CN204737021U

CN204737021U - Solar energy dirigible of double dynamical dual fail -safe

Info

Publication number: CN204737021U
Application number: CN201520391961.XU
Authority: CN
Inventors: 闵巍
Original assignee: WUXI JIEYING TECHNOLOGY Co Ltd
Current assignee: WUXI JIEYING TECHNOLOGY Co Ltd
Priority date: 2015-06-09
Filing date: 2015-06-09
Publication date: 2015-11-04
Anticipated expiration: 2025-06-09

Abstract

The utility model relates to a solar energy dirigible of double dynamical dual fail -safe belongs to new forms of energy aviation transport technologies field. Current aircraft all has only a driving system, is controlled by the terrorist in driving system inefficacy or cockpit, and passenger's life can't ensure, the utility model discloses a solar energy dirigible of double dynamical dual fail -safe at a power lose control, can also operate the driving system quickly separating of another kind of control system and inefficacy, as long as have a system normally to work among two kinds of driving system, passenger's life is just secure, simultaneously, the thin -film solar cell who utilizes the huge surface of dirigible to cover provides power, and this kind of solar energy dirigible of double dynamical dual fail -safe can vertical take -off, the descending, does not need airport runway, and the maintenance of being convenient for, maintenance, operation cost are low, along with the progressive thing networking new technology of science and solar cell's application, a solar energy dirigible of double dynamical dual fail -safe of safety, environmental protection will be human ideal vehicle.

Description

A kind of solar power dirigible of double dynamical double insurance

Technical field

The utility model relates to a kind of solar power dirigible of double dynamical double insurance, belongs to new forms of energy air transportation technology field.

Background technology

Adrm generally all build urban fringe in, great distance of going to the airport, block up, the time of waiting is long, burn during flight aircraft gasoline, noise, contaminated environment, aircraft trip neither be very safe, and in March, 2015, Germany Lufthansa Group copilot was chief aviation pilot pass outside hatch door, and premeditated crash passenger plane causes 150 people wrecked, terrorist is hijacked a plane, collide building, lost contact, and aircraft drifts off the course, ground crew and aircraft vehicular police, also be that some ways do not have, do not ensure the safety of passenger, boats and ships shipping is also that speed is slow, and by the restriction in navigation channel, trip is also inconvenient, and run into heavy rain, wind spout, passenger boat topples, and causes great personal casualty, property damage, high ferro, motor-car, subway are also build Eastern China, economically developed area in, and cost is high again, highway is gone on a journey, and congestion in road, limit are especially purchased, odd-and-even license plate rule etc., be badly in need of a kind of safety, environmental protection, the easily vehicle, present dirigible is a kind of steerable aircraft being lighter than air, the buoyancy relying on the hydrogen of air bag inner sealing or helium to produce aloft floats, rely on driving engine to produce parallel pulling force aloft to advance, dirigible has, volume is large, have a smooth flight, noise is low, can fly side, inverted flight, hovering, convenient operation is driven, dirigible safety is good, require low to pad, can fly by low-altitude low-speed, there is hovering ability, safety, cost is low, the energy saved by dirigible, cruise duration is long, voyage is far away, load is large, be convenient to maintaining, purchase commodity, maintenance expense, place cost of erection, flight takes with training fee lower, operation cost is 1/5 of aircraft, 1/10 of helicopter, along with the progressive Internet of Things up-to-date technology of science and the application of solar cell, dirigible has more wide prospect.

Utility model content

The purpose of this utility model is to overcome deficiency of the prior art, provides a kind of solar power dirigible of double dynamical double insurance.Due to the aerial aerocraft that dirigible is bulky, hydrogen in dirigible or helium provide dirigible lift upwards, the outside face that dirigible is huge is coated with thin-film solar cells, and the power storage of acquisition, in storage battery and standby battery, provides power to driving engine, under the lift of dirigible and the double dynamical effect of piggyback pod engine power, a kind of solar power dirigible of double dynamical double insurance can not need airfield runway, smooth roof in city, park, take off and land in vacant lot, lift is lost or engine breakdown runs out of steam as run into dirigible gas leakage in flight way, the extraordinary circumstances such as terrorist's airplane hijacking, in order to protect the safety of passenger in Security Module, airship envelope can be abandoned instantaneously or abandon piggyback pod instantaneously, rely on the power of Security Module and piggyback pod or Security Module and dirigible, as long as two kinds of power have a kind of power to work, just can ensure that Security Module pulsation-free lands, ensure the safety of passenger.

