TWM492369U - Stamping turbine blade power generator - Google Patents

Description

Stamped turbine fan generator

The present invention relates to a wind power generation device, in particular to a starter that can be started under wind conditions with less wind and a higher power generation under the same wind field conditions, and is particularly suitable for use in a stamping turbine for use on a vehicle. Fan generator.

According to the general environmental protection electrification trend of the vehicle, the charging can not be completed in time, only relying on the power stored, directly limiting the range of the vehicle's endurance, has been plagued by the use of all vehicles; Wind turbines are installed on various vehicles, and the wind energy is converted into mechanical energy by the maple impeller, and then the generator is driven by the transmission mechanism to promote the auxiliary power generation device for generating electricity by the generator.

In principle, the relative speed of the vehicle and the relative velocity of the air on the various vehicles have a relatively good air volume, so that the wind turbine can obtain more output power; however, the power of the wind power generation depends on the blades of the wind impeller. The speed of the lift generated by the aerodynamic force gives the rotational kinetic energy and the rotational angular velocity to obtain a larger torque.

At present, the focus of generator design is to improve the speed between the coil and the magnet in the generator. Therefore, the speed of the gear is increased by the gear set to increase the starting torque of the motor and increase the speed; most wind turbines or The starting torque of the micro-generator needs to be matched with the larger size fan blades in order to be more suitable for the low wind speed wind field, but the large fan blades also increase the load of the vehicle, and the generator is limited by the internal space size. The limited magnet or coil is included, and the kinetic energy of the gear transmission is also attenuated, which also causes the power of the entire group of wind turbines to be unable to increase.

Moreover, in the current wind turbines, the existing wind turbines need to occupy a large space and a proper wind field, and there is sufficient wind power; thus, the use of wind power generation on the vehicle is more difficult. The conventional permanent magnet brushless motor is a magnet mounted on the rotor. In the case of low speed operation, increasing the number of magnets can effectively increase the torque output of the motor, but when the number of poles of the motor increases, the magnetic must be relatively increased. The number of poles of the stone, thus causing problems of magnet adhesion, positioning and reliability; in addition, the number of coil slots of the stator is also relatively large, and the motor space is limited, thus causing problems in the actual production of the motor, making the multipole Motor design and production is not easy.

The main purpose of this creation is to provide a kind of punching turbine blade that can be started under wind conditions with less wind and can generate higher power in the same wind field conditions, especially suitable for installation on vehicles. Motor.

The stamped turbofan blade generator of the present invention basically comprises: a base, a first fan module, and a motor module; wherein the base is provided with a first ring bracket on a shaft of the shaft The first fan module is provided with at least one set of first wings connected to the first annular bracket and arranged in the same rotation direction; the motor module has at least one set fixed to the first ring a magnetic element of the outer ring of the bracket, and at least one set of coils corresponding to the periphery of the magnetic element.

The ramjet fan blade generator of the present invention can be mounted on a suitable mechanical structure through a pedestal. During operation, the first fan module can be relatively rotated by the wind, and then placed on the first ring bracket. The magnetic component can be inductively cut with the coil to generate electric power output through the coil; in particular, the airflow through the first fan module can be used to generate a supercharging effect, thereby greatly increasing the kinetic energy of the relative rotation of the first annular support, and the coil can be accelerated. The relative motion with the magnetic element can generate higher power generation under the same wind field conditions, and is particularly suitable for installation on the vehicle to act as an auxiliary power generating device.

The base further has an inner nozzle covering the first annular bracket and the first fan module, and an outer nozzle relatively covering the periphery of the inner nozzle and maintaining a predetermined distance from the inner nozzle Forming an inner air passage in the inner ring of the inner nozzle, and forming an outer air passage at a gap between the inner nozzle and the outer nozzle; the front edge of the outer nozzle extends oppositely from the front edge of the inner nozzle a predetermined length; and the ram turbine blade generator is disposed at the outer ring inner ring with at least one set of relatively rotatable first stage blades relative to the inner nozzle front edge, and the inner nozzle inner ring Having at least one set of pressurized blades that are gradually decreasing toward the rear and relatively rotatable relative to the front position of the first fan module, and at least one set of relative rotations relative to the rear position of the first annular bracket Turbine blades.

Further, the first annular bracket rear axle is provided with a second annular bracket and At least one second fan module, the at least one second fan module is coupled to the second ring bracket, and the at least one second fan module is provided with at least one set of opposite directions opposite to the first wing panel Two wing panels.

Further, the inner wall of the outer edge of the outer nozzle is a first reduced and enlarged Laval lance tube, and at least one set of size is arranged in the inner ring of the outer nozzle relative to the front edge of the inner nozzle. A first-stage blade that tapers toward the rear and is relatively rotatable.

The coil loop is disposed on a circumference of the second annular bracket.

