amplification is irrelevant mechanical using cable, chain, or rod mechanisms |
B64C 13/32
|
Transmitting means without power amplification or where power amplification is irrelevant mechanical using cam mechanisms |
B64C 13/34
|
Transmitting means without power amplification or where power amplification is irrelevant mechanical using toothed gearing |
B64C 13/36
|
Transmitting means without power amplification or where power amplification is irrelevant fluid |
B64C 13/38
|
Transmitting means with power amplification |
B64C 13/40
|
Transmitting means with power amplification using fluid pressure |
B64C 13/42
|
Transmitting means with power amplification using fluid pressure having duplication or stand-by provisions |
B64C 13/44
|
Transmitting means with power amplification using fluid pressure overriding of personal controlsTransmitting means with power amplification using fluid pressure with automatic return to inoperative position |
B64C 13/46
|
Transmitting means with power amplification using fluid pressure with artificial feel |
B64C 13/48
|
Transmitting means with power amplification using fluid pressure characterised by the fluid being gaseous |
B64C 13/50
|
Transmitting means with power amplification using electrical energy |
B64C 15/00
|
Attitude, flight direction or altitude control by jet reaction |
B64C 15/02
|
Attitude, flight direction or altitude control by jet reaction the jets being propulsion jets |
B64C 15/12
|
Attitude, flight direction or altitude control by jet reaction the jets being propulsion jets the power plant being tiltable |
B64C 15/14
|
Attitude, flight direction or altitude control by jet reaction the jets being other than main propulsion jets |
B64C 17/00
|
Aircraft stabilisation not otherwise provided for |
B64C 17/02
|
Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus |
B64C 17/04
|
Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus by pendular bodies |
B64C 17/06
|
Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus by gyroscopic apparatus |
B64C 17/08
|
Aircraft stabilisation not otherwise provided for by ballast supply or discharge |
B64C 17/10
|
Transferring fuel to adjust trim |
B64C 19/00
|
Aircraft control not otherwise provided for |
B64C 19/02
|
Conjoint controls |
B64C 21/00
|
Influencing air flow over aircraft surfaces by affecting boundary layer flow |
B64C 21/01
|
Boundary layer ingestion [BLI] propulsion |
B64C 21/02
|
Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like |
B64C 21/04
|
Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing |
B64C 21/06
|
Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for sucking |
B64C 21/08
|
Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like adjustable |
B64C 21/10
|
Influencing air flow over aircraft surfaces by affecting boundary layer flow using other surface properties, e.g. roughness |
B64C 23/00
|
Influencing air flow over aircraft surfaces, not otherwise provided for |
B64C 23/02
|
Influencing air flow over aircraft surfaces, not otherwise provided for by means of rotating members of cylindrical or similar form |
B64C 23/04
|
Influencing air flow over aircraft surfaces, not otherwise provided for by generating shock waves |
B64C 23/06
|
Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices |
B64C 23/08
|
Influencing air flow over aircraft surfaces, not otherwise provided for using Magnus effect |
B64C 25/00
|
Alighting gear |
B64C 25/02
|
Undercarriages |
B64C 25/04
|
Arrangement or disposition on aircraft |
B64C 25/06
|
Undercarriages fixed |
B64C 25/08
|
Undercarriages non-fixed, e.g. jettisonable |
B64C 25/10
|
Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like |
B64C 25/12
|
Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways |
B64C 25/14
|
Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like fore-and-aft |
B64C 25/16
|
Fairings movable in conjunction with undercarriage elements |
B64C 25/18
|
Operating mechanisms |
B64C 25/20
|
Operating mechanisms mechanical |
B64C 25/22
|
Operating mechanisms fluid |
B64C 25/24
|
Operating mechanisms electric |
B64C 25/26
|
Control or locking systems therefor |
B64C 25/28
|
Control or locking systems therefor with indicating or warning devices |
B64C 25/30
|
Control or locking systems therefor emergency actuated |
B64C 25/32
|
Alighting gear characterised by elements which contact the ground or similar surface |
B64C 25/34
|
Alighting gear characterised by elements which contact the ground or similar surface wheeled type, e.g. multi-wheeled bogies |
B64C 25/36
|
Arrangements or adaptations of wheels, tyres or axles in general |
B64C 25/38
|
Alighting gear characterised by elements which contact the ground or similar surface endless-track type |
B64C 25/40
|
Alighting gear characterised by elements which contact the ground or similar surface the elements being rotated before touch-down |
B64C 25/42
|
Arrangement or adaptation of brakes |
B64C 25/44
|
Actuating mechanisms |
B64C 25/46
|
Brake regulators for preventing skidding or aircraft somersaulting |
B64C 25/48
|
Actuating mechanisms differentially operated for steering purposes |
B64C 25/50
|
Steerable undercarriagesShimmy-damping |
B64C 25/52
|
Skis or runners |
B64C 25/54
|
Floats |
B64C 25/56
|
Floats inflatable |
B64C 25/58
|
Arrangements or adaptations of shock-absorbers or springs |
B64C 25/60
|
Oleo legs |
B64C 25/62
|
Spring shock-absorbersSprings |
B64C 25/64
|
Spring shock-absorbersSprings using rubber or like elements |
B64C 25/66
|
Convertible alighting gearCombinations of different kinds of ground or like engaging elements |
B64C 25/68
|
