CN202186516U

CN202186516U - High-altitude combined power-generating device

Info

Publication number: CN202186516U
Application number: CN2011200532950U
Authority: CN
Inventors: 唐耀辉
Original assignee: Individual
Current assignee: Individual
Priority date: 2011-03-03
Filing date: 2011-03-03
Publication date: 2012-04-11
Anticipated expiration: 2021-03-03

Abstract

The utility model relates to a high-altitude combined power-generating device. Facilities for stabilizing are a reinforced concrete foundation arranged on the ground or island reefs, a pulling cable and a height permitted cable. The upper end of the pulling cable is tied to an airplane body, the lower end of the pulling cable is fixed on the reinforced concrete foundation under the front of the airplane body, thereby ensuring the airplane body to be located at a proper horizontal position. The upper end of the height permitted cable is tied to the airplane body, the lower end of the height permitted cable is fixed on the reinforced concrete foundation right under the airplane body, thereby stabilizing the airplane body at a set height. The device utilizes two power-generating devices arranged on the airplane body to generate electricity. The high-altitude combined power-generating device is divided into a land taking-off type and an overwater taking-off type, and most part of the airplane body of the device is made of carbon fiber or fiberglass composite materials with high specific strength.

Description

The high-altitude combined power generation device

Technical field

The utility model relates to a kind of combined power generation device, particularly a kind of high-altitude combined power generation device that utilizes high altitude wind energy and high-altitude solar combined power generating.

Background technology

Along with the development of human society to energy demand and environmental requirement, the regenerative resource of cleaning becomes the important energy resource gradually.Solar power and wind energy are the most valued current green energy resources, and wind-power electricity generation and solar electrical energy generation are the topmost forms of utilizing of these two kinds of energy.But because therefore present solar electrical energy generation and wind energy generating plant can receive the region all apart from ground or the low latitude of air space above sea below 200 meters, the influence of many factors such as season and meteorology, randomness is stronger, and is at times strong and at other times weak, even cut in and out etc.In addition, the wind-force in low latitude is also less, and in general, these two kinds of energy seem in the low latitude, and grade is very low, is used with being difficult to stability and high efficiency.

There is winds aloft in high-altitude about height above sea level one myriametre.Winds aloft is that air circulation produces under the effect of deflection force of earth rotation.Therefore, winds aloft receives ground, and the influence of factors such as sea and season and meteorology is very little, and regularity is very strong, and wind direction is stable throughout the year, only concentrates on minority tens days in annual calm day.Though the air in high-altitude is thin, because the wind speed of winds aloft is high, wind-force is equivalent to ground and blows the storm wind more than 11 grades throughout the year.In different altitude above sea level and different its wind speed of latitude difference to some extent, still, on same position height, wind direction and wind speed are more stable.The wind-force of winds aloft approximately is tens times to tens times of low latitude wind, and the distribution of winds aloft is much more extensive than low latitude wind, and according to both gross horsepowers that can supply utilize according to a preliminary estimate, winds aloft exceeds more than hundred times than low latitude wind.

On the height at winds aloft place, cloud amount seldom, the radiation of sunshine is very stable in the daytime, do not rain, the harassment of adverse factors such as snow and ice hail and flying bird, therefore, high altitude wind energy and high-altitude solar power are two kinds of highly stable and profuse regenerative resources.Because relevant with it technical equipment does not appear as yet, so, fail so far these two kinds of green regenerative energy sources are used.

Summary of the invention

The purpose of the utility model is to provide a kind of high-altitude combined power generation device that utilizes high altitude wind energy and high-altitude solar power to come together to generate electricity.

