CN1834437A - I.C.jetting rotor engine - Google Patents

I.C.jetting rotor engine Download PDF

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Publication number
CN1834437A
CN1834437A CN 200610034739 CN200610034739A CN1834437A CN 1834437 A CN1834437 A CN 1834437A CN 200610034739 CN200610034739 CN 200610034739 CN 200610034739 A CN200610034739 A CN 200610034739A CN 1834437 A CN1834437 A CN 1834437A
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China
Prior art keywords
rotor
stator
shell
jetting
engine
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CN 200610034739
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Chinese (zh)
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汤卓勋
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Individual
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Individual
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Priority to CN 200610034739 priority Critical patent/CN1834437A/en
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Abstract

The present invention discloses an internal-combustion jet-type rotor engine. It is characterized by that it simulates motor structure, and combines it with the principle of piston type internal combustion engine and jet engine, in the inside of turbine rotor a stator with combustion cavity is set, the fuel is driven by high-pressure air pump and sprayed into the combustion cavity, the ignited explosive gas is passed through the jet cavity of turbine rotor to produce jet so as to drive rotor and make it implement monodirectional rotation.

Description

I. C. jetting rotor engine
[technical field]
The present invention relates to a kind of structure of explosive motor.
[background technique]
At present, various motor car engines mainly are piston internal-combustion engines on the market, and such motor passes through updating of last a century and develops, and are very perfect at present on design and manufacturing process, become the dominant type of motor car engine, experienced the commercialization production of last a century.
The main principle and the characteristics of this class motor are: utilize the to-and-fro motion of piston, form the full stroke of air inlet, compression, ignition promotion, exhaust.Because fuel oil is completely enclosed within the cylinder when acting, therefore the kinetic energy that produces can fully obtain utilizing, and forms effective Driving force.
But the maximum deficiency of this class motor is: owing to have the to-and-fro motion and the fuel oil compression process of piston, brought certain inertia loss and drag losses to motor, made the efficient of motor be difficult to obtain the raising of principle.In addition,, lose a part of power too, make engine structure become very complicated simultaneously owing to need the cooperation of various valves.
In the application of the prior art, another kind of motor is a jet engine, and its main type has turbojet engine and athodyd.
The basic principle and the characteristics of turbojet engine are as follows:
Turbojet engine is called for short turbojet engine, is made up of intake duct, gas compressor, firing chamber, turbine and jet pipe usually.Also has tail pipe burner between the turbine of part ordnance engine and jet pipe.
Turbojet engine belongs to hot machine, and the acting principle is similarly: release energy under the intake under the high pressure, low pressure.
High pressure draught enters the firing chamber subsequently.The fuel nozzle of firing chamber penetrates oil plant, and lights a fire after the air mixing, produces high-temperature high-pressure fuel gas, discharges backward.
High-temperature high-pressure fuel gas flows through high-temperature turbine backward, and can expand in turbine in the part is converted into mechanical energy, drives the turbine rotation.Because high-temperature turbine is contained on same the axle with gas compressor, therefore also drive pressure mechanism of qi rotation, thereby compression inhaled air repeatedly.
The high-temperature high-pressure fuel gas that flows out from high-temperature turbine continues to expand in jet pipe, to discharge backward from the afterbody spout at a high speed.This speed is more much bigger than the speed that air-flow enters motor, thereby has produced the reaction thrust to motor, orders about aircraft and flies forward.
Athodyd basic principle and characteristics are as follows:
Pressed engine is made up of intake duct (also claiming Diffuser), firing chamber, three ones of propelling nozzles, and is much simpler than turbojet engine.Its pluses and minuses are: the advantage of pressed engine be simple structure, in light weight, volume is little, thrust weight ratio is big, cost is low.But pressed engine does not have gas compressor, just can not start under the static situation in ground.
This shows that this class air breathing engine has flame or high hot air flow to spray from afterbody because of itself characteristic and when the work, can't be applicable to the various automobiles that travel on land.
[summary of the invention]
It is of the prior art above not enough in order to overcome that purpose of the present invention is exactly, and a kind of efficient low-consume, I. C. jetting rotor engine simple and compact for structure are provided.