The trailing edge of the outer nozzle extends a predetermined length from the trailing edge of the inner nozzle, and the trailing edge of the outer nozzle is slightly retracted, and the trailing edge of the inner nozzle forms a slightly outwardly extending nozzle.

The inner nozzle is provided with a plurality of wedge-shaped grooves at its nozzle.

The inner wall of the inner nozzle is a Laval spray tube which is firstly reduced and enlarged.

The trailing edge of the outer nozzle extends a predetermined length from the rear edge of the inner nozzle, and the trailing edge of the outer nozzle is slightly retracted, and the trailing edge of the inner nozzle forms a slightly outwardly extending nozzle; The tube is provided with a plurality of wedge-shaped grooves at the nozzle thereof; and the inner wall of the inner nozzle is a Laval lance tube which is firstly reduced and enlarged.

Specifically, the stamped turbine fan generator disclosed in the present invention can produce the following effects:

1. It can be started under wind conditions with less wind.

2. Higher power generation can be generated under the same wind field conditions.

10‧‧‧ Vehicles

11‧‧‧Electronic control system

12‧‧‧Transformers

13‧‧‧Battery

14‧‧‧Inverter

15‧‧‧Electric motor

20‧‧‧Pressed turbine fan generator

21‧‧‧Base

211‧‧‧ shaft

212‧‧‧First ring bracket

213‧‧‧Second ring bracket

214‧‧‧Inner nozzle

215‧‧‧outer nozzle

216‧‧‧ wedge groove

22‧‧‧First fan module

221‧‧‧First wing

23‧‧‧Second fan module

231‧‧‧second wing

24‧‧‧Motor Module

241‧‧‧ Magnetic components

242‧‧‧ coil

25‧‧‧First stage blades

261‧‧‧Supercharged blades

262‧‧‧Supercharged blades

263‧‧‧ Turbine blades

The first figure is a perspective cross-sectional view of a stamped turbine blade generator of the first embodiment of the present invention.

The second drawing is a plan sectional view of the stamped turbine blade generator of the first embodiment of the present invention.

The third figure is a perspective cross-sectional view of the stamped turbine blade generator of the second embodiment of the present invention.

The fourth figure is a plan sectional view of the stamped turbine blade generator of the second embodiment of the present invention.

The fifth drawing is a plan sectional view of the stamped turbine blade generator of the third embodiment of the present invention.

The sixth figure is an exploded view of the structure of the stamped turbine blade generator of the fourth embodiment of the present invention.

The seventh figure is a reference diagram for the configuration of the stamped turbine blade generator used in this creation.

This creation mainly provides a punching turbine blade generator that can be started under wind conditions with less wind and can generate higher power in the same wind field conditions, especially suitable for installation on vehicles. BRIEF DESCRIPTION OF THE DRAWINGS FIG. 1 is a perspective cross-sectional view of a stamped turbine blade generator of a first embodiment of the present invention, and a second sectional view of the stamped turbine blade generator of the first embodiment of the present invention, the stamped turbine blade generator 20 of the present invention, basically The above includes: a base 21, a first fan module 22, and a motor module 24; wherein:

The base 21 is provided with a first annular bracket 212 on a shaft 211.

The first fan module 22 is provided with at least one set of first wings 221 connected to the first annular bracket 212 and configured in the same rotational direction.

The motor module 24 has at least one set of magnetic elements 241 fixed to the outer circumference of the first annular support 212, and at least one set of coils 242 corresponding to the outer periphery of the magnetic element 241.

At the same time, the ramjet blade generator 10 of the present invention may further have an inner nozzle 214 covering the first annular bracket 212 and the first fan module 22, and An outer nozzle 215 is disposed on the periphery of the inner nozzle 214 and spaced apart from the inner nozzle 214 by a predetermined distance, so that an inner air passage is formed in the inner ring of the inner nozzle 214, and the inner nozzle 214 is An outer air passage is formed at the gap of the outer nozzle 215.

The outer edge of the outer nozzle 215 is opposite to the front end of the inner nozzle 214 by a predetermined length; and the integral punched turbine fan generator 20 is attached to the inner circumference of the outer nozzle 215 with respect to the front edge of the inner nozzle 214 At least one set of relatively rotatable first-stage blades 25 is disposed, and the inner ring of the inner nozzle 214 is provided with a complex array size gradually decreasing toward the rear with respect to the front position of the first fan module 22, and is relatively rotatable. The pressurized blades 261, 262, and at least one set of relatively rotatable turbine blades 263 are disposed relative to the rear of the first annular support 212.

