CN208734485U - A kind of wind electricity generating system for aerospace - Google Patents

Abstract

The utility model discloses a kind of wind electricity generating systems for aerospace, its structure includes shaft, connecting rod, inductor, conducting wire, transmitting catheter, accumulator, orbital module, controller, stabilising arrangement, flabellum, accumulator left end fits with orbital module right, controller left end is equipped with stabilising arrangement, flabellum insertion is installed on stabilising arrangement, a kind of wind electricity generating system for aerospace of the utility model, it is rotated by shaft, active force is transmitted on buffer stopper and piston rod, power is applied on screw rod by buffer stopper, screw rod, which moves up and down drive, rotates gear, and power is conducted to buffer spring to buffer, it is pushed inside hydraulic cylinder by piston rod simultaneously and squeezes oil liquid, so that the piston driving piston rod and reset spring of top, to carry out further buffering, stable effect is played to shaft, It avoids shifting when rotation, and causes Caton, effectively improve the service life of shaft.

Description

A kind of wind electricity generating system for aerospace

Technical field

The utility model is a kind of wind electricity generating system for aerospace, belongs to wind electricity generating system technical field.

Background technique

Wind-power electricity generation is that the kinetic energy kept watch switchs to electric energy, wind energy as a kind of clean renewable energy, increasingly by The attention of countries in the world, the amount of accumulateing is huge, and global wind energy is about 2.74 × 10^9MW, wherein available wind energy is 2 × 10^ 7MW, the water energy total amount than that can develop and use on the earth is also 10 times big, and wind is utilized by people very early -- mainly pass through windmill Come draw water, flour milling etc., and present, interested people are how to use wind to generate electricity.

Prior art discloses application No. is a kind of 201721444310.8 wind power generation dresses for aerospace It sets, comprising: product air duct and generating set；The long-pending air duct includes coaxial outer cylinder and inner cylinder；The outer circumference surface of the inner cylinder There is spacing between the inner wall of outer cylinder；Tubaeform ventilating duct is provided between the inner cylinder and outer cylinder；The ventilating duct one The outside of end connection outer cylinder, the inner cavity that other end connection inner cylinder has；Impeller is installed, the impeller includes leaf in the inner cylinder Piece and rotation axis；The blade is arranged on the rotating shaft, and spiral upwardly extends；The generating set setting is under product air duct Side；The rotation axis and generating set are sequentially connected, but the prior art is deviated due to being easy to produce vibration when shaft rotates, To cause Caton phenomenon, the service life of shaft is caused to be affected.

Utility model content

In view of the deficienciess of the prior art, the utility model aim is to provide a kind of wind power generation for aerospace Device, to cause Caton phenomenon, leads to shaft with the prior art of solution due to being easy to produce vibration offset when shaft rotation Service life the problem of being affected.

To achieve the goals above, the utility model is achieved through the following technical solutions: a kind of navigate for aviation It wind electricity generating system, structure include shaft, connecting rod, inductor, conducting wire, transmitting catheter, accumulator, orbital module, control Device processed, stabilising arrangement, flabellum, the shaft insertion are installed on stabilising arrangement, and the shaft is surrounded by flabellum, the connection Bar is mutually welded with stabilising arrangement, and the connecting rod is connected with controller, and the transmitting catheter insertion is installed on orbital module, institute It states transmitting catheter to be connected with accumulator, the accumulator left end fits with orbital module right, the orbital module and controller It mutually welds, the controller left end is equipped with stabilising arrangement, and the flabellum insertion is installed on stabilising arrangement, the stabilising arrangement packet Protecting crust, gear, screw rod, buffer spring, piston, piston rod, reset spring, hydraulic cylinder, fixator, buffer stopper are included, it is described Protecting crust is mutually welded with reset spring, and the protecting crust is connected with fixator, and the screw rod both ends are equipped with gear, the spiral shell Spinner handle is connected with reset spring, and the screw rod is mutually welded with buffer stopper, and the reset spring insertion is installed on buffer spring On, it fits above the piston with piston rod bottom, piston is equipped with inside the hydraulic cylinder, the piston rod insertion is installed on On reset spring, hydraulic cylinder is equipped with inside the protecting crust.

Further, inductor is equipped with above the controller.

Further, the conducting wire insertion is installed on inductor.

Further, the shaft is surrounded by buffer stopper.

Further, the connecting rod is an a length of 3m, width 0.5m, the rectangular parallelepiped structure of a height of 1m.