For achieving the above object, the present invention proposes a kind of I. C. jetting rotor engine, comprises main shaft, shell, rotor, stator, igniting system and pump housing assembly; Described shell, stator, igniting system and pump housing assembly are affixed successively; Described stator is provided with some burning cavitys that are used for fuel combustion, on this burning cavity wall igniter and fuel nozzle is installed; Described igniting system and pump housing assembly are electrically connected with described igniter, are connected with described fuel nozzle pipeline; Described rotor seal is in described shell, and in the cavity between stator and shell, and coaxial with described stator, described rotor is provided with spray chamber around described burning cavity correspondence; Described main shaft and rotor coaxial are connected, and at least one end is exposed to outside the described shell.
Above-mentioned I. C. jetting rotor engine also comprises cooling cover, and is affixed with described stator, shell, and joins with described stator and/or shell pipeline, is used to carry refrigerant to cool off described stator, shell.
Described shell comprises housing, forward end seal cover; Described forward end seal cover covers at described housing front end, and described housing rear end and described stator are affixed; Described main shaft one end connects described forward end seal cover and is exposed to outside the described forward end seal cover.
Described igniting system and pump housing assembly comprise ignition location induction installation, igniting high pressure generation and power distribution device, water pump, high-pressure oil gas mixing pump and oil pump, described water pump links to each other by pipeline with described cooling cover, described high-pressure oil gas mixing pump links to each other with fuel nozzle in the described stator burning cavity by pipeline, described oil pump links to each other with described main shaft by pipeline, and igniting high pressure generation and power distribution device are electrically connected with described igniter.
The spray chamber of described rotor and the quantity of firing chamber do not wait, and form between spray chamber and the firing chamber asynchronous on the space.
Described spray chamber is a spiral type, and the eddy effusion direction and the described rotor circumference of its generation are tangent.
Described rotor is provided with lateral margin vortex sheet in described spray chamber both side edges, and its circumferencial direction along described rotor forms vortex shape.
Described burning cavity wall offers opening, and this opening and described cooling cover pipeline join, and are used to the refrigerant that circulates.Described shell or housing outer wall are provided with heat radiating fin.Described shell or inner walls offer the flow-disturbing groove.
Owing to adopted above scheme, brought following beneficial effect:
One, simulating motor structure of the present invention, principle in conjunction with internal-combustion piston engine and air breathing engine, at the inboard burning cavity that is equivalent to stator that is provided with of turbine rotor, fuel oil drives through the high-pressure air pump and sprays into burning cavity, pass through the spray chamber generation and the tangent injection of cylindrical of turbine rotor through the detonation gas of igniting, thereby promote the unidirectional rotation of rotor.The quantity in design of the spray chamber of turbine rotor and firing chamber does not wait, thereby forms between spray chamber and the firing chamber asynchronous on the space, creates the chance of fuel injection, igniting eruption to burning cavity.This structure has been cancelled the reciprocating motion of the pistons of reciprocating engine, presses folk prescription fully to rotation, and the inertia loss that has caused when therefore having eliminated reciprocating motion of the pistons is greatly enhanced efficient.
Two, structure of the present invention is easy to adopt computer to control, can be according to the requirement of the rotating speed and the moment of torsion of rotor, according to firing mode work such as symmetrical two chambeies, four chambeies, six chambeies, eight chambeies or 12 chambeies, thereby when the rotor high-speed rotation does not need very big power, can reduce the quantity of work burning cavity by computer control automatically, thereby save fuel oil; The quantity of may command increase work burning cavity when high speed operation needs to strengthen power again.
Three, overall structure of the present invention is simple, and profile is succinct, but the equal coaxial design of fuel oil, the lubricated and pump housing that cools off required usefulness with ignition timing mechanism integrator, thereby dwindles machine volume, and the motor volume of specific power is littler, efficient is higher.
Four, the present invention has saved complicated various structure member such as valve, piston rod owing to adopt the jetting rotor structure, and weight is lighter, and vibration and noise are lower; And producing efficiency of assembling improves, maintains simple and easy to do.
[description of drawings]
Fig. 1 is an overall structure schematic representation of the present invention;
Fig. 2 is a forward end seal cover structure schematic representation of the present invention;
Fig. 3 is the shell construction schematic representation;
