WO2018027536A1 - Air booster - Google Patents

Air booster Download PDF

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Publication number
WO2018027536A1
WO2018027536A1 PCT/CN2016/094128 CN2016094128W WO2018027536A1 WO 2018027536 A1 WO2018027536 A1 WO 2018027536A1 CN 2016094128 W CN2016094128 W CN 2016094128W WO 2018027536 A1 WO2018027536 A1 WO 2018027536A1
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WO
WIPO (PCT)
Prior art keywords
air
flow path
tube
outer tube
output
Prior art date
Application number
PCT/CN2016/094128
Other languages
French (fr)
Chinese (zh)
Inventor
孟三中
陈宜诚
孟佩宏
陈倞宏
Original Assignee
孟三中
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 孟三中 filed Critical 孟三中
Priority to PCT/CN2016/094128 priority Critical patent/WO2018027536A1/en
Publication of WO2018027536A1 publication Critical patent/WO2018027536A1/en

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60KARRANGEMENT OR MOUNTING OF PROPULSION UNITS OR OF TRANSMISSIONS IN VEHICLES; ARRANGEMENT OR MOUNTING OF PLURAL DIVERSE PRIME-MOVERS IN VEHICLES; AUXILIARY DRIVES FOR VEHICLES; INSTRUMENTATION OR DASHBOARDS FOR VEHICLES; ARRANGEMENTS IN CONNECTION WITH COOLING, AIR INTAKE, GAS EXHAUST OR FUEL SUPPLY OF PROPULSION UNITS IN VEHICLES
    • B60K13/00Arrangement in connection with combustion air intake or gas exhaust of propulsion units
    • B60K13/02Arrangement in connection with combustion air intake or gas exhaust of propulsion units concerning intake
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38Introducing air inside the jet
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M23/00Apparatus for adding secondary air to fuel-air mixture
    • F02M23/04Apparatus for adding secondary air to fuel-air mixture with automatic control
    • F02M23/08Apparatus for adding secondary air to fuel-air mixture with automatic control dependent on pressure in main combustion-air induction system, e.g. pneumatic-type apparatus

Definitions

  • the invention relates to a device for improving the operating efficiency of a combustion device, in particular to an air booster capable of improving the intake efficiency of a combustion device and thereby improving its combustion and operation efficiency.
  • a typical automobile, locomotive, ship or lawn mower is a source of power using an internal combustion engine such as a reciprocating engine.
  • the engine operates by mixing air and fuel in the cylinders of the engine for intake, compression, explosion, and exhaust.
  • Four programs, such as gas, produce a power output.
  • the ratio of fuel to air exploded in the engine cylinder that is, the oil-gas ratio is an important parameter affecting the operation of the engine.
  • a good oil-gas ratio is beneficial to the complete combustion of the fuel, which can enhance the horsepower of the engine output while reducing Exhaust gas emissions.
  • the combustion efficiency of the combustion device such as the engine is increased to restore the original power.
  • the prior art uses a turbocharger to force the intake of the engine to solve the aforementioned problem of incomplete combustion of the engine.
  • the turbocharger can greatly increase the horsepower of the engine output, but the gear set and the exhaust turbine are quite cumbersome and energy-consuming, and the consequent oil loss will also increase significantly, so it is not in line with the average user only need to make the engine
  • the fuel combustion inside is more complete.
  • the turbocharger which is used for active intake, requires complex modifications to the engine. The technical level of use is high and the user cannot buy it back by the store. It is not easy to use.
  • the present invention has different first and second flow paths.
  • the vortex is formed by the way of velocity and direction airflow, and the nozzle configuration is used to obtain the accelerated jet flow, so that the air outputted by the device is increased, and a low pressure zone is formed inside the air inlet port, thereby improving the intake efficiency of the air inlet and improving
  • the engine inputs air pressure and increases its combustion efficiency and reduces exhaust pollution.
  • the present invention provides an air booster comprising an outer casing and an air intake member disposed in the outer casing, wherein:
  • the outer casing is a straight tubular casing and is provided at the front end with an output pipe having a width dimension smaller than a width dimension of the remaining portion of the outer casing, and a first flow passage and a gas chamber are formed in the interior of the outer casing from the rear to the front.
  • an output flow passage is a passage extending from the rear to the front, the front end of the first flow passage communicates with the side of the rear end of the air chamber, the air chamber is a space and the front side is gradually received from the rear to the front.
  • the output flow channel is formed in the output tube, the output flow channel is a straight channel and is connected to the front end of the air chamber, and a peripheral portion of the outer casing provided with the output tube forms a through hole;
  • the air inlet member is a tubular body and is disposed at the through hole.
  • the front end of the air inlet member is located in the air chamber and faces the rear end of the output flow channel, and a second flow path is formed inside the air inlet member.
  • the length of the second flow path extending is shorter than the length of the first flow path, the front end of the second flow path is narrower than the output flow path toward the center of the output flow path, and the rear end of the second flow path is located in the outer casing In addition, it communicates with the environment around the outside of the enclosure.
  • the opening of the present invention is formed at a position corresponding to the inside of the outer casing.
  • the outer casing of the present invention comprises an outer tube and a front cover coupled to the outer tube, the outer tube is a vertically arranged straight tube body and the upper and lower opposite ends are divided into a front end and a rear end.
  • the first flow passage is formed in the outer tube, and the first flow passage forms an opening at the front and rear ends of the outer tube;
  • the front cover is provided with a cover portion which is a cover body and is sleeved and fixed a front end of the outer tube, a front side of the cover portion forming a tapered portion whose shape gradually narrows toward the front, the output tube being formed by extending from the middle of the tapered portion, wherein the air chamber is formed In the cover portion, the through opening is formed around the cover portion, and the second flow path extends for a length shorter than half of the extension length of the first flow path.
  • the cover portion of the present invention is tightly fitted to the front end of the outer tube, and the through hole is formed in a tapered portion of the cover portion;
  • the air inlet member is provided with a block portion and a a tube portion connected to the block portion, the block portion is located in the air chamber and the outer end extends to the rear of the output flow channel, the tube portion is disposed at the through hole, and the block portion is connected a side adjacent to the tube portion abuts and adheres to an inner surface of the tapered portion,
  • the second flow passage is formed in the block portion and the tube portion, and the second flow passage extends a length shorter than the The first runner extends for a quarter of the length.
  • the cover portion of the present invention is tightly fitted to the front end of the outer tube, and the through hole is formed in the tapered portion of the cover portion, corresponding to the peripheral edge of the outer end of the opening, in the cover portion
  • the outer surface is recessed to form a non-circular recess, the through hole extends through the center of the recess;
  • the air inlet member is provided with a hook-shaped air tube, the air tube is located in the air chamber and the front end is located at the Behind the output flow path, the rear end of the air pipe is disposed at the opening, and a portion of the air pipe that passes outwardly through the opening forms a flared expansion portion, and the shape of the groove is matched around the air pipe Forming a panel, the panel is embedded and adhesively fixed in the recess, the second flow channel is formed in the air tube, and the second flow channel extends for a length shorter than the first flow path extension length One quarter of the.
  • the air inlet member is provided with a jet tube, the air tube is located
  • the gas chamber is located behind the output flow channel, and a bifurcated side tube is connected at a rear end of the gas injection tube, and a rear end of the two side tubes is closely worn at two openings, the first A second flow passage is formed in the lance tube and the side tubes, and the second flow passage extends for a length shorter than a quarter of the length of the first flow passage.
  • the outer tube of the present invention is a rectangular straight tube body, and the upper and lower spaced arrangement of the outer tube combines a plurality of rectangular guiding pieces, and the leading pieces of the odd sequence are from front to back.
  • the right end edge thereof is connected to the inner wall of the right side of the outer tube and the left end edge is inclined to the left and obliquely backward, and there is a gap between the left end edge of each of the odd-numbered guide pieces and the inner wall of the left side of the outer tube;
  • Each of the guide pieces having the even number of even numbers has a left end edge connected to the inner wall of the left side of the outer tube and a right end edge extending rightward and obliquely rearward, and the right end edge of each of the even-numbered guide pieces and the outer tube There is a gap between the inner walls of the right side;
  • the first flow path is that the space inside the outer tube is divided by a plurality of guiding pieces.
  • the outer tube of the present invention is a rectangular straight tube body in which the left and right halves are oppositely combined, and the outer casing further includes a rear cover which is a cover body and is tightly fitted and fixed thereto. A plurality of air holes are bored around the rear end of the outer tube 11 around the rear end of the outer tube 11.
  • the present invention incorporates a rear end fan intake configuration at the rear end of the housing.
  • the present invention connects an external pipe at the outer end of the air intake member, and the outer pipe connects the side to the fan air intake structure.
  • the invention is used in that the outlet tube is connected to the inlet of the combustion device, such as an engine, through an intake hose.
  • the combustion device When the combustion device is operated, the negative pressure generated inside the combustion device and the inlet will be from the output pipe. Starting to attract the airflow, the air in the environment will be respectively taken from the rear end of the first flow channel and the rear end of the second flow channel, respectively, by the rear end of the outer casing and the environment around the outer casing, so that the outside air passes through the two Different channels enter the air chamber collection within the enclosure.
  • the air flow speed in the first flow path and the second flow path are different, and the air flow directions of the two flow paths are different, so that
  • the flow of the direct flow from the second flow path to the center of the output flow path can be mutually drawn with the air flow around the air chamber, and a pressurized vortex is formed in the air chamber, and the space gradually reduced by the air chamber can gradually merge the air chamber into the output flow path.
  • the airflow is accelerated, so that the air flowing forward in the gas chamber can be accelerated by the gradually reduced space, and the vortex pressure can be used to enhance the pressure and speed of the output air output of the output pipe, at the air inlet of the combustion device.
  • a low pressure zone is formed inside to further improve the intake efficiency of the intake port.
  • the effect of the present invention is that the combustion fuel connected to the combustion apparatus of the present invention, such as the engine, is burned as completely as possible by the output of pressurized air, enhancing the horsepower of the engine, reducing engine carbon deposits and generating air pollutants.
  • the invention is easy to install, and can be installed and used by the user after purchase, which is convenient for the user to use.
  • Figure 1 is a perspective view of a first preferred embodiment of the present invention
  • Figure 2 is an exploded view of the first preferred embodiment of the present invention
  • Figure 3 is a cross-sectional view showing a first preferred embodiment of the present invention.
  • Figure 4 is a schematic view showing the implementation of the first preferred embodiment of the present invention.
  • Figure 5 is a schematic view of airflow guiding according to a first preferred embodiment of the present invention.
  • Figure 6 is a schematic view showing another embodiment of the first preferred embodiment of the present invention.
  • Figure 7 is a schematic view showing still another embodiment of the first preferred embodiment of the present invention.
  • Figure 8 is a schematic view showing the implementation of a second preferred embodiment of the present invention.
  • Figure 9 is an exploded view of a second preferred embodiment of the present invention.
  • Figure 10 is a cross-sectional view showing a second preferred embodiment of the present invention.
  • Figure 11 is an exploded view of a third preferred embodiment of the present invention.
  • Figure 12 is a longitudinal sectional view showing a third preferred embodiment of the present invention.
  • Figure 13 is a transverse cross-sectional view showing a third preferred embodiment of the present invention.
  • Figure 14 is a partial cross-sectional view showing a fourth preferred embodiment of the present invention.
  • the construction includes a housing 10 and an air inlet member 20 that is coupled to the housing 10, wherein:
  • the outer casing 10 includes an outer tube 11, a rear cover 15 coupled to the rear end of the outer tube 11, and a front cover 16 coupled to the front end of the outer tube 11.
  • the outer tube 11 is a rectangular straight tube body which is vertically and partially combined with the left and right halves of the housing.