Main technical schemes of the present utility model is achieved in that and is jointly made up of dirigible 1, Security Module 11 and piggyback pod 16; Security Module 11 is embedded in piggyback pod 16, is connected with piggyback pod attaching parts fourth 15 by Security Module and piggyback pod attaching parts first 12, Security Module and piggyback pod attaching parts second 13, Security Module and piggyback pod attaching parts the third 14, Security Module; Dirigible 1, on the top of Security Module 11, is connected with Security Module attaching parts fourth 10 by dirigible and Security Module attaching parts first 7, dirigible and Security Module attaching parts second 8, dirigible and Security Module attaching parts the third 9, dirigible; Piggyback pod 16 is made up of jointly driving engine 20, wing 21, flap rotation axis 22, support 23, master controller 17 and storage battery 18; Dirigible 1 outside face is coated with thin-film solar cells 2, and dirigible 1 inside is made up of jointly auxiliary standby air bag first 3, auxiliary standby air bag second 4, conductor wire 5, dirigible emergency controller 6 and standby battery 19;

Piggyback pod 16 outside is provided with driving engine 20, wing 21, flap rotation axis 22 and support 23; Inside is provided with master controller 17 and storage battery 18;

Thin-film solar cells 2 is connected with auxiliary standby air bag first 3, auxiliary standby air bag second 4, dirigible emergency controller 6 and standby battery 19 by conductor wire 5; Conductor wire 5 is connected with master controller 17, storage battery 18 and driving engine 20 with Security Module attaching parts second 8 with Security Module attaching parts first 7 and dirigible by dirigible;

Security Module 11 is circular cabin or square cabin or oval cabin or polygon cabin.

Master controller 17 controls being separated of dirigible 1 and Security Module 11, be moment explosion be separated or launch instantaneously be separated or moment snap close be separated.

Dirigible emergency controller 6 controls being separated of Security Module 11 and piggyback pod 16, be moment explosion be separated or launch instantaneously be separated or moment snap close be separated.

The connection of dirigible 1 and Security Module 11 is 2 connections on two ring surfaces or the Mulit-point Connection on two ring surfaces or connects between two ring surfaces.

The connection of Security Module 11 and piggyback pod 16 a bit connects or connects between Mulit-point Connection or two ring surfaces.

Compared with prior art, the beneficial effects of the utility model are: the aircraft such as existing aircraft or dirigible, substantially be all a kind of power system, controlled by terrorist in power system inefficacy or aircraft or hit by guided missile, passenger can only leave it to chance in the sky; The utility model adopts a kind of power system of double dynamical double insurance, at a kind of power system get out of hand of aircraft, the power system quick separating of another kind of power control system and inefficacy can also be operated, as long as have a kind of power system normally to work in two kinds of power systems, the life of passenger just can be protected; Meanwhile, aircraft of the present utility model can take off vertically, land, and utilizes solar power as power, to taking off and place also not requirement of landing; Along with the high speed development of science and technology, the use of superpower jet engine, sky airborne aircraft is more and more faster, at least can than aircraft carrier and LPX fast; The solar power dirigible of a kind of double dynamical double insurance of miniaturization will be the desirable vehicle of home journey.

Accompanying drawing explanation

Fig. 1 is integral structure schematic diagram of the present utility model.

Fig. 2 is Security Module structural representation of the present utility model.

Fig. 3 is piggyback pod structural representation of the present utility model.

Detailed description of the invention

A kind of hull surface of solar power dirigible of double dynamical double insurance is covered by thin-film solar cells, the electrical power storage produced is in solar cell and solar cell for subsequent use, for the driving engine of dirigible and piggyback pod provides power, Security Module, in the middle of dirigible and piggyback pod, is connected with dirigible and piggyback pod by upper and lower four attaching partss; In the middle of a kind of solar power airship flight of double dynamical double insurance, suddenly dirigible cisco unity malfunction is run into, flight management personnel are by controlling master controller, Security Module is made to be separated with dirigible instantaneously, Security Module is together with piggyback pod, by the engine power safe falling on wing, ensure the safety of passenger; In the middle of a kind of solar power airship flight of double dynamical double insurance, suddenly the driving engine cisco unity malfunction on wing is run into or the master controller in driving compartment is controlled by terrorist, working flight personnel are by dirigible emergency controller, Security Module is made to be separated with piggyback pod instantaneously, dirigible, together with Security Module, by the power of the auxiliary standby air bag in dirigible, operates dirigible emergency controller, make Security Module safe falling together with dirigible, ensure the life security of passenger.

Embodiment in is by reference to the accompanying drawings further described by the utility model below:

Along with the progressive dirigible of science and the weight of aircraft more and more lighter, thin-film solar cells conversion ratio also can be more and more higher, require that we more and more use clean energy resource, thin-film solar cells on dirigible provides power to the driving engine of dirigible and piggyback pod, hydrogen in dirigible or helium are returned whole aircraft and are provided lift upwards, because piggyback pod has certain weight, so be also not enough to make whole aircraft go up to the air, flap rotation axis is controlled by master controller, make wing vertical in ground when 90 degree, now the lift that provides of engine rotation is maximum, when not needing runway, a kind of solar power dirigible of double dynamical double insurance just can be made vertically to rise, rise to certain safe altitude, by manipulation flap rotation axis, drive the driving engine on wing and wing, rotate to horizontal direction, a kind of solar power dirigible of double dynamical double insurance just can be made to have the power of horizontal flight forward, in order to increase the electric energy generated of solar cell, also can cover film solar cell on wing, when the engine speed of piggyback pod slows down, under gravity, whole aircraft starts to decline, by controlling flap rotation axis, drive the driving engine on wing and wing, rotate to vertical direction, make a kind of landing of solar power dirigible safety and steady of double dynamical double insurance, the electric energy that thin-film solar cells on daytime dirigible produces, is stored in storage battery and standby battery, when flying for night, dirigible emergency controller be cannot work at piggyback pod get out of hand, engine damage, passenger survival uses when being on the hazard, can be the passenger in the flight attendant of Security Module or Security Module, operation dirigible emergency controller, Security Module is separated rapidly, away from danger with piggyback pod with dirigible, personnel in Security Module pass through to control the dirigible emergency controller in dirigible, the landing of safety, also can as the air-drop vehicle of a kind of goods handling to greatest extent or personnel, when arriving overhead, destination, chaufeur in piggyback pod controls master controller, dirigible is separated rapidly with piggyback pod together with the goods in Security Module or personnel, in Security Module, chaufeur controls the dirigible emergency controller in dirigible, safety, to land appointed place accurately, then rely on the power of dirigible to transport a small amount of personnel or goods is withdrawn.

Now enumerate embodiment as follows:

Embodiment one: in the middle of a kind of solar power airship flight of double dynamical double insurance, suddenly dirigible cisco unity malfunction is run into, flight management personnel are by controlling master controller, Security Module is made to be separated with dirigible instantaneously, Security Module is together with piggyback pod, by controlling flap rotation axis, drive the driving engine on wing and wing, rotate to vertical direction, make wing vertical in ground 90 degree, the lift that engine rotation provides is maximum, it is exactly now an autogyro, do not need to glide, by the anglec of rotation of controlling machine wing engine, just energy safe falling, ensure the safety of passenger.

Embodiment two: in the middle of a kind of solar power airship flight of double dynamical double insurance, suddenly run into driving engine on the wing master controller all in cisco unity malfunction or driving compartment to be controlled by terrorist, working flight personnel are by dirigible emergency controller, Security Module is made to be separated rapidly with piggyback pod with dirigible instantaneously, due to the heavier-weight of piggyback pod, Security Module and dirigible lighter in weight, by the power of the auxiliary standby air bag in dirigible, operation dirigible emergency controller, make Security Module safe falling together with dirigible, ensure the life security of passenger.

Claims

1. a solar power dirigible for double dynamical double insurance, is made up of jointly dirigible (1), Security Module (11) and piggyback pod (16); Security Module (11) is embedded in piggyback pod (16), is connected with piggyback pod attaching parts first (12), Security Module by Security Module with piggyback pod attaching parts second (13), Security Module with piggyback pod attaching parts third (14), Security Module with piggyback pod attaching parts fourth (15); Dirigible (1), on the top of Security Module (11), is connected with Security Module attaching parts fourth (10) with Security Module attaching parts third (9), dirigible with Security Module attaching parts second (8), dirigible with Security Module attaching parts first (7), dirigible by dirigible; Piggyback pod (16) is made up of jointly driving engine (20), wing (21), flap rotation axis (22), support (23), master controller (17) and storage battery (18); Dirigible (1) outside face is coated with thin-film solar cells (2), and dirigible (1) inside is made up of jointly auxiliary standby air bag first (3), auxiliary standby air bag second (4), conductor wire (5), dirigible emergency controller (6) and standby battery (19);

Piggyback pod (16) outside is provided with driving engine (20), wing (21), flap rotation axis (22) and support (23); Inside is provided with master controller (17) and storage battery (18);

Thin-film solar cells (2) is connected with auxiliary standby air bag first (3), auxiliary standby air bag second (4), dirigible emergency controller (6) and standby battery (19) by conductor wire (5); Conductor wire (5) is connected with master controller (17), storage battery (18) and driving engine (20) with Security Module attaching parts second (8) with Security Module attaching parts first (7) and dirigible by dirigible;

It is characterized in that, described Security Module (11) is circular cabin or oval cabin or polygon cabin.

2. the solar power dirigible of a kind of double dynamical double insurance according to claim 1, is characterized in that, described master controller (17) control dirigible (1) is separated with Security Module (11), is that moment explosion is separated or launches instantaneously separation or moment snap close separation.

3. the solar power dirigible of a kind of double dynamical double insurance according to claim 1, it is characterized in that, described dirigible emergency controller (6) control Security Module (11) is separated with piggyback pod (16), is that moment explosion is separated or launches instantaneously separation or moment snap close separation.

4. the solar power dirigible of a kind of double dynamical double insurance according to claim 1, is characterized in that, described dirigible (1) and the connection of Security Module (11) are 2 connections on two ring surfaces or the Mulit-point Connection on two ring surfaces or connect between two ring surfaces.

5. the solar power dirigible of a kind of double dynamical double insurance according to claim 1, is characterized in that, described Security Module (11) and the connection of piggyback pod (16) a bit connect or connect between Mulit-point Connection or two ring surfaces.