The profile of high-altitude combined power generation device main body is an electronic high-altitude vehicle, and its carrier is that aircraft body 1 adopts normal arrangement (or layouts such as canard, string data and Lian Yi), unit body (or multimachine body), single vertical tail (or many vertical tails).The rear end at vertical tail top is an electric propulsion system 2.Electric propulsion system 2 has two kinds of mode of operations, and a kind of is exactly electric propulsion system 2 patterns, and another kind is wind power generating set 2 patterns, and two kinds of patterns can be changed mutually.Therefore, also to two kinds of mode of operations should be arranged, a kind of is exactly high-altitude combined power generation device pattern to the high-altitude combined power generation device, and another kind is electronic high-altitude vehicle pattern, two kinds of patterns also can be corresponding conversion each other.Electric propulsion system 2 is drive systems of electronic high-altitude vehicle, when this drive system when electric propulsion system 2 mode converting become wind power generating set 2 patterns, electronic high-altitude vehicle pattern is the corresponding high-altitude combined power generation device pattern that converts to.

The structural principle of electric propulsion system 2 and the mutual conversion of wind power generating set 2 patterns; The slurry that generally adopts with present propeller aeroplane is the same apart from the structural principle of regulating and controlling mechanism; Just regulate and control varying in size of amplitude; The telecommand equipment that buys on the market and servo configuration at corresponding position, can be reached the purpose of regulation and control electric propulsion system 2 and wind power generating set 2 mutual translative mode through remote control.

The aircraft body 1 of high-altitude combined power generation device and corresponding stabilization works under the wind action of high-altitude, can produce enough big lift, guarantee that aircraft body 1 can be on both take the altitudes in high-altitude.This stabilization works is reinforced concrete foundation 7,8, trailing cable 3 and the limit for height rope 4 on ground or islands and reefs, and trailing cable 3 upper ends tie up on the aircraft body 1, and the lower end is fixed on the reinforced concrete foundation 7 on aircraft body ground, 1 front lower place or the islands and reefs.Guarantee that aircraft body 1 is in the proper level position; Limit for height rope 4 upper ends tie up on the aircraft body 1; The lower end is fixed on the reinforced concrete foundation 8 on ground under the aircraft body 1 or the islands and reefs; The aircraft body 1 of this device hovers in the torrent of winds aloft, is equal to it and in altitude air, does unaccelerated flight.The utilization of this device is contained in two kinds of generating set generatings on the aircraft body 1.Wherein a kind of generating set is to utilize the fuselage of aircraft body 1, wing and vertical tail to have very big face area, at the upper surface of aircraft body 1 with towards the major part of the side of sunshine, lays large-area solar battery group 5.Another kind of generating set is the wind power generating set 2 of aircraft body 1 vertical tail top rear; Wind power generating set 2 has two kinds of mode of operations; Wherein a kind of is exactly the pattern of wind power generating set 2 self, and another kind is electric propulsion system 2 patterns, and two kinds of patterns can be changed mutually.With electronic high-altitude vehicle pattern be complementary what be that pattern and the high-altitude combined power generation device of electric propulsion system 2 be complementary is the pattern of wind power generating set 2.The solar battery group 5 of high-altitude combined power generation device is stably utilized solar electrical energy generation between daytime, 2 of wind power generating set are stably utilized the high altitude wind energy generating round the clock.

Description of drawings

Below in conjunction with Figure of description the utility model is further described.

The utility model is the high-altitude combined power generation device; Fig. 1 of Figure of description is the land type that takes off of this device; Fig. 2 is the water takeoff type of this device; The difference of the two is: be equipped with under the fuselage of the aircraft body 1 of the land type that takes off and supply it under the fuselage of the land rolling start and the fixed landing gear 6. water takeoff types of landing usefulness, fixed landing gear 6 not to be installed, but the lower part of fuselage is made the type shape of hull lower part, for the take off usefulness of landing of hydroplane.The upper end of trailing cable 3 and limit for height rope 4 is joining aircraft body 1, and the lower end of trailing cable 3 is fixed on the reinforced concrete foundation 7 on the ground, aircraft body 1 front lower place (or islands and reefs).The lower end of limit for height rope 4 is fixed under the aircraft body 1 on the reinforced concrete foundation 8 on the ground (or islands and reefs).Trailing cable 3 and limit for height rope 4 also are simultaneously high-altitude combined power generation device (or islands and reefs) carriers of transmitting electric power earthward.