  • the two ends of the outer tube 11 are divided into front and rear and rear ends, and the outer tube 11 is surrounded by the outer tube 11
  • the four corners respectively form a chamfered shape 12, and the upper and lower spaced arrangement of the outer tube 11 combines a plurality of rectangular guide pieces 13.
  • Each of the guide pieces 13 of the odd-numbered sequence from the front to the rear has a right end edge connected to the inner wall of the right side of the outer tube 11 and a left end edge extending leftward and obliquely rearward, and the left end edge of each of the odd-numbered guide pieces 13
  • the rear cover 15 is a cover body and the front side is tightly fitted around the rear end of the outer tube 11 , and a plurality of air holes 151 are bored in the rear surface of the rear cover 15 .
  • the front cover 16 is provided with a cover portion 161.
  • the cover portion 161 is a cover body and the rear side is tightly fitted around the front end of the outer tube 11.
  • the front side of the cover portion 161 is gradually tapered toward the front.
  • the tapered portion 1611 defines an output tube 162 extending forwardly of the tapered portion 1611.
  • the output tube 162 is a straight tube and has a width smaller than a width dimension of the outer tube 11 and is formed in the cover portion 161.
  • An air chamber B the air chamber B is a space and the front side is gradually narrowed from the rear to the front.
  • the front end of the first flow path A communicates with the side of the rear end of the air chamber B, and an output flow path is formed in the output tube 162.
  • the output flow path c is a circular linear passage and communicates with the front end of the air chamber B.
  • a through opening 163 is bored around the tapered portion 1611 of the cover portion 161.
  • the air inlet member 20 is provided with a block portion 21 and a tube portion 22 connected to the block portion 21.
  • the block portion 21 of the air inlet member 20 is located in the air chamber B, and the outer end of the block portion 21 Extending the rear of the output flow path c, the air inlet member 20 is inserted and fixed to the opening 163 of the front cover 16 by the tube portion 22, and the block portion 21 abuts against the side of the tube portion 22 and Adhered to the inner surface of the tapered portion 1611, a second flow path D is formed in the block portion 21 and the tube portion 22.
  • the width of the front end of the second flow path D is narrower than the rear end of the output flow path c.
  • the length of the second flow path D is shorter than the length of the first flow path A.
  • the length of the second flow path D is shorter than the length of the first flow path A.
  • the first-class road A extends half or even a quarter of its length.
  • the outer tube 11 of the preferred embodiment is a rectangular straight tube body, and the outer tube 11 may be in the shape of a circular straight tube.
  • the cover is coupled to the rear cover 15 and the front cover 16 of the outer tube 11, and the circular profile of the outer tube 11 can be changed to a circular cover conforming to the outer shape of the outer casing 10, and the cover is coupled to the outer tube 11
  • the rear end and the front end constitute a circular straight tubular outer casing 10.
  • the plurality of guiding pieces 13 are separated from the first flow path A which is repeatedly bent and extended from the rear to the front and the left side in the inner portion of the outer tube 11.
  • a spiral piece extending rearwardly and forwardly is formed in the outer tube 11, and a first flow path A extending from the rear to the front is separated in the outer tube 11 as long as the length of the first flow path A is shorter than the second
  • the flow path D can exert the same effect regardless of whether the first flow path A which is repeatedly bent left and right or the first flow path A which is spirally extended.
  • the invention When the invention is used, it is connected to the air inlet of the combustion device, for example, the air inlet of the engine.
  • the use mode of the present invention is used alone, and the engine 30 is provided with an air inlet 301.
  • the end of the intake hose 301 is connected to one end of the intake hose 31, and the other end of the intake hose 31 is fitted to the output pipe 162 of the casing 10 of the present invention, so that the installation is completed, and the installation process is very easy.
  • FIG. 6 a plurality of uses of the present invention are used.
  • the present invention When the present invention is applied to an engine 30 having a plurality of intake ports 301, such as the engine 30 of a ship, the plurality of intake ports 301 can pass through multiple The intake hoses 31 connect a plurality of outlet tubes 162 of the present invention such that each of the inlets 301 of the engine 30 can benefit from the increased pressure of the input air by the present invention.
  • the inside and each of the intake ports 301 generate a negative pressure and an attractive force due to the operation of the engine 30, so that the present invention connected to each of the intake hoses 31 can be
  • the plurality of air holes 151 of the rear cover 15 attract air.
  • the air in the environment will be from the rear end of the first flow path A and the second flow path D. The rear ends are respectively attracted into the inside of the casing 10.
  • the air that is drawn into the first flow path A that is repeatedly bent and extended by the environment is attracted by the plurality of guide pieces 13 because the flow path is longer than the second flow path D, and the flow rate is slowed down, plus the flow
  • the time travels along the curved first flow path A, so that the air flow of the final slowing speed will flow into the air chamber B from the side of the air chamber B, and gradually accelerates along the inner circumferential surface of the tapered portion 1611, and then
  • the moving manner of the spiral flows out to the output flow path c of the output pipe 162; in contrast, the air flowing into the second flow path D of the air intake member 20 from the environment is the fastest because the flow path is the shortest and there is no obstruction in the middle.
  • the speed flows forward to the front end of the second flow path D, and is ejected toward the middle of the output flow path c inside the output pipe 162.
  • the central output tube is made by the difference in speed between the two and the difference in flow direction.
  • the direct injection airflow in 162 can be mutually drawn with the surrounding spiral moving airflow, and a vortex is formed between the airflow directly flowing in the center and the surrounding airflow, so that the air flowing forward in the air chamber B is not only the width of the air.
  • the gradually decreasing tapered section 1611 can achieve the effect of forward acceleration by means of a nozzle, and can further utilize the eddy current between the airflows to enhance the pressure and speed of the air outputted from the output flow passage c of the output pipe 162, so that the connection is
  • the fuel in the engine 30 of the invention can increase the intake efficiency of the intake port 301 due to the formation of a low pressure region inside the intake port 301, so that the fuel in the engine 30 can be completely burned, the fuel consumption is reduced, the horsepower of the engine 30 is enhanced, and the engine 30 is reduced. Ignition device carbon deposits and the generation of air pollutants.
  • the intake hose 31 shown in FIGS. 4 and 6 may be connected to the intake port 301 in a completely covered manner, and the intake hose 31 may be inserted into the intake air with a gap therebetween.
  • the engine 30 is provided with an air inlet 301.
  • An air inlet hose 31 is connected to the output pipe 162 of the casing 10 of the present invention.
  • the air inlet hose 31 is inserted into one end of the air inlet 301. There is a gap between the intake hose 31 and the intake port 301 in the port 301.
  • the negative pressure formed inside the intake port 301 will be the air around the outer side of the intake port 301 from the intake hose 31 and the output.
  • the gap between the tubes 162 is drawn into the air inlet 301, further increasing the amount of air input into the air inlet 301, further improving the efficiency of fuel combustion in the combustion device such as the engine 30, enhancing the horsepower of the engine 30 and reducing the carbon deposit of the ignition device. And the generation of air pollutants.
  • a second preferred embodiment of the present invention is to change the shape of the through opening 163 of the outer casing 10 and the structure of the air inlet member 20 in the first preferred embodiment, and the remaining configurations are the first preferred embodiment described above. The same is true in the examples.
  • a circular opening 163 is formed in the tapered portion 1611 of the front cover 16, corresponding to the periphery of the outer end of the opening 163.
  • a non-circular recess 1631 is recessed in the outer surface of the cover portion 161.
  • the recess 1631 is a rectangular slot in the preferred embodiment.
  • the through hole 163 extends through the center of the recess 1631.
  • the air intake member 20 of the second preferred embodiment is provided with a hook-shaped air pipe 23, and the air pipe 23 is located in the air chamber B.
  • the front end of the air pipe 23 is located behind the output flow path c, and the air pipe 23 is The front end faces the center of the output flow path c, the rear end of the air tube 23 passes through the opening 163, and a portion of the air tube 23 that passes outwardly through the opening 163 forms a flared expansion portion 24,
  • the shape of the slot 1631 should be formed, and a rectangular panel 25 is formed around the air tube 23, and the panel 25 is embedded and fixed in the recess 1631 to allow the air inlet member 20 to be fixed thereto.
  • the width of the front end of the second flow path D is narrower than the width dimension of the rear end of the output flow path c, and the front end of the second flow path D faces the output
  • the rear end of the flow path c is in the center of the output flow path c; the rear end of the second flow path D is located in the front cover 16 of the outer casing 10.
  • the length of the second flow path D is shorter than the length of the first flow path A.
  • the length of the second flow path D is shorter than the length.
  • the first flow path A extends half or even a quarter of the length. Since the rest of the configuration of the second preferred embodiment is the same as that described in the first preferred embodiment described above, the present invention is not described herein.
  • the air taken in by the rear end of the first flow path A advances in a path that is repeatedly curved left and right, since the path of the first flow path A is longer than the second flow path D. And a plurality of guide pieces 13 are obstructed, so the speed of the air flowing in the first flow path A is slower than the speed of the air flowing through the second flow path D. Since the velocity of the air ejected from the front end of the second flow path D is faster than the speed of the forward spiral around the air chamber B, the speed difference between the fast and the slow and the difference in the flow direction are in the second flow.
  • a vortex is generated between the airflow jetted from the front end of the tunnel D and the airflow flowing forwardly around the air chamber B, so that the air flowing forward in the air chamber B can be further utilized in addition to being accelerated forward due to the shape of the nozzle of the front cover 16.
  • the eddy current between the air flows enhances the pressure and velocity of the output air flow c.
  • a third preferred embodiment of the present invention is to change the shape of the front cover 16 of the outer casing 10 in the first and second preferred embodiments, and the shape of the air intake member 20, and the remaining configurations are the same as the above 1. The same as described in the second preferred embodiment.
  • the front cover 16 is provided with a cover portion 161 which is a cover body and is fastened to the outer tube at the rear side.
  • the left and right widths of the inner wall of the rear side of the cover portion 161 are larger than the left and right widths around the front end of the outer tube 11, and when the cover portion 161 is sleeved and fixed to the front end of the outer tube 11, the cover is Two through holes 163 are formed between the left and right sides of the portion 161 and the left and right sides of the front end of the outer tube 11. The remaining portion of the rear side of the cover portion 161 is fixed to the front and rear sides of the front end of the outer tube 11.
  • the front side of the cover portion 161 forms a tapered portion 1611 whose shape gradually narrows toward the front, and an output tube 162 is formed in the middle of the tapered portion 1611.
  • the output tube 162 is a straight tube and has a width smaller than the width.
  • the width of the outer tube 11 is such that a plenum B is formed in the cover portion 161, and the front side of the plenum B is gradually narrowed from the rear to the front, and the front end of the first flow passage A and the rear end of the air chamber B are Sideways communicate, and an output flow path c is formed in the output pipe 162.
  • the output flow path c is a circular linear passage and communicates with the front end of the gas chamber B.
  • the air inlet member 20 is disposed in the air chamber B.
  • the air inlet member 20 is provided with a jet tube 26 disposed in the air chamber B and located behind the output flow path c.
  • the rear end of the air tube 26 is connected to the two bifurcated side tubes 27, and the rear ends of the two side tubes 27 are closely spaced and fixed at the two through openings 163, and a gas tube 26 and two side tubes 27 of the air inlet member 20 are formed.
  • Second flow path D the width dimension of the front end of the second flow path D Narrower than the width dimension of the rear end of the output flow path c, and the front end of the second flow path D faces the rear end of the output flow path c, facing the center of the output flow path c, the rear end of the second flow path D Dividing into two places on the left and right sides and opening outside the front cover 16 of the outer casing 10, communicating with the environment around the outer casing 10, the length of the left and right sides of the second flow path D is shorter than the length of the first flow path A.