Fig. 4 is the rotor structure schematic representation;
Fig. 5 is stator (rear end sealing cover) structural representation that has the cavity that burns;
Fig. 6 is a housing rear end cooling cover structural representation;
Fig. 7 is igniting system and pump housing assembly structure schematic representation;
Fig. 8 is one of sectional structure schematic representation of stator of the present invention, rotor cooperation;
Fig. 9 is two of the sectional structure schematic representation that cooperates of stator of the present invention, rotor;
Figure 10 is a STRUCTURE DECOMPOSITION schematic representation of the present invention.
[embodiment]
Also the present invention is described in further detail in conjunction with the accompanying drawings below by specific embodiment.
Embodiment one: please refer to the overall structure figure of the present invention of Fig. 1, Fig. 9, this routine motor comprises main shaft, shell, rotor, stator, igniting system and pump housing assembly; Shell comprises forward end seal cover, housing; Forward end seal cover, housing, stator, igniting system and pump housing assembly are affixed successively; Stator is provided with some burning cavitys that are used for fuel combustion, and igniter spark plug and high-pressure oil gas mixing nozzle are installed on this burning cavity wall; Igniting system and pump housing assembly are electrically connected with spark plug, are connected by pipeline with nozzle; Rotor seal is in housing, and in the cavity between stator and housing, and coaxial with stator, rotor is provided with spray chamber around the burning cavity correspondence; Main shaft and rotor coaxial are connected, and an end is exposed to outside the shell.
Main shaft 1 outputs power when rotor is subjected to the powered of oil inflame injection.
Shell comprises: forward end seal cover 2, housing 3, design has the supporting frame by triangular arrangement on this housing, is used for installing and fixing on vehicle chassis.
The stator 4 that has the cavity that burns, design has the mounting hole of spark plug and high-pressure oil gas mixing nozzle.
The cooling cover 5 of housing rear end, the general water port of cooling water flow is wherein arranged, communicate with the weep hole of forward end seal cover through the water port of hull outside, form circulation by cooling waterpump, after lowering the temperature through radiator once more the intake pipe flange plate from the cooling cover 5 of housing rear end send into housing.
Igniting system of this motor and pump housing assembly 6, ignition location induction installation, igniting high pressure generation and power distribution device, water pump, high-pressure oil gas mixing pump and the oil pump of wherein integrated igniting system.Igniting system is provided with power line and signaling line threading hole with pump housing assembly, is used for drawing the igniting analytic signal to the power supply of igniting system and from the ignition location induction installation, is used for igniting and fuel feeding control for computer.
The rotor 7 that has the spiral type spray chamber is seal-installed in the housing 3, matches the vortex jet flow when producing oil gas mixed combustion, the high speed rotating of the whole upper rotor part of promotion with stator 4.
Please refer to forward end seal cover structure schematic representation shown in Figure 2, this forward end seal is covered with and is equipped with: toxic emission pipe flange 21, be used for being connected with silencing apparatus, and carry out noise elimination noise reduction.Bolt hole 23 is used as assembling.The tank 24 of cooling water, cooling water through this concentrated flow to waste pipe flange plate 22 places, from pumping to radiator by water pump here.Spindle hole 25 is installing spaces of reserving to main shaft and bearing support thereof.
Please refer to shell construction schematic representation shown in Figure 3, it is provided with: be used to be installed to the supporting frame 31 on the vehicle chassis, totally three, be triangularly arranged; The bolt hole pedestal 32 of assembling usefulness; Outside is provided with the heat radiating fin 37 of fin-shaped, can increase heat diffusion area, improves heat dissipation rate and radiating effect; Bearing support 36; The bolt hole 34 of assembling usefulness; Inwall is provided with flow-disturbing groove 38, to increase the anti-thrust drag that gas jet runs into; The effect to the housing heat radiation is played in the but logical water port 33 of current of cooling on the housing; Oil hole on the bearing support is used for the junctor oil pump and refuels to bearing.Exhaust port 35 is used for the discharge of the waste gas behind the combustion jet.
Please refer to rotor structure schematic representation shown in Figure 4, it is provided with: spiral type spray chamber 72, and the gas after the burning of stator burning cavity therefrom sprays, and generation and the tangent Driving force of circumference; Spindle bearing 71 is used to install main shaft, and spindle bearing is provided with the keyway that is used for fixing main shaft; Lateral margin vortex sheet 73, it becomes vortex shape to arrange along rotor circumference direction two lateral margins, is mainly used in not from the spray chamber ejection and from the twice work doing of the pressurized gas of axial outflow; Be provided with airtight groove 74 between rotor and the stator, realize by the non-contact mode airtight, because of the airtight needs of contact-type are taked lubricated and cooling, make structure obviously complicated, and only need deal with possible lateral leakage in this example, air tight manner just can reach requirement, and structure is simple many.In case there are pressurized gas to leak from here, then can be stopped to return by the stator end cap, discharge through lateral margin vortex sheet place, produce additional thrust.