The specific embodiment

In order to implement the utility model.Adopt the mode of airplane design that the high-altitude combined power generation device is designed, in order to reduce the wing load of aircraft body 1, aircraft body 1 adopts high carbon fibre composite material and the glass fiber compound material of strength-to-density ratio to make.Especially wind power generating set 2 (being electric propulsion system 2) manufacture and design lightweight as much as possible, the solar battery group 5 on the aircraft body 1 adopts thin film solar cells.

Make and after related work accomplishes, select the date of ceiling unlimited (or partly cloudy) at the high-altitude combined power generation device, with the upper end of trailing cable 3 and the limit for height rope 4 aircraft body 1 of ining succession, the lower end is bound up on the traction machine (full-sized car or large high-speed ship, down with).Starting traction machine is drawing aircraft body 1 against the wind direction of winds aloft and is sliding forward; After reaching suitable speed, utilize remote control mode to make the wind power generating set 2 of aircraft body 1 convert electric propulsion system 2 patterns to; The solar battery group 5 of this device is to electric propulsion system 2 power supplies simultaneously; High-altitude combined power generation device pattern converts electronic high-altitude vehicle pattern at once to, and electronic high-altitude vehicle quickens running take off under the driven in common of traction machine and electric propulsion system 2.After both arriving take the altitude, the solar battery group 5 of this device stops to electric propulsion system 2 power supplies, and electric propulsion system 2 patterns convert wind power generating set 2 patterns immediately into, and electronic high-altitude vehicle pattern converts high-altitude combined power generation device pattern simultaneously into.The lower end of trailing cable 3 is promptly fixing from the reinforced concrete foundation 7 that traction machine is transferred on the ground, aircraft body 1 front lower place (or islands and reefs), and it is fixing that the reinforced concrete foundation 8 on the ground (or islands and reefs) is then transferred under the aircraft body 1 from traction machine in the lower end of limit for height rope 4.

So far the electric power that sent of the wind power generating set on the combined power generation device of high-altitude 2 and solar battery group 5, through trailing cable 3 and limit for height rope 4 earthward (or islands and reefs) go up and carry, be connected to the grid.

Claims

1. a high-altitude combined power generation device is characterized in that: with aircraft body (1) and corresponding stabilization works; This stabilization works is provided in a side of reinforced concrete foundation (7), (8), trailing cable (3) and the limit for height rope (4) on ground or the islands and reefs; Trailing cable (3) upper end ties up on the aircraft body (1), and the lower end is fixed on the reinforced concrete foundation (7) of aircraft body (1) front lower place, guarantees that aircraft body (1) is in the proper level position; Limit for height rope (4) upper end ties up on the aircraft body (1); The lower end is fixed on the reinforced concrete foundation (8) under the aircraft body (1), and aircraft body (1) is stabilized in both take the altitudes, and the utilization of this device is contained in two kinds of generating set generatings on the aircraft body (1).

2. high-altitude according to claim 1 combined power generation device; It is characterized in that: be contained in two kinds of generating sets on the aircraft body (1); The rear end at the vertical tail top of aircraft body (1) is wind power generating set (2), the upper surface of aircraft body (1) and towards the side of sunshine, and major part is laid solar battery group (5); Wind power generating set (2) has two kinds of mode of operations; Wherein a kind of is exactly the pattern of wind power generating set (2) self, and another kind is electric propulsion system (a 2) pattern, and two kinds of patterns can be changed mutually; What be complementary with electronic high-altitude vehicle pattern is the pattern of electric propulsion system (2); What be complementary with high-altitude combined power generation device pattern is wind power generating set (2) pattern, and the solar battery group of high-altitude combined power generation device (5) is stably utilized solar electrical energy generation between daytime, and wind power generating set (2) is then stably utilized the high altitude wind energy generating round the clock.