  • the second flow path D extends for a length shorter than half or even a quarter of the length of the first flow path A. Since the rest of the configuration of the third preferred embodiment is the same as that described in the first and second preferred embodiments, the present invention is not limited thereto.
  • the same in addition to the two openings 163 formed between the left and right sides of the cover portion 161 of the front cover 16 and the left and right sides of the front end of the outer tube 11, the same may be used.
  • the shape of the cover portion is such that one side of the inner wall has a gap with the opposite side of the front end of the outer tube 11, and only a gap is formed between one side of the cover portion 161 and the opposite side of the front end of the outer tube 11. 163.
  • the gas injection pipe 26 of the gas inlet member 20 is only connected backward to a side pipe 27 extending rearwardly toward the opening 163.
  • the rear end of the side pipe 27 is fixedly disposed at the opening 163 to make the gas pipe. 26.
  • the rear end opening of the second flow path D formed in the side tube 27 is outside the front cover 16 of the outer casing 10 and communicates with the surrounding environment.
  • the air taken in by the rear end of the first flow path A advances in a path that is repeatedly curved left and right, since the path of the first flow path A is smaller than the second flow.
  • the track D is long and has a plurality of guide pieces 13 blocked, so the speed of the air flowing in the first flow path A is slower than the speed of the air flowing through the second flow path D.
  • air around the outer casing 10 enters the air intake member 20 from both rear ends of the second flow path D, and is then ejected toward the center of the output flow path c by the air injection tube 26, since the front end of the second flow path D
  • the velocity of the ejected air is faster than the velocity of the air accelerated by the forward spiral around the chamber B, and the airflow ejected at the front end of the second flow passage D and the periphery of the air chamber B by the difference in speed between the two and the difference in the flow direction
  • the eddy current is generated between the airflows flowing forwardly, so that the air flowing forward in the air chamber B can be further accelerated by the eddy current between the airflows in addition to the forward movement of the nozzles of the front cover 16, and the output flow path c is enhanced. Air pressure and speed.
  • the manner of attracting air in the environment into the first flow path A and the second flow path D is a negative pressure when the engine 30 operates.
  • the generated attraction attracts air and is a means of natural intake.
  • it can also be selected at the rear end of the first flow path A and the second flow path D, or the first flow path A and the second flow path D.
  • the rear end of the first unit is connected to the active intake device to force the intake air to increase the pressure of the air entering the engine 30.
  • the fourth embodiment of the present invention as shown in FIG. 14 is a means for adding a forced air intake in the configuration of the first preferred embodiment, and is coupled to the rear end of the rear cover 15 of the outer casing 10 as an active feed.
  • the rear end fan air intake structure 40 of the air means, and the outer tube 32 is connected to the tube portion 22 of the air inlet member 20 as described in the first preferred embodiment, and the external connection tube 32 is connected as an active air intake means.
  • Lateral fan intake configuration 41 The rest of the configuration of the fourth preferred embodiment of the present invention is the same as that described in the first preferred embodiment, and the present invention is not described herein.
  • the output flow path c is connected to the engine 30, and then the rear end fan intake structure 40 and the lateral fan intake structure 41 are respectively activated to surround the ambient air.
  • the suction is blown into the rear end of the first flow path A and the rear end of the second flow path D, so that the air ejected from the front end of the second flow path D and the air ejected from the front end of the first flow path A are collected in the air chamber B, by two
  • the difference in speed and the difference in flow direction generate eddy currents, so that the air flowing forward in the air chamber B can be further accelerated by the eddy current in addition to the pressurized air and the shape of the nozzle of the front cover 16, and the output flow path can be further enhanced.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
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  • Jet Pumps And Other Pumps (AREA)

Abstract

An air booster. A first flow channel (A), an air chamber (B), and an output flow channel (C) are formed inside a housing (10) in a successive manner. The first flow channel (A) is a channel extending crookedly. The air chamber (B) is a conical space. An air inlet part (20) penetrates the housing (10). A second flow channel (D) having a length shorter than that of the first flow channel (A) is formed in the air inlet part (20). A front end of the second flow channel (D) faces towards the output flow channel (C). When the output flow channel (C) is connected to a combustion device, for example, an air inlet (301) of an engine (30), the negative pressure generated during operating of the combustion device may cause the first flow channel (A) and the second flow channel (D) to take in air from surroundings. An airflow entering the air chamber (B) from the second flow channel (D) and an airflow entering the air chamber (B) from the first flow channel (A) pull each other to form a vortex flow, such that the speed and pressure of air can be increased when entering the combustion device, fuel in the combustion device is completely combusted, and the combustion efficiency of the combustion device is improved to reduce fuel consumption, promote output power, and reduce pollution by avoiding emission of black smoke caused by incomplete combustion.

Description

空气增力器Air booster 技术领域Technical field
本发明涉及一种增进燃烧装置运作效能的装置,尤其涉及一种能提升燃烧装置进气效率进而增进其燃烧与运作效率的空气增力器。The invention relates to a device for improving the operating efficiency of a combustion device, in particular to an air booster capable of improving the intake efficiency of a combustion device and thereby improving its combustion and operation efficiency.
背景技术Background technique
一般汽车、机车、船舶或割草机是使用内燃机例如往复式引擎作为动力的来源,此种引擎运作的方式,是在引擎的汽缸内混合空气和燃料后,进行进气、压缩、爆炸、排气等四个程序,进而产生动力的输出。A typical automobile, locomotive, ship or lawn mower is a source of power using an internal combustion engine such as a reciprocating engine. The engine operates by mixing air and fuel in the cylinders of the engine for intake, compression, explosion, and exhaust. Four programs, such as gas, produce a power output.
上述现有的引擎运作时,在引擎汽缸内爆炸的燃料和空气比例,即油气比是影响引擎运作的重要参数,良好的油气比有利于燃油完全的燃烧,可增强引擎输出的马力,同时减少废气的排放。When the above-mentioned existing engine is in operation, the ratio of fuel to air exploded in the engine cylinder, that is, the oil-gas ratio is an important parameter affecting the operation of the engine. A good oil-gas ratio is beneficial to the complete combustion of the fuel, which can enhance the horsepower of the engine output while reducing Exhaust gas emissions.
但空气由引擎的进气口进入至汽缸燃烧的过程中,会经过进气管路、节气门、进气歧管、燃烧室汽门等层层阻碍,且这些引擎进气过程中的阻碍若结构老化也会进一步削减空气进入汽缸的量。如此一来,会使引擎内的燃油燃烧不完全,增加油耗且造成引擎的马力降低,而燃烧不完全也增加引擎排气的空气污染物并使点火装置产生积碳产生恶性循环。However, when air enters the combustion of the cylinder from the intake port of the engine, it will be hindered by the intake pipe, the throttle valve, the intake manifold, the combustion chamber valve, etc., and the obstacles in the intake process of these engines are Aging also further reduces the amount of air entering the cylinder. As a result, the fuel in the engine is not completely burned, the fuel consumption is increased and the horsepower of the engine is lowered, and the incomplete combustion also increases the air pollutants of the engine exhaust gas and causes carbon deposits in the ignition device to generate a vicious circle.
为了弥补这个缺憾,使燃烧装置例如引擎的燃烧效率提升以回复原有的动力,现有技术有使用涡轮增压器对引擎强制进气,解决前述的引擎燃烧不完全的问题。利用涡轮增压器虽能大幅提升引擎输出的马力,但齿轮组与排气涡轮等相当笨重与耗能,随之而来的油料损耗也会明显增加,因此不符合一般使用者只需要使引擎内的燃油燃烧更完全的需求,此外,涡轮增压器这种主动进气的装置在使用时需要对引擎进行复杂的改装,使用的技术层次较高,使用者无法由商店自行买回安装,运用上不容易使用。In order to make up for this shortcoming, the combustion efficiency of the combustion device such as the engine is increased to restore the original power. The prior art uses a turbocharger to force the intake of the engine to solve the aforementioned problem of incomplete combustion of the engine. Although the turbocharger can greatly increase the horsepower of the engine output, but the gear set and the exhaust turbine are quite cumbersome and energy-consuming, and the consequent oil loss will also increase significantly, so it is not in line with the average user only need to make the engine The fuel combustion inside is more complete. In addition, the turbocharger, which is used for active intake, requires complex modifications to the engine. The technical level of use is high and the user cannot buy it back by the store. It is not easy to use.
发明内容Summary of the invention
由于现有的燃烧装置例如引擎缺乏容易安装的进气加压手段,因而有无法提升引擎运作效率的缺点。为此,本发明以第一流道、第二流道具有不同 速度、方向气流汇流的方式形成涡流,与使用喷嘴构型以得到加速喷流,使装置输出的空气增力,于进气口内部形成低压区,进而增进进气口的进气效率,达到提升引擎输入空气压力并增进其燃烧效率与降低排气污染的功效。Since existing combustion devices such as engines lack an air pressure pressurizing means that is easy to install, there is a disadvantage that the efficiency of the engine operation cannot be improved. To this end, the present invention has different first and second flow paths. The vortex is formed by the way of velocity and direction airflow, and the nozzle configuration is used to obtain the accelerated jet flow, so that the air outputted by the device is increased, and a low pressure zone is formed inside the air inlet port, thereby improving the intake efficiency of the air inlet and improving The engine inputs air pressure and increases its combustion efficiency and reduces exhaust pollution.
为达到上述目的,本发明提供一种空气增力器,包括一外壳以及一穿置在该外壳的进气件,其中:To achieve the above object, the present invention provides an air booster comprising an outer casing and an air intake member disposed in the outer casing, wherein:
该外壳是直管状的壳体并且在前端设有一输出管,该输出管的宽度尺寸小于该外壳的其余部分的宽度尺寸,在该外壳的内部由后向前相连形成一第一流道、一气室以及一输出流道,该第一流道是由后朝前弯曲延伸的通道,该第一流道的前端与该气室后端的侧旁相通,该气室是空间且前侧由后向前逐渐收窄,该输出流道形成在该输出管内,该输出流道是直线的通道并连接在该气室的前端,在该外壳设有该输出管以外的周围部分形成一穿口;The outer casing is a straight tubular casing and is provided at the front end with an output pipe having a width dimension smaller than a width dimension of the remaining portion of the outer casing, and a first flow passage and a gas chamber are formed in the interior of the outer casing from the rear to the front. And an output flow passage, the first flow passage is a passage extending from the rear to the front, the front end of the first flow passage communicates with the side of the rear end of the air chamber, the air chamber is a space and the front side is gradually received from the rear to the front. Narrow, the output flow channel is formed in the output tube, the output flow channel is a straight channel and is connected to the front end of the air chamber, and a peripheral portion of the outer casing provided with the output tube forms a through hole;
该进气件是管体并穿置在该穿口,该进气件的前端位于该气室内并朝向该输出流道的后端,在该进气件的内部形成一第二流道,该第二流道延伸的长度短于该第一流道延伸的长度,该第二流道的前端较该输出流道窄而朝向该输出流道的中央,该第二流道的后端位于该外壳之外,与该外壳外部周围的环境相通。The air inlet member is a tubular body and is disposed at the through hole. The front end of the air inlet member is located in the air chamber and faces the rear end of the output flow channel, and a second flow path is formed inside the air inlet member. The length of the second flow path extending is shorter than the length of the first flow path, the front end of the second flow path is narrower than the output flow path toward the center of the output flow path, and the rear end of the second flow path is located in the outer casing In addition, it communicates with the environment around the outside of the enclosure.
进一步,本发明所述穿口形成在所述外壳对应内部设有所述气室处。Further, the opening of the present invention is formed at a position corresponding to the inside of the outer casing.