Please refer to burn stator (rear end sealing cover) structural representation of cavity of shown in Figure 5 having, it is provided with: the bolt hole 41 of assembling usefulness; The bearing support that is used to install, bearing support are provided with the hole that is used to add lubricant oil; Cooling water flow through hole 42 on the burning cavity is used for to this cavity heat radiation; Burning cavity 45 becomes vortex shape to arrange, after the high-pressure atomization fuel oil here burns, through the spray chamber ejection of rotor; Be provided with spark plug mounting hole 44, high-pressure oil gas mixing nozzle 43 in the burning cavity 45, be used to form the injection of the atomized fuel that drives by pressurized gas; The fuel feeding of bearing oil and oil drainage hole link to each other with oil pump on the pump housing assembly, form lubrication oil circulation; Opposite side has a pair of oilhole equally, and being used for provides lubricant oil to the bearing of this side.
Please refer to housing rear end cooling cover shown in Figure 6, it is provided with: the bolt hole frame 51 of assembling usefulness; Current distributing slot 53; Bosh 52; The flange plate 54 of cooling water inlet pipe is used for joining with water pump.
Please refer to igniting system shown in Figure 7 and pump housing assembly, it is provided with: assembling bolt hole support 61; Inner for laying the integrated space of igniting system and each pump; Power supply and signaling line threading hole 52; Be used for fixing the integrated bolt hole of each pump housing 53.
Please refer to the sectional structure schematic representation that Fig. 8, stator of the present invention shown in Figure 9, rotor, housing cooperate; Stator 4 is positioned at housing inner axes position, and the spiral type spray chamber of turbine rotor 7 is between the burning cavity of housing and stator.Spray into burning cavity when fuel oil drives through the high-pressure air pump, pass through the spray chamber generation and the tangent injection of cylindrical of turbine rotor through the detonation gas of igniting, thereby promote the unidirectional rotation of rotor.The quantity in design of the spray chamber of turbine rotor and firing chamber does not wait, thereby forms between spray chamber and the firing chamber asynchronous on the space, creates the chance of fuel injection, igniting eruption to burning cavity.
Please refer to STRUCTURE DECOMPOSITION schematic representation of the present invention shown in Figure 10.In the present invention, several big parts are overall structure, and component are less, therefore are convenient to assembling.
In assembling process, at first bearing is installed in the bearing support of housing and burning cavity, accurately behind the location, install sealing gasket and seal closure additional.Afterwards, the forward end seal cover is installed on the housing.Then, main shaft is installed in the axis hole of rotor, the back, location locks with key, and the position that attention key exposes can not be excessive, in order to avoid the inner face of scraping burning cavity.
Then, the epitrochanterian main shaft that installs main shaft is passed the bearing of housing, be installed on the housing.After installing, the bearing on the stator (rear end sealing cover) is aimed at main shaft.Forward end seal closure direction promotes, and at last these several parts is combined as a whole.Behind the bolt hole that secured in alignment is used, promptly available corresponding bolts is fixed.In the above process, also must install the cylinder pad additional.
After this, on the sealing cover of burning cavity rear end, put housing rear end cooling cover, installed the cylinder pad additional, aimed at spiro keyhole position postpone and fixed with corresponding bolts.
After this, just can install parts such as spark plug and oil nozzle, after need connecting in advance, can the fixed hole of igniting system and pump housing assembly aligning burning cavity rear end sealing cover be fixed with bolt with the position that igniting system and pump housing assembly are connected.
After finishing, promptly formed working morphology of the present invention with being connected of the radiator of outside, main control computer, power supply, fuel tank etc.
In specific embodiment, can also make suitable technological adjustment according to principle of the present invention.As can with go up example comprise forward end seal cover 2 one-body molded with the shell of housing 3 be one whole; Light a fire system and pump housing assembly and cooling cover can be integrated; It is described that the shape structure of each parts also is not limited to example; These all belong within the scope of the present invention.

