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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 |
1/ | 00 | Dropping, ejecting, releasing, or receiving articles, liquids, or the like, in flight (with respect to weapon sights, F 41 G takes precedence; parachutes B 64 D 17/00; ejectable seats B 64 D 25/10; ejectable capsules B 64 D 25/12; refuelling during flight B 64 D 39/00; launching apparatus for projecting projectiles or missiles F 41 F 1/00, F 41 F 7/00; rocket or torpedo launchers F 41 F 3/00) |
1/ | 02 | . | Dropping, ejecting, or releasing articles (jettisonable fuel reservoirs B 64 D 37/12) |
1/ | 04 | . | . | the articles being explosive, e.g. bombs (arming or setting bomb fuzes F 42 C) |
1/ | 06 | . | . | . | Bomb releasing; Bomb doors |
1/ | 08 | . | . | the articles being load-carrying devices |
1/ | 10 | . | . | . | Stowage arrangements for the devices in aircraft |
1/ | 12 | . | . | . | Releasing |
1/ | 14 | . | . | . | Absorbing landing shocks |
1/ | 16 | . | Dropping or releasing powdered, liquid or gaseous matter, e.g. for fire-fighting (jettisoning fuel B 64 D 37/26) [5] |
1/ | 18 | . | . | by spraying, e.g. insecticides (spraying apparatus in general B 05 B) |
1/ | 20 | . | . | for sky-writing |
1/ | 22 | . | Taking-up articles from earth's surface |
3/ | 00 | Aircraft adaptations to facilitate towing or being towed (B 64 D 39/00 takes precedence; ground installations for launching or towing aircraft B 64 F; towing ropes per se D 07 B) |
3/ | 02 | . | for towing targets (towed targets per se F 41 J) |
5/ | 00 | Aircraft transported by aircraft, e.g. for release or reberthing during flight (flying units formed by separate aircraft B 64 C 37/02) |
7/ | 00 | Arrangement of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft (dropping bombs or the like B 64 D 1/00; armaments or mountings therefor per se F 41) |
7/ | 02 | . | the armaments being firearms |
7/ | 04 | . | . | fixedly mounted |
7/ | 06 | . | . | movably mounted |
7/ | 08 | . | Arrangement of rocket launchers (rocket launchers per se, e.g. rocket pods, F 41 F 3/06) |
9/ | 00 | Equipment for handling freight; Equipment for facilitating passenger embarkation or the like (emergency equipment B 64 D 17/00, B 64 D 19/00, B 64 D 25/00; structures integral with fuselage to facilitate loading, fuselage floors specially adapted for freight, steps mounted on, and retractable within, aircraft B 64 C; ground installations B 64 F) |
10/ | 00 | Flying suits (helmets in general A 42 B 3/00; breathing helmets A 62 B 18/00) |
11/ | 00 | Passenger or crew accommodation; Flight-deck installations not otherwise provided for |
11/ | 02 | . | Toilet fittings (of general application A 47 K) |
11/ | 04 | . | Galleys |
11/ | 06 | . | Arrangements or adaptations of seats (seat constructions for emergency purposes B 64 D 25/04) |
13/ | 00 | Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space (treatment rooms with artificial climate for medical purposes A 61 G 10/02; respiratory apparatus in general A 62 B; for vehicles in general B 60 H) |
13/ | 02 | . | the air being pressurised |
13/ | 04 | . | . | Automatic control of pressure |
13/ | 06 | . | the air being conditioned (pressurising B 64 D 13/02) |
13/ | 08 | . | . | the air being heated or cooled |
15/ | 00 | De-icing or preventing icing on exterior surfaces of aircraft (motor vehicles specially adapted for carrying de-icing equipment B 60 P) |
15/ | 02 | . | by ducted hot gas or liquid |
15/ | 04 | . | . | Hot gas application |
15/ | 06 | . | . | Liquid application (in general B 05) |
15/ | 08 | . | . | . | exuded from surface |
15/ | 10 | . | . | . | sprayed over surface |
15/ | 12 | . | by electric heating (H 05 B 3/84 takes precedence; electric heating elements in general H 05 B) [5] |
15/ | 14 | . | . | controlled cyclically along length of surface |
15/ | 16 | . | by mechanical means, e.g. pulsating mats or shoes attached to, or built into, surface |
15/ | 18 | . | . | the surface being an aerofoil, rotor, or propeller |
15/ | 20 | . | Means for detecting icing or initiating de-icing |
15/ | 22 | . | . | Automatic initiation by icing detector |
17/ | 00 | Parachutes (non-canopied parachutes B 64 D 19/00) |
17/ | 02 | . | Canopy arrangement or construction |
17/ | 04 | . | . | formed with two or more canopies arranged about a common axis |
17/ | 06 | . | . | formed with two or more canopies arranged in a cluster |
17/ | 08 | . | . | Secondary or shock-absorbing canopies attached to load line |
17/ | 10 | . | . | Ribbon construction or the like |
17/ | 12 | . | . | constructed to provide variable or non-uniform porosity over area of canopy |
17/ | 14 | . | . | with skirt or air-deflecting panels |
17/ | 16 | . | . | . | secured to hem of main canopy |
17/ | 18 | . | . | Vent arrangement or construction |
17/ | 20 | . | . | . | variable in area |
17/ | 22 | . | Load suspension |
17/ | 24 | . | . | Rigging lines |
17/ | 26 | . | . | . | attached to hem of canopy |
17/ | 28 | . | . | . | attached to apex of canopy |
17/ | 30 | . | . | Harnesses [4] |
17/ | 32 | . | . | . | Construction of quick-release box |
17/ | 34 | . | . | adapted to control direction or rate of descent |
17/ | 36 | . | . | incorporating friction devices or frangible connections to reduce shock loading of canopy |
17/ | 38 | . | . | Releasable fastening devices between parachute and load or pack |
17/ | 40 | . | Packs |
17/ | 42 | . | . | rigid |
17/ | 44 | . | . | . | forming part of load |
17/ | 46 | . | . | Closing means |
17/ | 48 | . | . | with separate pack for extractor of auxiliary parachute |
17/ | 50 | . | . | formed with separate compartments for main canopy, rigging lines, or auxiliary parachute |
17/ | 52 | . | . | Opening, e.g. manual |
17/ | 54 | . | . | . | automatic |
17/ | 56 | . | . | . | . | responsive to barometric pressure |
17/ | 58 | . | . | . | . | responsive to time-delay mechanism |
17/ | 60 | . | . | . | . | by static line |
17/ | 62 | . | Deployment |
17/ | 64 | . | . | by extractor parachute |
17/ | 66 | . | . | . | attached to hem of main canopy |
17/ | 68 | . | . | . | attached to apex of main canopy |
17/ | 70 | . | . | by springs |
17/ | 72 | . | . | by explosive or inflatable means (connection of valves to inflatable elastic bodies B 60 C 29/00) |
17/ | 74 | . | . | Sequential deployment of a plurality of canopies |
17/ | 76 | . | . | facilitated by method of folding or packing |
17/ | 78 | . | in association with other load-retarding apparatus |
17/ | 80 | . | in association with aircraft, e.g. for braking thereof |
19/ | 00 | Non-canopied parachutes |
19/ | 02 | . | Rotary-wing parachutes |
| B64D 21/00 - B64D 47/08 |