更进一步,本发明所述外壳包括一外管以及一结合在该外管的前盖,该外管是竖直设置的直管体且上、下相反的两端分为前、后端,所述的第一流道形成在该外管内,且该第一流道在该外管的前、后两端形成开口;该前盖设有一套盖部,该套盖部是盖体并且套合固定在该外管的前端,该套盖部的前侧形成形状逐渐朝前收窄的渐缩段,所述输出管是由该渐缩段的中间朝前伸设形成,所述气室形成在该套盖部内,所述穿口形成在该套盖部的周围,所述第二流道延伸的长度短于该第一流道延伸长度的一半。Further, the outer casing of the present invention comprises an outer tube and a front cover coupled to the outer tube, the outer tube is a vertically arranged straight tube body and the upper and lower opposite ends are divided into a front end and a rear end. The first flow passage is formed in the outer tube, and the first flow passage forms an opening at the front and rear ends of the outer tube; the front cover is provided with a cover portion which is a cover body and is sleeved and fixed a front end of the outer tube, a front side of the cover portion forming a tapered portion whose shape gradually narrows toward the front, the output tube being formed by extending from the middle of the tapered portion, wherein the air chamber is formed In the cover portion, the through opening is formed around the cover portion, and the second flow path extends for a length shorter than half of the extension length of the first flow path.
较佳的,本发明所述套盖部紧密套合在所述外管的前端,所述穿口穿设在该套盖部的渐缩段;所述进气件设有一块状部以及一与该块状部相连的管部,该块状部位于所述的气室内且外端伸抵所述的输出流道的后方,该管部穿置在该穿口,且该块状部接邻该管部的一侧抵靠并粘合在该渐缩段的内面,所述第二流道形成在该块状部与该管部内,该第二流道延伸的长度短于所述的第一流道延伸长度的四分之一。 Preferably, the cover portion of the present invention is tightly fitted to the front end of the outer tube, and the through hole is formed in a tapered portion of the cover portion; the air inlet member is provided with a block portion and a a tube portion connected to the block portion, the block portion is located in the air chamber and the outer end extends to the rear of the output flow channel, the tube portion is disposed at the through hole, and the block portion is connected a side adjacent to the tube portion abuts and adheres to an inner surface of the tapered portion, the second flow passage is formed in the block portion and the tube portion, and the second flow passage extends a length shorter than the The first runner extends for a quarter of the length.
较佳的,本发明所述套盖部紧密套合在所述外管的前端,所述穿口穿设在该套盖部的渐缩段,对应该穿口外端的周缘,在该套盖部的外表面凹入形成一非圆形的嵌槽,该穿口贯穿该嵌槽的中央;所述进气件设有一勾状的气管,该气管位于所述的气室内且前端位于所述的输出流道的后方,该气管的后端穿置在该穿口,在该气管向外穿出该穿口的部分形成一喇叭形状的扩张部,配合该嵌槽的形状,在该气管的周围形成一嵌板,该嵌板嵌设并粘合固定在该嵌槽内,所述第二流道形成在该气管内,该第二流道延伸的长度短于所述的第一流道延伸长度的四分之一。Preferably, the cover portion of the present invention is tightly fitted to the front end of the outer tube, and the through hole is formed in the tapered portion of the cover portion, corresponding to the peripheral edge of the outer end of the opening, in the cover portion The outer surface is recessed to form a non-circular recess, the through hole extends through the center of the recess; the air inlet member is provided with a hook-shaped air tube, the air tube is located in the air chamber and the front end is located at the Behind the output flow path, the rear end of the air pipe is disposed at the opening, and a portion of the air pipe that passes outwardly through the opening forms a flared expansion portion, and the shape of the groove is matched around the air pipe Forming a panel, the panel is embedded and adhesively fixed in the recess, the second flow channel is formed in the air tube, and the second flow channel extends for a length shorter than the first flow path extension length One quarter of the.
较佳的,本发明所述套盖部内壁的相反两侧各与所述外管前端周围的相对侧之间有间隙,所述的穿口形成在该套盖部内壁的一侧与该外管前端周围的相对侧之间,并在该套盖部的另一侧与该外管前端的相对侧之间形成另一穿口;所述的进气件设有一喷气管,该喷气管位于所述的气室内并位于所述的输出流道的后方,在该喷气管的后端连接两分叉的侧管,两侧管的后端紧密穿置在两穿口处固定,所述第二流道形成在该喷气管以及两侧管内,该第二流道延伸的长度短于所述第一流道延伸长度的四分之一。Preferably, there is a gap between opposite sides of the inner wall of the cover portion of the present invention and an opposite side of the front end of the outer tube, and the through hole is formed on one side of the inner wall of the cover portion and the outer portion. Between the opposite sides of the front end of the tube, and another opening between the other side of the cover portion and the opposite side of the front end of the outer tube; the air inlet member is provided with a jet tube, the air tube is located The gas chamber is located behind the output flow channel, and a bifurcated side tube is connected at a rear end of the gas injection tube, and a rear end of the two side tubes is closely worn at two openings, the first A second flow passage is formed in the lance tube and the side tubes, and the second flow passage extends for a length shorter than a quarter of the length of the first flow passage.
进一步,本发明所述的外管是矩形直管体,在该外管内以上、下间隔的排列方式结合多个矩形的导引片,由前至后数来为奇数序列的各导引片,其右端缘连接在该外管右侧的内壁且左端缘朝左并朝后斜向延伸,奇数序列的各导引片的左端缘与该外管左侧的内壁之间有间隙;由前至后数来为偶数序列的各导引片,其左端缘连接在该外管左侧的内壁且右端缘朝右并朝后斜向延伸,偶数序列的各导引片的右端缘与该外管右侧的内壁之间有间隙;所述的第一流道是该外管内的空间被多个导引片分隔而成。Further, the outer tube of the present invention is a rectangular straight tube body, and the upper and lower spaced arrangement of the outer tube combines a plurality of rectangular guiding pieces, and the leading pieces of the odd sequence are from front to back. The right end edge thereof is connected to the inner wall of the right side of the outer tube and the left end edge is inclined to the left and obliquely backward, and there is a gap between the left end edge of each of the odd-numbered guide pieces and the inner wall of the left side of the outer tube; Each of the guide pieces having the even number of even numbers has a left end edge connected to the inner wall of the left side of the outer tube and a right end edge extending rightward and obliquely rearward, and the right end edge of each of the even-numbered guide pieces and the outer tube There is a gap between the inner walls of the right side; the first flow path is that the space inside the outer tube is divided by a plurality of guiding pieces.
更进一步,本发明所述外管是左、右两半壳体相对组合而成的矩形直管体,所述的外壳进一步包括一后盖,该后盖是盖体并且紧密套合固定在该外管11后端的周围,在该后盖的后面穿设多个气孔。Furthermore, the outer tube of the present invention is a rectangular straight tube body in which the left and right halves are oppositely combined, and the outer casing further includes a rear cover which is a cover body and is tightly fitted and fixed thereto. A plurality of air holes are bored around the rear end of the outer tube 11 around the rear end of the outer tube 11.
较佳的,本发明在所述外壳的后端结合一后端风扇进气构造。Preferably, the present invention incorporates a rear end fan intake configuration at the rear end of the housing.
较佳的,本发明在所述的进气件的外端连接一外接管,以该外接管连接一侧向风扇进气构造。Preferably, the present invention connects an external pipe at the outer end of the air intake member, and the outer pipe connects the side to the fan air intake structure.
本发明使用时,是以输出管通过进气软管接向燃烧装置例如引擎的进气口。当燃烧装置运作时,燃烧装置内部与进气口处产生的负压会由输出管处 开始吸引气流,这时环境中的空气会分别由第一流道的后端以及第二流道的后端,分别由该外壳的后端以及该外壳周围的环境吸气,使外界的空气经由两不同的通道进入该外壳内的气室汇集。The invention is used in that the outlet tube is connected to the inlet of the combustion device, such as an engine, through an intake hose. When the combustion device is operated, the negative pressure generated inside the combustion device and the inlet will be from the output pipe. Starting to attract the airflow, the air in the environment will be respectively taken from the rear end of the first flow channel and the rear end of the second flow channel, respectively, by the rear end of the outer casing and the environment around the outer casing, so that the outside air passes through the two Different channels enter the air chamber collection within the enclosure.
当空气流入第一流道时,由于气流移动的路径较第二流道的路径长,使得第一流道内与第二流道内流动的气流速度有差异,加上两流道的气流方向不同,使第二流道向输出流道的中央直喷的气流能与气室周围气流互相牵引,在气室内形成加压的涡流,而气室逐渐向前缩减的空间能将气室逐渐汇入输出流道的气流加速,使气室内向前流动的空气除了利用逐渐缩减的空间进行加速以外,还能利用涡流加压,增强输出管的输出流道输出空气的压力与速度,在燃烧装置的进气口内部形成低压区,进而增进进气口的进气效率。When the air flows into the first flow path, since the path of the air flow movement is longer than the path of the second flow path, the air flow speed in the first flow path and the second flow path are different, and the air flow directions of the two flow paths are different, so that The flow of the direct flow from the second flow path to the center of the output flow path can be mutually drawn with the air flow around the air chamber, and a pressurized vortex is formed in the air chamber, and the space gradually reduced by the air chamber can gradually merge the air chamber into the output flow path. The airflow is accelerated, so that the air flowing forward in the gas chamber can be accelerated by the gradually reduced space, and the vortex pressure can be used to enhance the pressure and speed of the output air output of the output pipe, at the air inlet of the combustion device. A low pressure zone is formed inside to further improve the intake efficiency of the intake port.
本发明的功效在于,藉由输出加压空气的方式,使连接本发明的燃烧装置例如引擎内的燃油尽可能完整燃烧,增强引擎的马力,减少引擎积碳以及排放空气污染物的产生。此外,本发明安装容易,让使用人购买后可自行安装使用,方便使用者利用。The effect of the present invention is that the combustion fuel connected to the combustion apparatus of the present invention, such as the engine, is burned as completely as possible by the output of pressurized air, enhancing the horsepower of the engine, reducing engine carbon deposits and generating air pollutants. In addition, the invention is easy to install, and can be installed and used by the user after purchase, which is convenient for the user to use.
附图说明DRAWINGS
图1是本发明第一较佳实施例的立体图;Figure 1 is a perspective view of a first preferred embodiment of the present invention;
图2是本发明第一较佳实施例的分解图;Figure 2 is an exploded view of the first preferred embodiment of the present invention;
图3是本发明第一较佳实施例的剖面图;Figure 3 is a cross-sectional view showing a first preferred embodiment of the present invention;
图4是本发明第一较佳实施例的实施示意图;Figure 4 is a schematic view showing the implementation of the first preferred embodiment of the present invention;
图5是本发明第一较佳实施例的气流导向示意图;Figure 5 is a schematic view of airflow guiding according to a first preferred embodiment of the present invention;
图6是本发明第一较佳实施例的另一实施示意图;Figure 6 is a schematic view showing another embodiment of the first preferred embodiment of the present invention;
图7是本发明第一较佳实施例的再一实施示意图;Figure 7 is a schematic view showing still another embodiment of the first preferred embodiment of the present invention;
图8是本发明第二较佳实施例的实施示意图;Figure 8 is a schematic view showing the implementation of a second preferred embodiment of the present invention;
图9是本发明第二较佳实施例的分解图;Figure 9 is an exploded view of a second preferred embodiment of the present invention;
图10是本发明第二较佳实施例的剖面图;Figure 10 is a cross-sectional view showing a second preferred embodiment of the present invention;
图11是本发明第三较佳实施例的分解图;Figure 11 is an exploded view of a third preferred embodiment of the present invention;
图12是本发明第三较佳实施例纵向的剖面图;Figure 12 is a longitudinal sectional view showing a third preferred embodiment of the present invention;
图13是本发明第三较佳实施例横向的剖面图;Figure 13 is a transverse cross-sectional view showing a third preferred embodiment of the present invention;
图14是本发明第四较佳实施例的部分剖面示意图。 Figure 14 is a partial cross-sectional view showing a fourth preferred embodiment of the present invention.