Further, the inductor uses model JLD1U, has response fast, precision is high, the good feature of stability.

Further, the controller uses NE040S controller, and strong interference immunity, control is simply.

Beneficial effect

A kind of wind electricity generating system for aerospace of the utility model, is rotated by shaft, active force is transmitted to On buffer stopper and piston rod, power is applied on screw rod by buffer stopper, screw rod, which moves up and down drive, rotates gear, and Power is conducted to buffer spring to buffer, while being pushed inside hydraulic cylinder by piston rod and squeezing oil liquid, so that the work of top It fills in and drives piston rod and reset spring, to carry out further buffering, stable effect is played to shaft, hair when avoiding rotating Raw offset, and Caton is caused, effectively improve the service life of shaft.

Detailed description of the invention

Upon reading the detailed description of non-limiting embodiments with reference to the following drawings, other spies of the utility model Sign, objects and advantages will become more apparent upon:

Fig. 1 is a kind of structural schematic diagram of the wind electricity generating system for aerospace of the utility model；

Fig. 2 is a kind of structural schematic diagram of stabilising arrangement of the utility model.

In figure: shaft -1, connecting rod -2, inductor -3, conducting wire -4, transmitting catheter -5, accumulator -6, orbital module -7, control Device -8 processed, stabilising arrangement -9, flabellum -10, protecting crust -901, gear -902, screw rod -903, buffer spring -904, piston - 905, piston rod -906, reset spring -907, hydraulic cylinder -908, fixator -909, buffer stopper -910.

Specific embodiment

To be easy to understand the technical means, creative features, achievement of purpose, and effectiveness of the utility model, below In conjunction with specific embodiment, the utility model is further described.

Fig. 1, Fig. 2 are please referred to, the utility model provides a kind of wind electricity generating system technical solution for aerospace: its Structure includes shaft 1, connecting rod 2, inductor 3, conducting wire 4, transmitting catheter 5, accumulator 6, orbital module 7, controller 8, stablizes dress 9, flabellum 10 is set, the insertion of shaft 1 is installed on stabilising arrangement 9, and the shaft 1 is surrounded by flabellum 10, the connecting rod 2 It is welded with 9 phase of stabilising arrangement, the connecting rod 2 is connected with controller 8, and the insertion of transmitting catheter 5 is installed on orbital module 7 On, the transmitting catheter 5 is connected with accumulator 6, and 6 left end of accumulator fits with 7 right of orbital module, the orbital module 7 weld with 8 phase of controller, and 8 left end of controller is equipped with stabilising arrangement 9, and the insertion of flabellum 10 is installed on stabilising arrangement 9 On, the stabilising arrangement 9 includes protecting crust 901, gear 902, screw rod 903, buffer spring 904, piston 905, piston rod 906, reset spring 907, hydraulic cylinder 908, fixator 909, buffer stopper 910, the protecting crust 901 are welded with 907 phase of reset spring It connects, the protecting crust 901 is connected with fixator 909, and 903 both ends of screw rod are equipped with gear 902, the screw rod 903 It is connected with reset spring 907, the screw rod 903 is welded with 910 phase of buffer stopper, and the insertion of reset spring 907 is installed on On buffer spring 904,905 top of piston fits with 906 bottom of piston rod, and piston is equipped with inside the hydraulic cylinder 908 905, the insertion of piston rod 906 is installed on reset spring 907, and hydraulic cylinder 908 is equipped with inside the protecting crust 901, described Inductor 3 is equipped with above controller 8, the insertion of conducting wire 4 is installed on inductor 3, and the shaft 1 is surrounded by buffer stopper 910, the connecting rod 2 is an a length of 3m, and width 0.5m, the rectangular parallelepiped structure of a height of 1m, the inductor 3 is using model JLD1U has response fast, and precision is high, the good feature of stability, and the controller 8 uses NE040S controller, anti-interference By force, control is simple.

Accumulator 6 described in this patent is one of hydropneumatic system energy savings device, it is in due course It is that compression energy or position can store by the energy conversion in system, can be changed into when system needs, and by compression energy or position Hydraulic or air pressure etc. can and release, mend feed system again, when system instantaneous pressure increase when, this part can be absorbed in it Energy, to guarantee that whole system pressure is normal, the orbital module 7 is also referred to as space capsule, and orbital module is navigated after airship injection Its employee makees, the place of life, and in cabin in addition to having the life devices such as food, drinking-water and collecting excrement and urine device, there are also spaces to answer It is set with the instrument with scientific experimentation.