Claims (10)

1, a kind of I. C. jetting rotor engine is characterized in that: comprise main shaft, shell, rotor, stator, igniting system and pump housing assembly; Described shell, stator, igniting system and pump housing assembly are affixed successively; Described stator is provided with some burning cavitys that are used for fuel combustion, on this burning cavity wall igniter and fuel nozzle is installed; Described igniting system and pump housing assembly are electrically connected with described igniter, are connected with described fuel nozzle pipeline; Described rotor seal is in described shell, and in the cavity between stator and shell, and coaxial with described stator, described rotor is provided with spray chamber around described burning cavity correspondence; Described main shaft and rotor coaxial are connected, and at least one end is exposed to outside the described shell.
2, I. C. jetting rotor engine as claimed in claim 1 is characterized in that: also comprise cooling cover, and affixed with described stator and/or shell, and join with described stator, shell pipeline, be used to carry refrigerant to cool off described stator, shell.
3, I. C. jetting rotor engine as claimed in claim 1 is characterized in that: described shell comprises housing, forward end seal cover; Described forward end seal cover covers at described housing front end, and described housing rear end and described stator are affixed; Described main shaft one end connects described forward end seal cover and is exposed to outside the described forward end seal cover.
4, I. C. jetting rotor engine as claimed in claim 1, it is characterized in that: described igniting system and pump housing assembly comprise ignition location induction installation, igniting high pressure generation and power distribution device, water pump, high-pressure oil gas mixing pump and oil pump, described water pump links to each other by pipeline with described cooling cover, described high-pressure oil gas mixing pump links to each other with fuel nozzle in the described stator burning cavity by pipeline, described oil pump links to each other with described main shaft by pipeline, and igniting high pressure generation and power distribution device are electrically connected with described igniter.
5, as each described I. C. jetting rotor engine among the claim 1-4, it is characterized in that: the spray chamber of described rotor and the quantity of firing chamber do not wait, and form between spray chamber and the firing chamber asynchronous on the space.
6, as each described I. C. jetting rotor engine among the claim 1-4, it is characterized in that: described spray chamber is a spiral type, and the eddy effusion direction and the described rotor circumference of its generation are tangent.
7, as each described I. C. jetting rotor engine among the claim 1-4, it is characterized in that: described rotor is provided with lateral margin vortex sheet in described spray chamber both side edges, and its circumferencial direction along described rotor forms vortex shape.
8, as each described I. C. jetting rotor engine among the claim 1-4, it is characterized in that: described burning cavity wall offers opening, and this opening and described cooling cover pipeline join, and are used to the refrigerant that circulates.
9, as each described I. C. jetting rotor engine among the claim 1-4, it is characterized in that: described shell or housing outer wall are provided with heat radiating fin.
10, I. C. jetting rotor engine as claimed in claim 3 is characterized in that: described shell or inner walls offer the flow-disturbing groove.
CN 200610034739 2006-03-27 2006-03-27 I.C.jetting rotor engine Pending CN1834437A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200610034739 CN1834437A (en) 2006-03-27 2006-03-27 I.C.jetting rotor engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200610034739 CN1834437A (en) 2006-03-27 2006-03-27 I.C.jetting rotor engine

Publications (1)

Publication Number Publication Date
CN1834437A true CN1834437A (en) 2006-09-20

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Family Applications (1)

Application Number Title Priority Date Filing Date
CN 200610034739 Pending CN1834437A (en) 2006-03-27 2006-03-27 I.C.jetting rotor engine

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014089771A1 (en) * 2012-12-12 2014-06-19 杨民结 Wheel-type internal combustion engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014089771A1 (en) * 2012-12-12 2014-06-19 杨民结 Wheel-type internal combustion engine
CN104937237A (en) * 2012-12-12 2015-09-23 周建煌 Wheel-type internal combustion engine
CN104937237B (en) * 2012-12-12 2017-09-15 周建煌 Wheeled explosive motor

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