附图标记说明:Description of the reference signs:
10外壳                     11外管10 outer casing 11 outer tube
12倒角形状                 13导引片12 chamfer shape 13 guide piece
15后盖                     151气孔15 back cover 151 air holes
16前盖                     161套盖部16 front cover 161 sets of cover
1611渐缩段                 162输出管1611 tapered section 162 output tube
163穿口                    1631嵌槽163 piercing 1631 slot
20进气件                   21块状部20 air intake parts 21 block parts
22管部                     23气管22 tube parts 23 trachea
24扩张部                   25嵌板24 expansion section 25 panel
26喷气管                   27侧管26 jet tube 27 side tube
30引擎                     301进气口30 engine 301 air inlet
31进气软管                 32外接管31 intake hose 32 external adapter
40后端风扇进气构造         41侧向风扇进气构造40 rear fan inlet structure 41 lateral fan intake structure
A第一流道                  B气室A first flow channel B gas chamber
c输出流道                  D第二流道c output flow channel D second flow channel
具体实施方式detailed description
为能详细了解本发明的技术特征及实用功效,并可依照说明书的内容来实施,进一步以如图式所示的较佳实施例,详细说明如下。In order to understand the technical features and practical effects of the present invention in detail, it can be implemented in accordance with the contents of the specification, and further described in detail with reference to the preferred embodiments shown in the drawings.
请参看图1至图3所示的本发明第一较佳实施例,其构造包括一外壳10以及一穿置结合在该外壳10的进气件20,其中:Referring to the first preferred embodiment of the present invention shown in FIGS. 1 through 3, the construction includes a housing 10 and an air inlet member 20 that is coupled to the housing 10, wherein:
该外壳10包括一外管11、一结合在该外管11后端的后盖15,以及一结合在该外管11前端的前盖16。该外管11是竖直且由左、右两半壳体相对组合而成的矩形直管体,该外管11上下相反方向的两端分为前后与后端,在该外管11周围的四个角落分别形成一倒角形状12,在该外管11内以上、下间隔的排列方式结合多个矩形的导引片13。The outer casing 10 includes an outer tube 11, a rear cover 15 coupled to the rear end of the outer tube 11, and a front cover 16 coupled to the front end of the outer tube 11. The outer tube 11 is a rectangular straight tube body which is vertically and partially combined with the left and right halves of the housing. The two ends of the outer tube 11 are divided into front and rear and rear ends, and the outer tube 11 is surrounded by the outer tube 11 The four corners respectively form a chamfered shape 12, and the upper and lower spaced arrangement of the outer tube 11 combines a plurality of rectangular guide pieces 13.
由前至后数来为奇数序列的各导引片13,其右端缘连接在外管11右侧的内壁且左端缘朝左并朝后斜向延伸,奇数序列的各导引片13的左端缘与该外管11左侧的内壁之间有间隙,奇数序列各导引片13的其余两侧端缘与该外管 11的对应内壁连接;由前至后数来为偶数序列的各导引片13,其左端缘连接在外管11左侧的内壁且右端缘朝右并朝后斜向延伸,偶数序列的各导引片13的右端缘与该外管11右侧的内壁之间有间隙,偶数序列各导引片13的其余两侧端缘与该外管11的对应内壁连接;该外管71内的空间被多个导引片13分隔成一由后往前左右反复弯曲延伸的第一流道A,该第一流道A在该外管11的前、后两端形成开口。Each of the guide pieces 13 of the odd-numbered sequence from the front to the rear has a right end edge connected to the inner wall of the right side of the outer tube 11 and a left end edge extending leftward and obliquely rearward, and the left end edge of each of the odd-numbered guide pieces 13 There is a gap between the inner wall of the left side of the outer tube 11 and the remaining two side edges of the odd-numbered series of guiding pieces 13 and the outer tube Corresponding inner wall connection of 11; each guide piece 13 having an even sequence from front to back, the left end edge of which is connected to the inner wall of the left side of the outer tube 11 and the right end edge is rightward and obliquely extended rearward, and the guides of the even sequence There is a gap between the right end edge of the lead piece 13 and the inner wall of the right side of the outer tube 11, and the remaining two side edges of the even-numbered guide pieces 13 are connected to the corresponding inner wall of the outer tube 11; the space inside the outer tube 71 The plurality of guiding pieces 13 are divided into a first flow path A which is repeatedly bent and extended from the front to the front and the left and right, and the first flow path A forms an opening at the front and rear ends of the outer tube 11.
该后盖15是盖体并且以前侧紧密套合固定在该外管11后端的周围,在该后盖15的后面穿设多个气孔151。该前盖16设有一套盖部161,该套盖部161是盖体并且以后侧紧密套合固定在该外管11前端的周围,该套盖部161的前侧形成形状逐渐朝前收窄的渐缩段1611,在该渐缩段1611的中间朝前伸设一输出管162,该输出管162是直管且宽度尺寸小于该外管11的宽度尺寸,在该套盖部161内形成一气室B,该气室B是空间且前侧由后向前逐渐收窄,该第一流道A的前端与该气室B后端的侧旁相通,在该输出管162内形成一输出流道c,该输出流道c是圆型的直线通道且与该气室B的前端相通,在该套盖部161的渐缩段1611的周围穿设一穿口163。The rear cover 15 is a cover body and the front side is tightly fitted around the rear end of the outer tube 11 , and a plurality of air holes 151 are bored in the rear surface of the rear cover 15 . The front cover 16 is provided with a cover portion 161. The cover portion 161 is a cover body and the rear side is tightly fitted around the front end of the outer tube 11. The front side of the cover portion 161 is gradually tapered toward the front. The tapered portion 1611 defines an output tube 162 extending forwardly of the tapered portion 1611. The output tube 162 is a straight tube and has a width smaller than a width dimension of the outer tube 11 and is formed in the cover portion 161. An air chamber B, the air chamber B is a space and the front side is gradually narrowed from the rear to the front. The front end of the first flow path A communicates with the side of the rear end of the air chamber B, and an output flow path is formed in the output tube 162. c. The output flow path c is a circular linear passage and communicates with the front end of the air chamber B. A through opening 163 is bored around the tapered portion 1611 of the cover portion 161.
该进气件20设有一块状部21以及一与该块状部21相连的管部22,该进气件20的块状部21位于该气室B内,该块状部21的外端伸抵该输出流道c的后方,该进气件20以该管部22穿置固定在该前盖16的穿口163,该块状部21接邻该管部22的一侧抵靠并粘合在该渐缩段1611的内面,在该块状部21与该管部22内形成一第二流道D,该第二流道D前端的宽度尺寸窄于该输出流道c后端的宽度尺寸,且该第二流道D的前端朝向该输出流道c的后端,正对该输出流道c的中央,该第二流道D的后端位于该外壳10的前盖16之外,与该外壳10外部周围的环境相通,且该第二流道D延伸的长度短于该第一流道A延伸的长度,较佳的,该第二流道D延伸的长度短于该第一流道A延伸长度的一半甚至四分之一。The air inlet member 20 is provided with a block portion 21 and a tube portion 22 connected to the block portion 21. The block portion 21 of the air inlet member 20 is located in the air chamber B, and the outer end of the block portion 21 Extending the rear of the output flow path c, the air inlet member 20 is inserted and fixed to the opening 163 of the front cover 16 by the tube portion 22, and the block portion 21 abuts against the side of the tube portion 22 and Adhered to the inner surface of the tapered portion 1611, a second flow path D is formed in the block portion 21 and the tube portion 22. The width of the front end of the second flow path D is narrower than the rear end of the output flow path c. a width dimension, and a front end of the second flow path D faces the rear end of the output flow path c, facing the center of the output flow path c, and a rear end of the second flow path D is located at the front cover 16 of the outer casing 10. The length of the second flow path D is shorter than the length of the first flow path A. Preferably, the length of the second flow path D is shorter than the length of the first flow path A. The first-class road A extends half or even a quarter of its length.
本较佳实施例所述的外管11,除上述第一较佳实施例是设为矩形直管体以外,也可以将所述的外管11设为圆形直管体的形状,这时套盖结合在该外管11的后盖15与前盖16,可随着该外管11的圆形轮廓改变成符合该外壳10外形的圆形盖体,进而套盖结合在该外管11的后端与前端,组成圆形直管状的外壳10。 In addition to the above-described first preferred embodiment, the outer tube 11 of the preferred embodiment is a rectangular straight tube body, and the outer tube 11 may be in the shape of a circular straight tube. The cover is coupled to the rear cover 15 and the front cover 16 of the outer tube 11, and the circular profile of the outer tube 11 can be changed to a circular cover conforming to the outer shape of the outer casing 10, and the cover is coupled to the outer tube 11 The rear end and the front end constitute a circular straight tubular outer casing 10.
本发明的第一流道A,除上述第一较佳实施例是以多个导引片13在该外管11的内部分隔出由后往前左右反复弯曲延伸的第一流道A以外,也可改在该外管11内形成由后向前延伸的螺旋片体,在该外管11内分隔出由后向前螺旋延伸的第一流道A,只要第一流道A延伸的长度短于第二流道D,无论是左右反复弯曲延伸的第一流道A或是螺旋延伸的第一流道A都能发挥相同的功效。In the first flow path A of the present invention, in addition to the first preferred embodiment, the plurality of guiding pieces 13 are separated from the first flow path A which is repeatedly bent and extended from the rear to the front and the left side in the inner portion of the outer tube 11. A spiral piece extending rearwardly and forwardly is formed in the outer tube 11, and a first flow path A extending from the rear to the front is separated in the outer tube 11 as long as the length of the first flow path A is shorter than the second The flow path D can exert the same effect regardless of whether the first flow path A which is repeatedly bent left and right or the first flow path A which is spirally extended.
本发明使用时是与燃烧装置的进气口,例如引擎的进气口连接,如图4、图5所示,是单独使用一个本发明的使用方式,该引擎30设有一进气口301,在进气口301连接一进气软管31的一端,将该进气软管31的另一端套合在本发明外壳10的输出管162,即可完成安装,安装过程十分地容易。又如图6所示,是使用多个本发明的使用方式,当本发明运用在具有多个进气口301的引擎30,例如船舶的引擎30时,多个进气口301可分别通过多个进气软管31连接多个本发明的输出管162,使引擎30的每个进气口301都能利用本发明提升输入空气的压力而获益。When the invention is used, it is connected to the air inlet of the combustion device, for example, the air inlet of the engine. As shown in FIG. 4 and FIG. 5, the use mode of the present invention is used alone, and the engine 30 is provided with an air inlet 301. The end of the intake hose 301 is connected to one end of the intake hose 31, and the other end of the intake hose 31 is fitted to the output pipe 162 of the casing 10 of the present invention, so that the installation is completed, and the installation process is very easy. Further, as shown in FIG. 6, a plurality of uses of the present invention are used. When the present invention is applied to an engine 30 having a plurality of intake ports 301, such as the engine 30 of a ship, the plurality of intake ports 301 can pass through multiple The intake hoses 31 connect a plurality of outlet tubes 162 of the present invention such that each of the inlets 301 of the engine 30 can benefit from the increased pressure of the input air by the present invention.