Arrester hooks |
B64C 27/00
|
RotorcraftRotors peculiar thereto |
B64C 27/02
|
Gyroplanes |
B64C 27/04
|
Helicopters |
B64C 27/06
|
Helicopters with single rotor |
B64C 27/08
|
Helicopters with two or more rotors |
B64C 27/10
|
Helicopters with two or more rotors arranged coaxially |
B64C 27/12
|
Rotor drives |
B64C 27/14
|
Direct drive between power plant and rotor hub |
B64C 27/16
|
Drive of rotors by means, e.g. propellers, mounted on rotor blades |
B64C 27/18
|
Drive of rotors by means, e.g. propellers, mounted on rotor blades the means being jet-reaction apparatus |
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
|
Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with rotor blades fixed in flight to act as lifting surfaces |
B64C 27/26
|
Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings |
B64C 27/28
|
Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with forward-propulsion propellers pivotable to act as lifting rotors |
B64C 27/30
|
Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft with provision for reducing drag of inoperative rotor |
B64C 27/32
|
Rotors |
B64C 27/33
|
Rotors having flexing arms |
B64C 27/35
|
Rotors having elastomeric joints |
B64C 27/37
|
Rotors having articulated joints |
B64C 27/39
|
Rotors having articulated joints with individually articulated blades, i.e. with flapping or drag hinges |
B64C 27/41
|
Rotors having articulated joints with flapping hinge or universal joint, common to the blades |
B64C 27/43
|
Rotors having articulated joints with flapping hinge or universal joint, common to the blades see-saw type, i.e. two-bladed rotor |
B64C 27/45
|
Rotors having articulated joints with a feathering hinge only |
B64C 27/46
|
Blades |
B64C 27/48
|
Root attachment to rotor head |
B64C 27/50
|
Blades foldable to facilitate stowage of aircraft |
B64C 27/51
|
Damping of blade movements |
B64C 27/52
|
Tilting of rotor bodily relative to fuselage |
B64C 27/54
|
Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement |
B64C 27/56
|
Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated |
B64C 27/57
|
Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement characterised by the control initiating means, e.g. manually actuated automatic or condition responsive, e.g. responsive to rotor speed, torque or thrust |
B64C 27/58
|
Transmitting means, e.g. interrelated with initiating means or means acting on blades |
B64C 27/59
|
Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical |
B64C 27/64
|
Transmitting means, e.g. interrelated with initiating means or means acting on blades using fluid pressure, e.g. having fluid power amplification |
B64C 27/68
|
Transmitting means, e.g. interrelated with initiating means or means acting on blades using electrical energy, e.g. having electrical power amplification |
B64C 27/72
|
Means acting on blades |
B64C 27/78
|
Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement in association with pitch adjustment of blades of anti-torque rotor |
B64C 27/80
|
Mechanisms for controlling blade adjustment or movement relative to rotor head, e.g. lag-lead movement for differential adjustment of blade pitch between two or more lifting rotors |
B64C 27/82
|
RotorcraftRotors peculiar thereto characterised by the provision of an auxiliary rotor or fluid-jet device for counter-balancing lifting-rotor torque or changing direction of rotorcraft |
B64C 27/467
|
Aerodynamic features |
B64C 27/473
|
Constructional features |
B64C 27/605
|
Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including swash plate, spider or cam mechanisms |
B64C 27/615
|
Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including flaps mounted on blades |
B64C 27/625
|
Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical including rotating masses or servo rotors |
B64C 27/635
|
Transmitting means, e.g. interrelated with initiating means or means acting on blades mechanical specially for controlling lag-lead movements of blades |
B64C 29/00
|
Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft |
B64C 29/02
|
Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded |
B64C 29/04
|
Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis vertical when grounded characterised by jet-reaction propulsion |
B64C 30/00
|
Supersonic type aircraft |
B64C 31/00
|
Aircraft intended to be sustained without power plantPowered hang-glider-type aircraftMicrolight-type aircraft |
B64C 31/02
|
Gliders, e.g. sailplanes |
B64C 31/04
|
Man-powered aircraft |
B64C 31/06
|
Kites |
B64C 31/024
|
Gliders, e.g. sailplanes with auxiliary power plant |
B64C 31/028
|
Hang-glider-type aircraftMicrolight-type aircraft |
B64C 31/032
|
Hang-glider-type aircraftMicrolight-type aircraft having delta shaped wing |
B64C 31/036
|
Hang-glider-type aircraftMicrolight-type aircraft having parachute-type wing |
B64C 33/00
|
Ornithopters |
B64C 33/02
|
WingsActuating mechanisms therefor |
B64C 35/00
|
Flying-boatsSeaplanes |
B64C 35/02
|
Flying-boat hulls |
B64C 37/00
|
Convertible aircraft |
B64C 37/02
|
Flying units formed by separate aircraft |
B64C 39/00
|
Aircraft not otherwise provided for |
B64C 39/02
|
Aircraft not otherwise provided for characterised by special use |
B64C 39/04
|
Aircraft not otherwise provided for having multiple fuselages or tail booms |
B64C 39/06
|
Aircraft not otherwise provided for having disc- or ring-shaped wings |
B64C 39/08
|
Aircraft not otherwise provided for having multiple wings |
B64C 39/10
|
All-wing aircraft |
B64C 39/12
|
Canard-type aircraft |
B64C 99/00
|
Subject matter not provided for in other groups of this subclass |