In the above-mentioned structure, the first stage blade 25 can be utilized when the external air pressure is greater than the internal air pressure than the first stage blade 25 and the respective booster blades 261, 262 and the turbine blade 263 are themselves loaded. The pressure difference between the pressurized blades 261 and 262 and the inner and outer sides of the turbine blade 263 causes the air to flow from the high pressure to the low pressure, causing the first stage blades 25 and the respective boosting blades 261 and 262 to be lifted by the lift.

The first-stage blades 25 and the respective booster blades 261 and 262 and the turbine blades 263 are rotated by themselves during the traveling of the carrier, and the externally flowing air is sucked and drained into the outer air passage and the inner air passage respectively, and the inner nozzle 214 is added. The inner wall is a Laval spray tube that is first narrowed and enlarged, so that the gas passing through the middle can accelerate the flow, and the air sucked in front is compressed by the pressurized blades 261, 262, and the high pressure is gradually formed into a high compression ratio at a high compression ratio. Pushing the first annular module 212 and the magnetic element 241 to rotate under the first fan module 22, and the air quickly flowing out after the high-pressure air passes through the minimum cross-sectional area of the inner air passage, then pushing the turbine blade 263 opposite to the rear to rotate. .俾 can effectively improve the operating kinetic energy of the motor module 24.

Furthermore, the trailing edge of the outer nozzle 215 is opposite to the rear edge of the inner nozzle 214 by a predetermined length, and the trailing edge of the outer nozzle 215 is slightly retracted, and the trailing edge of the inner nozzle 214 forms a slight direction. The outer nozzle; even the inner nozzle 214 can be further provided with a plurality of wedge grooves 216 at its nozzle.

When the air flows through the first fan module 22 to the end nozzle of the inner nozzle 214 and the annular wedge groove 216, the lower air pressure and the rapid air of the outer air passage form a spoiler of the nozzle mouth, and the turbine blade is added. The suction force behind the 263 further accelerates the rapid discharge of the high-pressure air inside the inner air passage through the first fan module 22, so that the first fan module 22 obtains more kinetic energy, thereby improving the kinetic energy of the entire motor module 24.

In principle, the ramjet blade generator 20 of the present invention can be mounted on a suitable mechanical structure through the base 21, and in operation, the first fan module 22 can be driven by the wind to rotate relative to each other. The magnetic element 241 and the coil 242 disposed on the first annular bracket 212 are inductively cut and mutually generated to generate electric power output through the coil; in particular, the airflow passing through the first fan module 22 can generate a supercharging effect, thereby greatly improving the The relative motion of the ring holder 212 relative to the rotational kinetic energy accelerates the relative movement of the coil 242 and the magnetic element 241, and can generate a relatively high power generation under the same wind field conditions, and is particularly suitable for being used on an auxiliary power generating device for mounting on a carrier.

In the embodiment shown in the first and second figures, when the first fan module 22 rotates, the first annular bracket 212 rotates relative to each other at the same time, thereby accelerating the relative movement of the coil 242 and the magnetic element 241. Under the same wind field conditions, it can generate higher power generation, especially suitable Mounted on the carrier 10 as shown in FIG. 7 , electrically connected to the electronic control system 11 , the transformer 12 , the battery 13 , the inverter 14 , and the motor 15 of the carrier 10 for use as an auxiliary power generating device for the carrier 10 When driving, use oncoming wind power to generate electricity.

In addition, the ramjet blade generator 10 of the present invention can be further configured as a third section to create a perspective view of the ramjet blade generator of the second embodiment and a fourth diagram of the stamping of the second embodiment. A second annular bracket 213 and at least one second fan module 23 are pivotally disposed behind the first annular bracket 212, and the at least one second fan module 23 is coupled to the first fan bracket The two annular brackets 213 are connected, and the at least one second fan module 23 is provided with at least one set of second wings 231 opposite to the first wing 221; and the coil 242 is looped on the second The circumference of the annular bracket 213. Therefore, the second annular module 213 is driven by the second annular module 213 to rotate with the first annular support 212 at a relative reverse speed, and the magnetic component 241 and the ring fixed to the outer ring of the first annular support 212 are accelerated. The kinetic energy of the relative rotation of the coil 242 disposed at the periphery of the second annular bracket 213 is increased to generate more power.

Even the ramjet blade generator 10 of the present invention can be implemented as shown in the fifth sectional view of the third embodiment of the ramjet blade generator, and further the inner wall of the outer nozzle 215. The first embodiment of the outer nozzle 215 is provided with at least one set of sizes which are gradually reduced toward the rear and relatively rotatable relative to the inner edge of the inner nozzle 214. The stage vanes 25 form a relatively rotatable, unloaded booster vane which allows for better operating kinetic energy.