当前述作为燃烧装置的两种引擎30运作时,其内部以及各进气口301处会因引擎30的运作而产生负压与吸引力,使连接在各进气软管31的本发明能由后盖15的多个气孔151处吸引空气,请参看图5所示的本发明第一较佳实施例,此时环境中的空气会由第一流道A的后端以及第二流道D的后端分别被吸引进入外壳10的内部。When the two engines 30 as the combustion device are operated as described above, the inside and each of the intake ports 301 generate a negative pressure and an attractive force due to the operation of the engine 30, so that the present invention connected to each of the intake hoses 31 can be The plurality of air holes 151 of the rear cover 15 attract air. Referring to the first preferred embodiment of the present invention shown in FIG. 5, the air in the environment will be from the rear end of the first flow path A and the second flow path D. The rear ends are respectively attracted into the inside of the casing 10.
由环境中被吸引流入左右反复弯曲延伸的第一流道A的空气,由于流动的路径较第二流道D长且流动时会受多个导引片13的阻碍而使得流速减缓,加上流动时是沿着弯曲的第一流道A行进,因此最后减缓速度的气流会由气室B的侧旁旋转流入气室B内,沿着渐缩段1611倾斜的内周面向前逐渐加速,再以螺旋的移动方式向该输出管162的输出流道c流出;相对的,由环境中流入进气件20的第二流道D的空气由于流动的路径最短且中间没有阻碍,因此能以最快的速度向前流动至第二流道D的前端,向输出管162内部的输出流道c的中间喷出。The air that is drawn into the first flow path A that is repeatedly bent and extended by the environment is attracted by the plurality of guide pieces 13 because the flow path is longer than the second flow path D, and the flow rate is slowed down, plus the flow The time travels along the curved first flow path A, so that the air flow of the final slowing speed will flow into the air chamber B from the side of the air chamber B, and gradually accelerates along the inner circumferential surface of the tapered portion 1611, and then The moving manner of the spiral flows out to the output flow path c of the output pipe 162; in contrast, the air flowing into the second flow path D of the air intake member 20 from the environment is the fastest because the flow path is the shortest and there is no obstruction in the middle. The speed flows forward to the front end of the second flow path D, and is ejected toward the middle of the output flow path c inside the output pipe 162.
由于第二流道D前端喷出的空气的速度,比气室B周围逐渐开始向前加速流动的空气速度快,藉由两者之间的速度差以及流动方向的差异,使中央向输出管162内直喷的气流能与周围螺旋移动的气流互相牵引,在中央直接前进的气流与周围的气流之间形成涡流,使气室B内向前流动的空气除了利用宽度 逐渐缩减的渐缩段1611,以喷嘴的方式达到向前加速的效果以外,还能进一步利用气流之间的涡流,增强输出管162的输出流道c所输出空气的压力与速度,使连接本发明的引擎30内的燃油,因进气口301内部形成低压区,可增加进气口301的进气效率,使引擎30内的燃油能完全地燃烧,减少油耗、增强引擎30的马力且减少点火装置积碳以及空气污染物的产生。Since the velocity of the air ejected from the front end of the second flow path D is faster than the air velocity gradually starting to accelerate forward around the air chamber B, the central output tube is made by the difference in speed between the two and the difference in flow direction. The direct injection airflow in 162 can be mutually drawn with the surrounding spiral moving airflow, and a vortex is formed between the airflow directly flowing in the center and the surrounding airflow, so that the air flowing forward in the air chamber B is not only the width of the air. The gradually decreasing tapered section 1611 can achieve the effect of forward acceleration by means of a nozzle, and can further utilize the eddy current between the airflows to enhance the pressure and speed of the air outputted from the output flow passage c of the output pipe 162, so that the connection is The fuel in the engine 30 of the invention can increase the intake efficiency of the intake port 301 due to the formation of a low pressure region inside the intake port 301, so that the fuel in the engine 30 can be completely burned, the fuel consumption is reduced, the horsepower of the engine 30 is enhanced, and the engine 30 is reduced. Ignition device carbon deposits and the generation of air pollutants.
本发明使用时,前述图4、图6所示的进气软管31除了以完全涵盖的方式与进气口301连接以外,也可以将进气软管31以周围具有间隙的方式插入进气口301内。请配合参看图7,该引擎30设有一进气口301,在本发明外壳10的输出管162连接一进气软管31,该进气软管31朝向该进气口301的一端插入该进气口301内,且该进气软管31与该进气口301之间有间隙。When the present invention is used, the intake hose 31 shown in FIGS. 4 and 6 may be connected to the intake port 301 in a completely covered manner, and the intake hose 31 may be inserted into the intake air with a gap therebetween. Within port 301. Referring to FIG. 7, the engine 30 is provided with an air inlet 301. An air inlet hose 31 is connected to the output pipe 162 of the casing 10 of the present invention. The air inlet hose 31 is inserted into one end of the air inlet 301. There is a gap between the intake hose 31 and the intake port 301 in the port 301.
如此,经由本发明加速的气流由输出流道c向进气口301内流出时,在进气口301内部形成的负压会将进气口301外侧周围的空气由进气软管31与输出管162之间的间隙牵引进入进气口301内,进一步增加输入进气口301内空气的量,更加提升燃烧装置如引擎30内燃油燃烧的效率,增强引擎30的马力且减少点火装置积碳以及空气污染物的产生。Thus, when the airflow accelerated by the present invention flows out of the intake port 301 from the output flow path c, the negative pressure formed inside the intake port 301 will be the air around the outer side of the intake port 301 from the intake hose 31 and the output. The gap between the tubes 162 is drawn into the air inlet 301, further increasing the amount of air input into the air inlet 301, further improving the efficiency of fuel combustion in the combustion device such as the engine 30, enhancing the horsepower of the engine 30 and reducing the carbon deposit of the ignition device. And the generation of air pollutants.
本发明第二较佳实施例,是改变第一较佳实施例中所述外壳10的穿口163的形状以及所述的进气件20的构造,其余构造皆与上述的第一较佳实施例中记载的相同。如图8至图10所示,在本发明的第二较佳实施例中,是在前盖16的渐缩段1611穿设一圆形的穿口163,对应该穿口163外端的周缘,在该套盖部161的外表面凹入形成一非圆形的嵌槽1631,如本较佳实施例该嵌槽1631是矩形槽,该穿口163贯穿该嵌槽1631的中央。A second preferred embodiment of the present invention is to change the shape of the through opening 163 of the outer casing 10 and the structure of the air inlet member 20 in the first preferred embodiment, and the remaining configurations are the first preferred embodiment described above. The same is true in the examples. As shown in FIG. 8 to FIG. 10, in the second preferred embodiment of the present invention, a circular opening 163 is formed in the tapered portion 1611 of the front cover 16, corresponding to the periphery of the outer end of the opening 163. A non-circular recess 1631 is recessed in the outer surface of the cover portion 161. The recess 1631 is a rectangular slot in the preferred embodiment. The through hole 163 extends through the center of the recess 1631.
第二较佳实施例的进气件20设有一勾状的气管23,该气管23位于所述的气室B内,该气管23的前端位于该输出流道c的后方,且该气管23的前端朝向所述的输出流道c的中央,该气管23的后端穿置在该穿口163,在该气管23向外穿出该穿口163的部分形成一喇叭形状的扩张部24,对应该嵌槽1631的形状,在该气管23的周围环绕形成一矩形的嵌板25,该嵌板25嵌设并粘合固定在该嵌槽1631内,使该进气件20穿置固定在该外壳10的前盖16。The air intake member 20 of the second preferred embodiment is provided with a hook-shaped air pipe 23, and the air pipe 23 is located in the air chamber B. The front end of the air pipe 23 is located behind the output flow path c, and the air pipe 23 is The front end faces the center of the output flow path c, the rear end of the air tube 23 passes through the opening 163, and a portion of the air tube 23 that passes outwardly through the opening 163 forms a flared expansion portion 24, The shape of the slot 1631 should be formed, and a rectangular panel 25 is formed around the air tube 23, and the panel 25 is embedded and fixed in the recess 1631 to allow the air inlet member 20 to be fixed thereto. The front cover 16 of the outer casing 10.
在该气管23内形成所述的第二流道D,该第二流道D前端的宽度尺寸窄于所述的输出流道c后端的宽度尺寸,该第二流道D的前端朝向该输出流道c的后端,正对该输出流道c的中央;该第二流道D的后端位于该外壳10的前盖16之 外,与所述外壳10周围的环境相通,且该第二流道D延伸的长度短于所述第一流道A延伸的长度,较佳的,该第二流道D延伸的长度短于该第一流道A延伸长度的一半甚至四分之一。由于第二较佳实施例其余的构造由于皆与上述的第一较佳实施例中所述的构造相同,因此本发明在此不加以赘述。Forming the second flow path D in the gas pipe 23, the width of the front end of the second flow path D is narrower than the width dimension of the rear end of the output flow path c, and the front end of the second flow path D faces the output The rear end of the flow path c is in the center of the output flow path c; the rear end of the second flow path D is located in the front cover 16 of the outer casing 10. The length of the second flow path D is shorter than the length of the first flow path A. Preferably, the length of the second flow path D is shorter than the length. The first flow path A extends half or even a quarter of the length. Since the rest of the configuration of the second preferred embodiment is the same as that described in the first preferred embodiment described above, the present invention is not described herein.
本发明第二较佳实施例使用时,如图10所示,由第一流道A后端吸入的空气会以左右反复弯曲的路径前进,由于第一流道A的路径比第二流道D长且有多个导引片13阻碍,因此在第一流道A流动的空气的速度会比通过第二流道D流动的空气的速度慢。由于第二流道D前端喷出的空气的速度,比气室B周围向前螺旋加速的空气速度快,藉由两者快、慢之间的速度差以及流动方向的差异,在第二流道D前端喷出的气流与气室B周围向前螺旋流动的气流之间产生涡流,使气室B内向前流动的空气除了因为前盖16喷嘴的外形而向前加速以外,还能进一步利用气流之间的涡流,增强输出流道c输出空气的压力与速度。When the second preferred embodiment of the present invention is used, as shown in FIG. 10, the air taken in by the rear end of the first flow path A advances in a path that is repeatedly curved left and right, since the path of the first flow path A is longer than the second flow path D. And a plurality of guide pieces 13 are obstructed, so the speed of the air flowing in the first flow path A is slower than the speed of the air flowing through the second flow path D. Since the velocity of the air ejected from the front end of the second flow path D is faster than the speed of the forward spiral around the air chamber B, the speed difference between the fast and the slow and the difference in the flow direction are in the second flow. A vortex is generated between the airflow jetted from the front end of the tunnel D and the airflow flowing forwardly around the air chamber B, so that the air flowing forward in the air chamber B can be further utilized in addition to being accelerated forward due to the shape of the nozzle of the front cover 16. The eddy current between the air flows enhances the pressure and velocity of the output air flow c.
本发明第三较佳实施例,是改变第一、第二较佳实施例中所述外壳10的前盖16的形状,以及所述的进气件20的形状,其余构造皆与上述的第一、第二较佳实施例中记载的相同。如图11至图13所示,在本发明的第二较佳实施例中,该前盖16设有一套盖部161,该套盖部161是盖体并且以后侧套合固定在该外管11前端的周围,该套盖部161后侧内壁的左右宽度比所述外管11前端周围的左右宽度大,当该套盖部161套合固定在该外管11前端时,在该套盖部161的左右两侧与该外管11前端的左右两侧之间形成两穿口163,该套盖部161后侧的其余部分则是紧夹该外管11前端的前后两侧固定。A third preferred embodiment of the present invention is to change the shape of the front cover 16 of the outer casing 10 in the first and second preferred embodiments, and the shape of the air intake member 20, and the remaining configurations are the same as the above 1. The same as described in the second preferred embodiment. As shown in FIG. 11 to FIG. 13 , in the second preferred embodiment of the present invention, the front cover 16 is provided with a cover portion 161 which is a cover body and is fastened to the outer tube at the rear side. Around the front end, the left and right widths of the inner wall of the rear side of the cover portion 161 are larger than the left and right widths around the front end of the outer tube 11, and when the cover portion 161 is sleeved and fixed to the front end of the outer tube 11, the cover is Two through holes 163 are formed between the left and right sides of the portion 161 and the left and right sides of the front end of the outer tube 11. The remaining portion of the rear side of the cover portion 161 is fixed to the front and rear sides of the front end of the outer tube 11.
