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| SECTION B PERFORMING OPERATIONS; TRANSPORTING |
| B 64 | AIRCRAFT; AVIATION; COSMONAUTICS |
| B 64 D | EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS |
23/ | 00 | Training of parachutists |
25/ | 00 | Emergency apparatus or devices, not otherwise provided for (parachutes B64D 17/00, B64D 19/00; jettisoning of fuel tanks or fuel B64D 37/00; safety belts or body harnesses in general A62B 35/00; safety belts or body harnesses for land vehicles B60R 22/00; severable or jettisonable parts of fuselage facilitating emergency escape B64C) [4] |
25/ | 02 | . | Supports or holding means for living bodies (for ejector seats B64D 25/115) [5] |
25/ | 04 | . | . | Seat modifications |
25/ | 06 | . | . | Harnessing [4] |
25/ | 08 | . | Ejecting or escaping means (escape apertures B64C) |
25/ | 10 | . | . | Ejector seats |
25/ | 102 | . | . | . | Propelling means, e.g. by a combination of catapult and rocket means (B64D 25/11, B64D 25/112 take precedence) [5] |
25/ | 105 | . | . | . | . | by catapult means only [5] |
25/ | 108 | . | . | . | . | by rocket means only [5] |
25/ | 11 | . | . | . | Controlling attitude or direction of ejector seat or associated mechanism prior to ejection [5] |
25/ | 112 | . | . | . | Controlling attitude or direction of ejector seat after ejection [5] |
25/ | 115 | . | . | . | Occupant restraining, positioning or protecting devices [5] |
25/ | 118 | . | . | . | Separation of occupant from seat after ejection [5] |
25/ | 12 | . | . | Ejectable capsules |
25/ | 14 | . | . | Inflatable escape chutes (connection of valves to inflatable elastic bodies B60C 29/00) |
25/ | 16 | . | . | Dinghy stowage |
25/ | 18 | . | . | Flotation gear (aircraft alighting gear B64C) |
25/ | 20 | . | . | Releasing of crash-position indicators |
27/ | 00 | Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby (attitude, flight- direction, or altitude control of aircraft by jet reaction B64C) |
27/ | 02 | . | Aircraft characterised by the type or position of power plant (fuselages or wings adapted for mounting power plant B64C) |
27/ | 04 | . | . | of piston type |
27/ | 06 | . | . | . | within, or attached to, wing |
27/ | 08 | . | . | . | within, or attached to, fuselage |
27/ | 10 | . | . | of gas-turbine type (B64D 27/16 takes precedence) |
27/ | 12 | . | . | . | within, or attached to, wing |
27/ | 14 | . | . | . | within, or attached to, fuselage |
27/ | 16 | . | . | of jet type |
27/ | 18 | . | . | . | within, or attached to, wing |
27/ | 20 | . | . | . | within, or attached to, fuselage |
27/ | 22 | . | . | using atomic energy |
27/ | 24 | . | . | using steam, electricity, or spring force (B64D 27/16 takes precedence) |
27/ | 26 | . | Aircraft characterised by construction of power-plant mounting |
29/ | 00 | Power-plant nacelles, fairings, or cowlings (nacelles not otherwise provided for B64C) |
29/ | 02 | . | associated with wings (wings adapted for mounting power plant B64C) |
29/ | 04 | . | associated with fuselages |
29/ | 06 | . | Attaching of nacelles, fairings, or cowlings |
29/ | 08 | . | Inspection panels for power plants |
31/ | 00 | Power plant control; Arrangement thereof (flying controls B64C) |
31/ | 02 | . | Initiating means |
31/ | 04 | . | . | actuated personally |
31/ | 06 | . | . | actuated automatically |
31/ | 08 | . | . | . | for keeping cruising speed constant (conjoint control of power plant and propeller B64C) |
31/ | 10 | . | . | . | for preventing asymmetric thrust upon failure of one power plant |
31/ | 12 | . | . | . | for equalising or synchronising power plants |
31/ | 14 | . | Transmitting means between initiating means and power plants |
33/ | 00 | Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for |