Such as: the wind-force that Li master worker passes through outer room in operation drives flabellum 10 to rotate, so that shaft 1 is rotated, Active force is transmitted on buffer stopper 910 and piston rod 906, power is applied on screw rod 903 by buffer stopper 910, screw rod 903, which move up and down drive, rotates gear 902, and power is conducted to buffer spring 904 and is buffered, while by piston rod 906 push extruding oil liquid inside hydraulic cylinder 908, so that the piston 905 of top drives piston rod 906 and reset spring 907, from And carry out further buffering, stable effect is played to shaft 1, enable flabellum 10 it is stable rotate, navigate for aviation It generates electricity.

The utility model solves the prior art due to being easy to produce vibration offset when shaft rotates, to cause Caton existing As the problem of causing the service life of shaft to be affected, the utility model is combined with each other by above-mentioned component, passes through shaft Active force is transmitted on buffer stopper and piston rod, power is applied on screw rod by buffer stopper, screw rod moves up and down by rotation Drive rotates gear, and power is conducted to buffer spring and is buffered, while being pushed and being squeezed inside hydraulic cylinder by piston rod Pressure oil liquid, so that the piston driving piston rod and reset spring of top play stabilization to shaft to carry out further buffering Effect, avoid shifting when rotation, and cause Caton, effectively improve the service life of shaft.

The basic principles and main features of the present invention and the advantages of the present invention have been shown and described above, for For those skilled in the art, it is clear that the present invention is not limited to the details of the above exemplary embodiments, and without departing substantially from this In the case where the spirit or essential attributes of utility model, the utility model can be realized in other specific forms.Therefore, no matter From the point of view of which point, the present embodiments are to be considered as illustrative and not restrictive, and the scope of the utility model is by institute Attached claim rather than above description limit, it is intended that will fall within the meaning and scope of the equivalent elements of the claims All changes are embraced therein.It should not treat any reference in the claims as limiting related right It is required that.

In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art The other embodiments being understood that.

Claims (5)

1. a kind of wind electricity generating system for aerospace, it is characterised in that: its structure include shaft (1), connecting rod (2), Inductor (3), conducting wire (4), transmitting catheter (5), accumulator (6), orbital module (7), controller (8), stabilising arrangement (9), flabellum (10), shaft (1) insertion is installed on stabilising arrangement (9), and the shaft (1) is surrounded by flabellum (10), the connection Bar (2) is mutually welded with stabilising arrangement (9), and the connecting rod (2) is connected with controller (8), transmitting catheter (5) the insertion peace Loaded on orbital module (7), the transmitting catheter (5) is connected with accumulator (6), accumulator (6) left end and orbital module (7) Right fits, and the orbital module (7) is mutually welded with controller (8), and controller (8) left end is equipped with stabilising arrangement (9), institute It states flabellum (10) insertion to be installed on stabilising arrangement (9), the stabilising arrangement (9) includes protecting crust (901), gear (902), spiral shell Spinner handle (903), piston (905), piston rod (906), reset spring (907), hydraulic cylinder (908), is fixed buffer spring (904) Device (909), buffer stopper (910), the protecting crust (901) are mutually welded with reset spring (907), the protecting crust (901) and solid Determine device (909) to be connected, screw rod (903) both ends are equipped with gear (902), the screw rod (903) and reset spring (907) it is connected, the screw rod (903) is mutually welded with buffer stopper (910), and reset spring (907) insertion is installed on slow It rushes on spring (904), fits above the piston (905) with piston rod (906) bottom, set inside the hydraulic cylinder (908) Have piston (905), piston rod (906) insertion is installed on reset spring (907), is equipped with inside the protecting crust (901) Hydraulic cylinder (908).

2. a kind of wind electricity generating system for aerospace according to claim 1, it is characterised in that: the controller (8) top is equipped with inductor (3).

3. a kind of wind electricity generating system for aerospace according to claim 1, it is characterised in that: the conducting wire (4) insertion is installed on inductor (3).

4. a kind of wind electricity generating system for aerospace according to claim 1, it is characterised in that: the shaft (1) buffer stopper (910) are surrounded by.

5. a kind of wind electricity generating system for aerospace according to claim 1, it is characterised in that: the connecting rod It (2) is an a length of 20cm, width 2cm, the rectangular parallelepiped structure of a height of 6cm.