该套盖部161的前侧形成形状逐渐朝前收窄的渐缩段1611,在该渐缩段1611的中间朝前伸设一输出管162,该输出管162是直管且宽度尺寸小于该外管11的宽度尺寸,在该套盖部161内形成一气室B,该气室B的前侧由后向前逐渐收窄,所述的第一流道A的前端与该气室B后端的侧旁相通,在该输出管162内形成一输出流道c,该输出流道c是圆型的直线通道且与该气室B的前端相通。The front side of the cover portion 161 forms a tapered portion 1611 whose shape gradually narrows toward the front, and an output tube 162 is formed in the middle of the tapered portion 1611. The output tube 162 is a straight tube and has a width smaller than the width. The width of the outer tube 11 is such that a plenum B is formed in the cover portion 161, and the front side of the plenum B is gradually narrowed from the rear to the front, and the front end of the first flow passage A and the rear end of the air chamber B are Sideways communicate, and an output flow path c is formed in the output pipe 162. The output flow path c is a circular linear passage and communicates with the front end of the gas chamber B.
所述的进气件20设置在该气室B内,该进气件20设有一喷气管26,该喷气管26设于该气室B内并位于该输出流道c的后方,在该喷气管26的后端连接两分叉的侧管27,两侧管27的后端紧密穿置在两穿口163处固定,在该进气件20的喷气管26以及两侧管27内形成一第二流道D,该第二流道D前端的宽度尺寸 窄于该输出流道c后端的宽度尺寸,且该第二流道D的前端朝向该输出流道c的后端,正对该输出流道c的中央,该第二流道D的后端分为左右两处且开口在该外壳10的前盖16之外,与该外壳10周围的环境相通,该第二流道D左右各侧延伸的长度短于该第一流道A延伸的长度,较佳的,上述该第二流道D延伸的长度短于该第一流道A延伸长度的一半甚至四分之一。由于第三较佳实施例其余的构造皆与第一、第二较佳实施例中记载的相同,因此本发明在此不加以限制。The air inlet member 20 is disposed in the air chamber B. The air inlet member 20 is provided with a jet tube 26 disposed in the air chamber B and located behind the output flow path c. The rear end of the air tube 26 is connected to the two bifurcated side tubes 27, and the rear ends of the two side tubes 27 are closely spaced and fixed at the two through openings 163, and a gas tube 26 and two side tubes 27 of the air inlet member 20 are formed. Second flow path D, the width dimension of the front end of the second flow path D Narrower than the width dimension of the rear end of the output flow path c, and the front end of the second flow path D faces the rear end of the output flow path c, facing the center of the output flow path c, the rear end of the second flow path D Dividing into two places on the left and right sides and opening outside the front cover 16 of the outer casing 10, communicating with the environment around the outer casing 10, the length of the left and right sides of the second flow path D is shorter than the length of the first flow path A. Preferably, the second flow path D extends for a length shorter than half or even a quarter of the length of the first flow path A. Since the rest of the configuration of the third preferred embodiment is the same as that described in the first and second preferred embodiments, the present invention is not limited thereto.
上述本发明第三较佳实施例,除了是在该前盖16的套盖部161的左右两侧与该外管11前端周围的左右两侧之间形成两穿口163以外,也可将该套盖部的形状设为内壁的一侧与该外管11前端周围相对侧有间隙,仅在该套盖部161周围的其中一侧与该外管11前端的相对侧之间形成一穿口163,这时该进气件20的喷气管26仅向后连接一个朝向该穿口163向后延伸的侧管27,该侧管27的后端穿置固定在该穿口163,使喷气管26、侧管27内形成的第二流道D的后端开口在该外壳10的前盖16之外,与周围的环境相通。In the third preferred embodiment of the present invention, in addition to the two openings 163 formed between the left and right sides of the cover portion 161 of the front cover 16 and the left and right sides of the front end of the outer tube 11, the same may be used. The shape of the cover portion is such that one side of the inner wall has a gap with the opposite side of the front end of the outer tube 11, and only a gap is formed between one side of the cover portion 161 and the opposite side of the front end of the outer tube 11. 163. At this time, the gas injection pipe 26 of the gas inlet member 20 is only connected backward to a side pipe 27 extending rearwardly toward the opening 163. The rear end of the side pipe 27 is fixedly disposed at the opening 163 to make the gas pipe. 26. The rear end opening of the second flow path D formed in the side tube 27 is outside the front cover 16 of the outer casing 10 and communicates with the surrounding environment.
本发明第三较佳实施例使用时,如图11、图12所示,由第一流道A后端吸入的空气会以左右反复弯曲的路径前进,由于第一流道A的路径比第二流道D长且有多个导引片13阻碍,因此在第一流道A流动的空气的速度会比通过第二流道D流动的空气的速度慢。此外,该外壳10周围的空气会由第二流道D的两个后端进入该进气件20内,接着由喷气管26朝输出流道c的中央喷出,由于第二流道D前端喷出的空气的速度,比气室B周围向前螺旋加速的空气速度快,藉由两者的速度差以及流动方向的差异,在第二流道D前端喷出的气流与气室B周围向前螺旋流动的气流之间产生涡流,使气室B内向前流动的空气除了因为前盖16喷嘴的外形而向前加速以外,还能进一步利用气流之间的涡流,增强输出流道c输出空气的压力与速度。When the third preferred embodiment of the present invention is used, as shown in FIG. 11 and FIG. 12, the air taken in by the rear end of the first flow path A advances in a path that is repeatedly curved left and right, since the path of the first flow path A is smaller than the second flow. The track D is long and has a plurality of guide pieces 13 blocked, so the speed of the air flowing in the first flow path A is slower than the speed of the air flowing through the second flow path D. In addition, air around the outer casing 10 enters the air intake member 20 from both rear ends of the second flow path D, and is then ejected toward the center of the output flow path c by the air injection tube 26, since the front end of the second flow path D The velocity of the ejected air is faster than the velocity of the air accelerated by the forward spiral around the chamber B, and the airflow ejected at the front end of the second flow passage D and the periphery of the air chamber B by the difference in speed between the two and the difference in the flow direction The eddy current is generated between the airflows flowing forwardly, so that the air flowing forward in the air chamber B can be further accelerated by the eddy current between the airflows in addition to the forward movement of the nozzles of the front cover 16, and the output flow path c is enhanced. Air pressure and speed.
本发明除前述第一至第三较佳实施例,当安装在引擎30使用时,吸引环境中的空气进入第一流道A与第二流道D的方式,是以引擎30运作时的负压产生的吸引力将空气吸入,是一种自然进气的手段,除此以外,也可以在第一流道A与第二流道D的后端,或第一流道A与第二流道D择一的后端连接主动进气的装置,以强制进气的手段达到提升空气进入引擎30的压力的功效。 In addition to the foregoing first to third preferred embodiments, when the engine 30 is installed, the manner of attracting air in the environment into the first flow path A and the second flow path D is a negative pressure when the engine 30 operates. The generated attraction attracts air and is a means of natural intake. In addition, it can also be selected at the rear end of the first flow path A and the second flow path D, or the first flow path A and the second flow path D. The rear end of the first unit is connected to the active intake device to force the intake air to increase the pressure of the air entering the engine 30.
如图14所示的本发明第四实施例,是在如第一较佳实施例的构造中增加强制进气的手段,是在所述外壳10的后盖15的后端结合一作为主动进气手段的后端风扇进气构造40,并在如第一较佳实施例中所述的进气件20的管部22连接一外接管32,以该外接管32连接一作为主动进气手段的侧向风扇进气构造41。由于本发明前述第四较佳实施例其余构造皆与第一较佳实施例中所述相同,故本发明在此不加以赘述。The fourth embodiment of the present invention as shown in FIG. 14 is a means for adding a forced air intake in the configuration of the first preferred embodiment, and is coupled to the rear end of the rear cover 15 of the outer casing 10 as an active feed. The rear end fan air intake structure 40 of the air means, and the outer tube 32 is connected to the tube portion 22 of the air inlet member 20 as described in the first preferred embodiment, and the external connection tube 32 is connected as an active air intake means. Lateral fan intake configuration 41. The rest of the configuration of the fourth preferred embodiment of the present invention is the same as that described in the first preferred embodiment, and the present invention is not described herein.
当前述本发明第四较佳实施例使用时,是将输出流道c接向引擎30,接着分别启动该后端风扇进气构造40以及该侧向风扇进气构造41,将周围环境的空气吸引吹入第一流道A的后端与第二流道D的后端,使第二流道D前端喷出的空气与第一流道A前端喷出的空气在气室B汇集,藉由两者的速度差以及流动方向的差异产生涡流,使气室B内向前流动的空气除了因为加压的空气以及前盖16喷嘴的外形而向前加速以外,还能进一步利用涡流,增强输出流道c输出空气的压力与速度。When the fourth preferred embodiment of the present invention is used, the output flow path c is connected to the engine 30, and then the rear end fan intake structure 40 and the lateral fan intake structure 41 are respectively activated to surround the ambient air. The suction is blown into the rear end of the first flow path A and the rear end of the second flow path D, so that the air ejected from the front end of the second flow path D and the air ejected from the front end of the first flow path A are collected in the air chamber B, by two The difference in speed and the difference in flow direction generate eddy currents, so that the air flowing forward in the air chamber B can be further accelerated by the eddy current in addition to the pressurized air and the shape of the nozzle of the front cover 16, and the output flow path can be further enhanced. c Output air pressure and speed.
以上所述仅为本发明的较佳实施例而已,并非用以限定本发明主张的权利范围,凡其它未脱离本发明所揭示的精神所完成的等效改变或修饰,均应包括在本发明的申请专利范围内。 The above description is only the preferred embodiment of the present invention, and is not intended to limit the scope of the claims of the present invention, and other equivalent changes or modifications which are not departing from the spirit of the present invention should be included in the present invention. Within the scope of the patent application.

Claims (10)

  1. 一种空气增力器,其特征在于,包括一外壳以及一穿置在所述外壳的进气件,其中:An air booster includes an outer casing and an air intake member disposed through the outer casing, wherein:
    所述外壳是直管状的壳体并且在前端设有一输出管,所述输出管的宽度尺寸小于所述外壳的其余部分的宽度尺寸,在所述外壳的内部由后向前相连形成一第一流道、一气室以及一输出流道,所述第一流道是由后朝前弯曲延伸的通道,所述第一流道的前端与所述气室后端的侧旁相通,所述气室是空间且前侧由后向前逐渐收窄,所述输出流道形成在所述输出管内,所述输出流道是直线的通道并连接在所述气室的前端,在所述外壳设有所述输出管以外的周围部分形成一穿口;The outer casing is a straight tubular casing and is provided at the front end with an output pipe having a width dimension smaller than a width dimension of a remaining portion of the outer casing, and a first flow is formed from the rear to the front inside the outer casing. a passage, an air chamber, and an output flow passage, the first flow passage being a passage extending from a rearward forward direction, a front end of the first flow passage communicating with a side of the rear end of the air chamber, the air chamber being a space The front side is gradually narrowed from the rear to the front, the output flow path is formed in the output tube, the output flow path is a straight passage and is connected to the front end of the air chamber, and the output is provided in the outer casing a peripheral portion other than the tube forms a through opening;
    所述进气件是管体并穿置在所述穿口,所述进气件的前端位于所述气室内并朝向所述输出流道的后端,在所述进气件的内部形成一第二流道,所述第二流道延伸的长度短于所述第一流道延伸的长度,所述第二流道的前端较所述输出流道窄而朝向所述输出流道的中央,所述第二流道的后端位于所述外壳之外,与所述外壳外部周围的环境相通。The air inlet member is a tubular body and is disposed at the through hole, and a front end of the air inlet member is located in the air chamber and faces a rear end of the output flow passage, and a inside of the air inlet member is formed a second flow path, the length of the second flow path extending is shorter than the length of the first flow path, and the front end of the second flow path is narrower than the output flow path toward the center of the output flow path. The rear end of the second flow passage is located outside the outer casing and communicates with an environment surrounding the outer portion of the outer casing.
