CN2175183Y - Remote control air-ship - Google Patents
Remote control air-ship Download PDFInfo
- Publication number
- CN2175183Y CN2175183Y CN 93224337 CN93224337U CN2175183Y CN 2175183 Y CN2175183 Y CN 2175183Y CN 93224337 CN93224337 CN 93224337 CN 93224337 U CN93224337 U CN 93224337U CN 2175183 Y CN2175183 Y CN 2175183Y
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- Prior art keywords
- utility
- cabin
- model
- remote control
- driving engine
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- Expired - Fee Related
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Abstract
The utility model belongs to an aircraft, particularly a remote control airship used for aerial surveillance and signal transmission. The utility model adopts the technical proposal that the covering inner surface of the ship body is provided with a supporting frame, a hanging cabin on the lower surface of the ship body is provided with a controller receiver and a corresponding actuating mechanism, both ends of a supporting rod penetrating and connecting to the side wall of the hanging cabin are provided and connected with engines, a transmitter of the controller is arranged on the ground, etc. The utility model has the advantages of good flight stability in the sky, easy manipulation, small integral volume, etc. Moreover, the utility model can be additionally provided with devices such as monitoring devices, signal forwarding devices, etc., according to the requirements of trades. Therefore, the utility model has wide application.
Description
The utility model belongs to aircraft, is meant a kind of remote control airship that is used for aerial monitoring and signal transmission especially.
Existing simple and easy aircraft is (as dirigible at present, fire balloon etc.) be keystone configuration mostly in hull or fire balloon, to fill hydrogen, helium or hot air, and hanging of hull or fire balloon bottom driving engine is set in the cabin or turn to, accessory equipment such as jacking system uses to reach manned, loading flight or sports, it is big that the simple and easy aircraft of employing said structure exists the aircraft own vol, poor stability in the flight course (generally can only smooth flight under three grades of natural wind conditions), the comparatively single technical deficiency that waits of purposes.
The purpose of this utility model is to provide a kind of remote control airship, employing is installed support frame additional at ship shell inside face, assemble driving engine in the cabin hanging of hull lower surface, remote controller receiver and corresponding actuating unit and transmission component, and in technical measures such as ground configuration remote controller emitters, and can in hanging the cabin, install accessory equipments such as monitoring, signal forwarding additional according to the industry needs to reach the purpose that overcomes the prior art deficiency.
Integral structure of the present utility model is: a kind of remote control airship comprises hull, hangs the cabin, is arranged at driving engine, remote controller receiver and corresponding actuating unit in the cabin and the emitter that is arranged in ground-surface remote controller; Hull is made up of the arc rod member 2 that is anchored on the effective quantity on the bar shaped connecting rod 1 support frame of forming and the flexible ship shell 3 that the shop is overlying on the support frame outside face, hang cabin 4 and be anchored on the hull lower surface, be connected to strut bar 5 both ends of hanging the cabin sidewall and be symmetrically arranged with driving engine 6, the gear 7 that fastens as one with strut bar middle part cooperates with gear 8 on the actuating unit 16 by the transmission component of routine, each mouth of actuating unit 18 respectively with rudder face, gear 8, and other accessory equipment connects.
Specific structural features of the present utility model has: driving engine is the duct driving engine, hull length 5-10 rice, and charge air is 18-58m
3, active respectively yaw rudder 11 and the elevating rudder 12 of being connected with of vertical tail 9 and tailplane 10 ends, it is fastening to adopt bracing cable 13 to connect between vertical tail and the tailplane.
Accessory structure of the present utility model has:
Hang bilge portion and be fastened with alighting gear 14.
Accompanying drawing of the present utility model has:
Fig. 1 is an integral structure sketch of the present utility model.
Fig. 2 is a right elevation of the present utility model.
The connection diagram of Fig. 3 actuating unit and rudder face.
Fig. 4 is actuating unit and driving engine connection diagram.