33/ | 02 | . | of combustion air intakes (air intakes for gas-turbine plants or jet-propulsion plants per se F02C 7/04; air intakes for combustion engines in general F02M 35/00) |
33/ | 04 | . | of exhaust outlets or jet pipes (exhaust outlets for combustion engines in general F01N; jet pipes or nozzles for jet-propulsion plants per se F02K; plants characterised by the form or arrangement of the jet pipe or nozzle F02K) [3] |
33/ | 08 | . | of power plant cooling systems (cooling of internal-combustion engines per se F01P; cooling of gas-turbine plants or jet-propulsion plants per se F02C, F02K) |
33/ | 10 | . | . | Radiator arrangement |
33/ | 12 | . | . | . | of retractable type |
35/ | 00 | Transmitting power from power plant to propellers or rotors; Arrangements of transmissions (propellers or rotors per se, helicopter transmissions B64C) |
35/ | 02 | . | characterised by the type of power plant |
35/ | 04 | . | characterised by the transmission driving a plurality of propellers or rotors |
35/ | 06 | . | . | the propellers or rotors being counter-rotating |
35/ | 08 | . | characterised by the transmission being driven by a plurality of power plants |
37/ | 00 | Arrangements in connection with fuel supply for power plant (refuelling during flight B64D 39/00) |
37/ | 02 | . | Tanks (tanks constructed integrally with aircraft wings B64C; tanks in general B65D) |
37/ | 04 | . | . | Arrangement thereof in or on aircraft |
37/ | 06 | . | . | Constructional adaptations thereof |
37/ | 08 | . | . | . | Internal partitioning |
37/ | 10 | . | . | . | to facilitate fuel pressurisation |
37/ | 12 | . | . | . | jettisonable |
37/ | 14 | . | . | Filling or emptying (transferring fuels to adjust aircraft trim B64C) |
37/ | 16 | . | . | . | Filling systems (ground installations for fuelling aircraft B64F) |
37/ | 18 | . | . | . | . | Conditioning fuel during filling |
37/ | 20 | . | . | . | Emptying systems |
37/ | 22 | . | . | . | . | facilitating emptying in any position of tank |
37/ | 24 | . | . | . | . | using gas pressure |
37/ | 26 | . | . | . | . | Jettisoning of fuel |
37/ | 28 | . | . | . | . | Control thereof |
37/ | 30 | . | Fuel systems for specific fuels |
37/ | 32 | . | Safety measures not otherwise provided for, e.g. preventing explosive conditions (extinguishing or preventing fires in aircraft A62C) |
37/ | 34 | . | Conditioning fuel, e.g. heating (during filling B64D 37/18) |
39/ | 00 | Refuelling during flight (filling or emptying fuel tanks B64D 37/14) |
39/ | 02 | . | Means for paying-in or out hose |
39/ | 04 | . | Adaptations of hose construction (pipes in general F16L) |
39/ | 06 | . | Connecting hose to aircraft; Disconnecting hose therefrom |
41/ | 00 | Power installations for auxiliary purposes |
43/ | 00 | Arrangements or adaptations of instruments (arrangements of cameras B64D 47/08; aeronautical measuring instruments per se G01C) |
43/ | 02 | . | for indicating aircraft speed or stalling conditions |
45/ | 00 | Aircraft indicators or protectors not otherwise provided for (camouflage F41H 3/00) |
45/ | 02 | . | Lightning protectors (lightning arrestors H01C 7/12, H01C 8/04, H01G 9/18, H01T; circuit arrangements therefor H02H); Static dischargers (in general H05F 3/00) |
45/ | 04 | . | Landing aids; Safety measures to prevent collision with earth's surface |
45/ | 06 | . | . | mechanical |
45/ | 08 | . | . | optical |
47/ | 00 | Equipment not otherwise provided for |
47/ | 02 | . | Arrangements or adaptations of signal or lighting devices |
47/ | 04 | . | . | the lighting devices being primarily intended to illuminate the way ahead |
47/ | 06 | . | . | for indicating aircraft presence |
47/ | 08 | . | Arrangements of cameras |
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