  2. 如权利要求1所述的空气增力器,其特征在于,所述穿口形成在所述外壳对应内部的设有所述气室处。The air booster according to claim 1, wherein said opening is formed at a corresponding inner portion of said outer casing.
  3. 如权利要求2所述的空气增力器,其特征在于,所述外壳包括一外管以及一结合在所述外管的前盖,所述外管是竖直设置的直管体且上、下相反的两端分为前、后端,所述第一流道形成在所述外管内,且所述第一流道在所述外管的前、后两端形成开口;所述前盖设有一套盖部,所述套盖部是盖体并且套合固定在所述外管的前端,所述套盖部的前侧形成形状逐渐朝前收窄的渐缩段,所述输出管是由所述渐缩段的中间朝前伸设形成,所述气室形成在所述套盖部内,所述穿口形成在所述套盖部的周围,所述第二流道延伸的长度短于所述第一流道延伸长度的一半。The air booster according to claim 2, wherein said outer casing comprises an outer tube and a front cover coupled to said outer tube, said outer tube being a vertically disposed straight tube body and The opposite ends are divided into a front end and a rear end, the first flow path is formed in the outer tube, and the first flow path forms an opening at the front and rear ends of the outer tube; the front cover is provided with a a cover portion, the cover portion is a cover body and is sleeved and fixed on a front end of the outer tube, and a front side of the cover portion forms a tapered portion whose shape gradually narrows toward the front, and the output tube is The middle of the tapered section is formed to extend forwardly, the air chamber is formed in the cover portion, the through hole is formed around the cover portion, and the length of the second flow passage extends is shorter than The first flow path extends for half of the length.
  4. 如权利要求3所述的空气增力器,其特征在于,所述套盖部紧密套合在所述外管的前端,所述穿口穿设在所述套盖部的渐缩段;所述进气件设有一块状部以及一与所述块状部相连的管部,所述块状部位于所述的气室内且外端伸抵所述的输出流道的后方,所述管部穿置在所述穿口,且所述块状部接邻所述管部的一侧抵靠并粘合在该渐缩段的内面,所述第二流道形成在所 述块状部与所述管部内,所述第二流道延伸的长度短于所述第一流道延伸长度的四分之一。The air booster according to claim 3, wherein the cover portion is tightly fitted to the front end of the outer tube, and the through hole is formed in a tapered portion of the cover portion; The air inlet member is provided with a block portion and a pipe portion connected to the block portion, the block portion is located in the air chamber and the outer end extends to the rear of the output flow channel, the tube a portion is disposed in the opening, and a side of the block portion adjacent to the tube portion abuts and adheres to an inner surface of the tapered portion, and the second flow path is formed at the portion In the block portion and the tube portion, the second flow path extends for a length shorter than a quarter of the first flow path extension length.
  5. 如权利要求3所述的空气增力器,其特征在于,所述套盖部紧密套合在所述外管的前端,所述穿口穿设在所述套盖部的渐缩段,对应所述穿口外端的周缘,在所述套盖部的外表面凹入形成一非圆形的嵌槽,所述穿口贯穿该嵌槽的中央;所述进气件设有一勾状的气管,所述气管位于所述气室内且前端位于所述的输出流道的后方,所述气管的后端穿置在所述穿口,在所述气管向外穿出所述穿口的部分形成一喇叭形状的扩张部,配合所述嵌槽的形状,在所述气管的周围形成一嵌板,所述嵌板嵌设并粘合固定在所述嵌槽内,所述第二流道形成在所述气管内,所述第二流道延伸的长度短于所述第一流道延伸长度的四分之一。The air booster according to claim 3, wherein the cover portion is tightly fitted to the front end of the outer tube, and the through hole is formed in a tapered portion of the cover portion, corresponding to a peripheral edge of the outer end of the opening is concavely formed on the outer surface of the cover portion to form a non-circular recess, the through hole penetrating the center of the recess; the air inlet member is provided with a hook-shaped air tube. The air tube is located in the air chamber and the front end is located behind the output flow channel, the rear end of the air tube is disposed at the through hole, and a portion of the air tube that passes outwardly through the through hole forms a a flare-shaped expansion portion, in combination with the shape of the recessed groove, forming a panel around the air tube, the panel being embedded and adhesively fixed in the recessed groove, the second flow path being formed in In the trachea, the second flow path extends for a length shorter than a quarter of the first flow path extension length.
  6. 如权利要求3所述的空气增力器,其特征在于,所述套盖部内壁的相反两侧各与所述外管前端周围的相对侧之间有间隙,所述穿口形成在所述套盖部内壁的一侧与所述外管前端周围的相对侧之间,并在所述套盖部的另一侧与所述外管前端的相对侧之间形成另一穿口;所述进气件设有一喷气管,所述喷气管位于所述的气室内并位于所述的输出流道的后方,在所述喷气管的后端连接两分叉的侧管,两侧管的后端紧密穿置在两穿口处固定,所述第二流道形成在所述喷气管以及两侧管内,所述第二流道延伸的长度短于所述第一流道延伸长度的四分之一。The air booster according to claim 3, wherein a gap is formed between opposite sides of the inner wall of the cover portion and an opposite side of the front end of the outer tube, and the opening is formed in the Between one side of the inner wall of the cover portion and the opposite side of the front end of the outer tube, and another opening is formed between the other side of the cover portion and the opposite side of the front end of the outer tube; The air inlet member is provided with a jet pipe, the gas pipe is located in the gas chamber and located behind the output flow channel, and a bifurcated side pipe is connected at the rear end of the gas pipe, and the two sides of the pipe are The end is tightly inserted at two openings, the second flow passage is formed in the jet tube and the two side tubes, and the second flow path extends for a length shorter than a quarter of the extension length of the first flow path One.
  7. 如权利要求3至6中任一项所述的空气增力器,其特征在于,所述的外管是矩形直管体,在所述外管内以上、下间隔的排列方式结合多个矩形的导引片,由前至后数来为奇数序列的各导引片,其右端缘连接在所述外管右侧的内壁且左端缘朝左并朝后斜向延伸,奇数序列的各导引片的左端缘与所述外管左侧的内壁之间有间隙;由前至后数来为偶数序列的各导引片,其左端缘连接在所述外管左侧的内壁且右端缘朝右并朝后斜向延伸,偶数序列的各导引片的右端缘与所述外管右侧的内壁之间有间隙;所述第一流道是所述外管内的空间被多个导引片分隔而成。The air booster according to any one of claims 3 to 6, wherein the outer tube is a rectangular straight tube body, and the upper and lower spaced arrangement in the outer tube is combined with a plurality of rectangular shapes. The guiding piece is an odd-numbered series of leading pieces from front to back, the right end edge of which is connected to the inner wall of the right side of the outer tube and the left end edge is leftward and obliquely extends rearward, and the odd sequence is guided. a gap is formed between the left end edge of the sheet and the inner wall of the left side of the outer tube; each of the guide sheets having an even sequence from front to back has a left end edge connected to the inner wall of the left side of the outer tube and the right end edge Rightward and obliquely extending rearward, there is a gap between the right end edge of each of the even-numbered guide pieces and the inner wall of the right side of the outer tube; the first flow path is a space in the outer tube is guided by a plurality of guide pieces Separated.
  8. 如权利要求7所述的空气增力器,其特征在于,所述外管是左、右两半壳体相对组合而成的矩形直管体,所述外壳进一步包括一后盖,所述后盖 是盖体并且紧密套合固定在所述外管11后端的周围,在所述后盖的后面穿设多个气孔。The air booster according to claim 7, wherein the outer tube is a rectangular straight tube body in which the left and right halves are oppositely combined, and the outer casing further includes a rear cover, the rear cover It is a cover body and is tightly fitted around the rear end of the outer tube 11, and a plurality of air holes are bored behind the rear cover.
  9. 如权利要求1或2或3所述的空气增力器,其特征在于,在所述外壳的后端结合一后端风扇进气构造。The air booster of claim 1 or 2 or 3, wherein a rear end fan intake structure is coupled to the rear end of the outer casing.
  10. 如权利要求9所述的空气增力器,其特征在于,在所述进气件的外端连接一外接管,以所述外接管连接一侧向风扇进气构造。 The air booster according to claim 9, wherein an outer pipe is connected to an outer end of said air intake member, and said outer pipe connecting side is connected to a fan air intake structure.
PCT/CN2016/094128 2016-08-09 2016-08-09 Air booster WO2018027536A1 (en)

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Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2596052Y (en) * 2002-11-12 2003-12-31 刘晨 Power accelerator for automobile
CN201100191Y (en) * 2007-07-25 2008-08-13 尹翠君 Gas engine negative pressure flow guider
US7552722B1 (en) * 2007-12-26 2009-06-30 Toyota Motor Engineering & Manufacturing North America, Inc. Exhaust gas recirculator devices
CN201753630U (en) * 2010-08-24 2011-03-02 重庆瑞阳科技开发有限公司 Flow mixer
CN104564451A (en) * 2014-12-24 2015-04-29 潍柴动力股份有限公司 Engine and air intake device thereof for improving EGR (exhaust gas recirculation) rate of engine
CN105008706A (en) * 2013-02-28 2015-10-28 邦迪克斯商用车系统有限责任公司 Gas recirculation in turbocharged diesel engines
TWM523757U (en) * 2016-01-11 2016-06-11 San-Chun Meng Air booster
CN205370751U (en) * 2016-01-13 2016-07-06 孟三中 Air booster
TWM534696U (en) * 2016-08-03 2017-01-01 San-Chun Meng Air booster

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN2596052Y (en) * 2002-11-12 2003-12-31 刘晨 Power accelerator for automobile
CN201100191Y (en) * 2007-07-25 2008-08-13 尹翠君 Gas engine negative pressure flow guider
US7552722B1 (en) * 2007-12-26 2009-06-30 Toyota Motor Engineering & Manufacturing North America, Inc. Exhaust gas recirculator devices
CN201753630U (en) * 2010-08-24 2011-03-02 重庆瑞阳科技开发有限公司 Flow mixer
CN105008706A (en) * 2013-02-28 2015-10-28 邦迪克斯商用车系统有限责任公司 Gas recirculation in turbocharged diesel engines
CN104564451A (en) * 2014-12-24 2015-04-29 潍柴动力股份有限公司 Engine and air intake device thereof for improving EGR (exhaust gas recirculation) rate of engine
TWM523757U (en) * 2016-01-11 2016-06-11 San-Chun Meng Air booster
CN205370751U (en) * 2016-01-13 2016-07-06 孟三中 Air booster
TWM534696U (en) * 2016-08-03 2017-01-01 San-Chun Meng Air booster

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