Accompanying drawing has provided embodiment of the present utility model, in conjunction with the accompanying drawings embodiment of the present utility model is described in further detail:
Fig. 1 is the structure diagram of present embodiment, integral structure as described above, on two bar shaped connecting rods 1, be fastened with ten curved rods 2 and constitute support frame with screw, above-mentioned binding rod member is that main material is made with the alloy aluminum, it is fastening with bar shaped connecting rod 1 usefulness screw respectively to hang the both sides, cabin, ship shell outside face is that primary raw material is made with Buddhist nun's tower silk fabric electrostatic prevention aluminizer, and it is that main material is made that internal layer adopts the polyethylene or the polyvinylchloride that are coated with complex film.Driving engine is an electrothermic type 10-18CC engine model, fuel oil is methyl alcohol and castor oil, mixture ratio is 9:1 or 5:1, maximum power is 3 horsepowers, be anchored on gear 8 engagements of gear 7 by assembling on reducing gear 15 and the actuating unit at strut bar middle part, and the sheave surface of reducing gear 15 is provided with tension spring 21, remote controller and actuating unit are selected special-purpose model plane telecommand equipment for use, produce the Futaba telecommand equipment as Japan, skid formula alighting gear is with to hang bilge portion fastening be an integral body, and connecting rod and actuating unit rocking arm 9 are connected with living in selling with the fastening rocking arm 20 of rudder face lower surface.8.2 meters of hull total lengths, the widest part diameter 2m, filling gas in the ship is helium, the dirigible monnolithic case is long water droplet shape.
The utility model is work like this:
When airship flight aloft the time, can stir the master cock on the emitter, the electric signal that receiver can transmit emitter is transformed into mechanical action, thereby control yaw rudder, the deflection of elevating rudder and the rotation of gear 8, with turning to of control driving engine, thereby finish climbing of dirigible, hovering, flare maneuvers such as vertical takeoff and landing.
Technological progress and substantive distinguishing features that the utility model is obtained are:
1, overall volume is little, and good stability in the flight course (generally can resist the level Four natural wind) is easily handled, and flying speed is adjustable.
2, the user can assemble other auxiliary equipment according to the needs of different industries in hanging the cabin, such as monitoring, sniffer, can be used for geological prospecting, meteorological remote sensing, and the industries such as rain making and signal forwarding, of many uses.
Claims (3)
1, a kind of remote control airship comprises hull, hangs the cabin, is arranged at driving engine, remote controller receiver and corresponding actuating unit in the cabin and the emitter that is arranged in ground-surface remote controller; It is characterized in that the flexible ship shell 3 that support frame that hull is made up of the arc rod member 2 that is anchored on the effective quantity on the bar shaped connecting rod 1 and shop are overlying on the support frame outside face forms, hang cabin 4 and be anchored on the hull lower surface, be connected to strut bar 5 both ends of hanging the cabin sidewall and be symmetrically arranged with driving engine 6, the gear 7 that fastens as one with strut bar middle part cooperates with gear 8 on the actuating unit 16 by the transmission component of routine, each mouth of actuating unit 18 respectively with rudder face, gear 8, and other accessory equipment connects.
2, a kind of remote control airship according to claim 1 is characterized in that driving engine is the duct driving engine, hull length 5-10 rice, and charge air is 18-58m
3, active respectively yaw rudder 11 and the elevating rudder 12 of being connected with of vertical tail 9 and tailplane 10 ends, it is fastening to adopt bracing cable 13 to connect between vertical tail and the tailplane.
3, a kind of remote control airship according to claim 1 and 2 is characterized in that hanging bilge portion and is fastened with alighting gear 14.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 93224337 CN2175183Y (en) | 1993-09-09 | 1993-09-09 | Remote control air-ship |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 93224337 CN2175183Y (en) | 1993-09-09 | 1993-09-09 | Remote control air-ship |
Publications (1)
Publication Number | Publication Date |
---|---|
CN2175183Y true CN2175183Y (en) | 1994-08-24 |
Family
ID=33802399
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 93224337 Expired - Fee Related CN2175183Y (en) | 1993-09-09 | 1993-09-09 | Remote control air-ship |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN2175183Y (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111846191A (en) * | 2020-07-27 | 2020-10-30 | 重庆交通大学 | Combined power airship |
-
1993
- 1993-09-09 CN CN 93224337 patent/CN2175183Y/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111846191A (en) * | 2020-07-27 | 2020-10-30 | 重庆交通大学 | Combined power airship |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C19 | Lapse of patent right due to non-payment of the annual fee | ||
CF01 | Termination of patent right due to non-payment of annual fee |