Of course, the stamped-turbine blade generator 10 of the present invention can also be implemented as shown in the exploded view of the stamped turbine blade generator of the fourth embodiment as shown in the sixth figure, directly on the axis of the base 21 The upper shaft of the rod 211 is provided with a first annular bracket 212 having at least one set of magnetic elements 241 and a first flap 221 provided with at least one set of the same annular configuration connected to the first annular bracket 212. a fan module 22, and a rear axle of the first annular bracket 212 is disposed opposite to the first annular bracket 212, and a peripheral ring is provided with at least one set corresponding to the periphery of the magnetic component 241. The second annular bracket 213 of the coil 242 and a second fan module 23 connected to the second annular bracket 213 and having at least one set of second wings 231. During operation, the first fan module 22 and the second fan module 23 can be driven by the wind to rotate in opposite directions, thereby allowing the magnetic components 241 respectively disposed on the first and second annular brackets 212, 213 and line The loops 242 are mutually inductively cut to generate electric power outputted through the coil 242; in particular, the airflow of the first fan module 22 and the second fan module 23 generates a supercharging effect, and the first and second annular brackets 212 and 213 can be greatly improved. Relative rotational kinetic energy, while the relative motion of the acceleration coil 242 and the magnetic element 241 also has the same performance to generate higher power generation under the same wind field conditions.

Compared with the conventional structure, the stamped turbine fan generator disclosed in the present invention can produce the following effects:

1. It can be started under wind conditions with less wind.

2. Higher power generation can be generated under the same wind field conditions.

20‧‧‧Pressed turbine fan generator

21‧‧‧Base

214‧‧‧Inner nozzle

215‧‧‧outer nozzle

216‧‧‧ wedge groove

211‧‧‧ shaft

212‧‧‧First ring bracket

213‧‧‧Second ring bracket

22‧‧‧First fan module

221‧‧‧First wing

24‧‧‧Motor Module

241‧‧‧ Magnetic components

242‧‧‧ coil

25‧‧‧First stage blades

261‧‧‧Supercharged blades

262‧‧‧Supercharged blades

263‧‧‧ Turbine blades

Claims (9)

A ramjet fan blade generator includes: a base, a first annular bracket is disposed on a shaft of a shaft; and a first fan module is provided with at least one set connected to the first annular bracket and a first wing plate of the same direction of rotation; a motor module having at least one set of magnetic elements fixed to the outer ring of the first ring frame, and at least one set of coils corresponding to the periphery of the magnetic element. The ram turbine blade generator according to claim 1, wherein the base further has an inner nozzle covering the first annular bracket and the first fan module, and a relative covering An outer nozzle surrounding the inner nozzle and maintaining a predetermined distance from the inner nozzle, forming an inner air passage in the inner ring of the inner nozzle and forming an outer portion in the gap between the inner nozzle and the outer nozzle An air passage; the front edge of the outer nozzle extends relative to a predetermined length of the inner edge of the inner nozzle; and the ram turbine blade generator is disposed at the inner circumference of the outer nozzle relative to the front edge of the inner nozzle a set of relatively rotatable first stage vanes, and at least one set of relatively rotatable booster vanes with respect to the front end of the inner spout inner tube relative to the first fan module, and relative to the first annular bracket The rear position is provided with at least one set of relatively rotatable turbine blades. The ramjet blade generator of the first or second aspect of the invention, wherein the ramjet blade generator is pivotally disposed with a second annular bracket and at least one of the first annular bracket a second fan module, the at least one second fan module is coupled to the second ring bracket, and the at least one second fan module is provided with at least one set of second wings that are opposite to the first wing . The ramjet blade generator of claim 3, wherein the coil loop is disposed at a periphery of the second annular bracket. The ramjet blade generator according to the second aspect of the invention, wherein the outer wall of the outer edge of the outer nozzle is a firstly reduced and enlarged Laval lance tube, and the inner ring of the outer nozzle is opposite At least one set of relatively rotatable first stage blades is provided at the leading edge of the inner nozzle. The ramjet blade generator according to claim 2, wherein the trailing edge of the outer nozzle extends a predetermined length from the trailing edge of the inner nozzle, and the trailing edge of the outer nozzle is slightly retracted. The trailing edge of the inner nozzle forms a slightly outwardly flared nozzle. A ramjet blade generator as claimed in claim 2, wherein the inner nozzle is provided with a plurality of wedge-shaped recesses at its nozzle. The ramjet blade generator according to claim 2, wherein the inner wall of the inner nozzle is a Laval lance tube which is firstly reduced and enlarged. The ramjet blade generator according to claim 2, wherein the trailing edge of the outer nozzle extends a predetermined length from the trailing edge of the inner nozzle, and the trailing edge of the outer nozzle is slightly retracted. a trailing edge of the inner nozzle forming a slightly outwardly extending nozzle; the inner nozzle is provided with a plurality of wedge-shaped recesses at the nozzle thereof; and the inner wall of the inner nozzle is vertically reduced and expanded by Laval Spray tube.