CN110162863A - The thermal coupling design method of electric ducted fan - Google Patents

The thermal coupling design method of electric ducted fan Download PDF

Info

Publication number
CN110162863A
CN110162863A CN201910403121.3A CN201910403121A CN110162863A CN 110162863 A CN110162863 A CN 110162863A CN 201910403121 A CN201910403121 A CN 201910403121A CN 110162863 A CN110162863 A CN 110162863A
Authority
CN
China
Prior art keywords
ducted fan
motor
fan
thrust
efficiency
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
CN201910403121.3A
Other languages
Chinese (zh)
Other versions
CN110162863B (en
Inventor
李也
金宇智
张磊
董超凡
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Beijing Weihang Technology Co Ltd
Original Assignee
Beijing Weihang Technology Co Ltd
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 Beijing Weihang Technology Co Ltd filed Critical Beijing Weihang Technology Co Ltd
Priority to CN201910403121.3A priority Critical patent/CN110162863B/en
Publication of CN110162863A publication Critical patent/CN110162863A/en
Application granted granted Critical
Publication of CN110162863B publication Critical patent/CN110162863B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/10Geometric CAD
    • G06F30/15Vehicle, aircraft or watercraft design
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00Computer-aided design [CAD]
    • G06F30/20Design optimisation, verification or simulation

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Theoretical Computer Science (AREA)
  • Geometry (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • General Engineering & Computer Science (AREA)
  • Evolutionary Computation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pure & Applied Mathematics (AREA)
  • Mathematical Optimization (AREA)
  • Mathematical Analysis (AREA)
  • Computational Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

The present invention provides a kind of thermal coupling design methods of electric ducted fan, in the thermal coupling design method of electric ducted fan of the invention, consider that wheel hub in ducted fan compares the influence of the actual efficiency and actual thrust of fan blade and the influence of the power to the radiating requirements of motor (calorific value that the heat dissipation capacity on motor case surface is greater than motor) and motor, by the wheel hub of motor than being integrated into the design process of ducted fan with radiating requirements, it can make while the design result of ducted fan meets the requirement of multi-state environment, so that motor is met radiating requirements (calorific value that the heat dissipation capacity on motor case surface is greater than motor) and makes the volume minimization of motor, to improve the power to weight ratio of motor in ducted fan.

Description

The thermal coupling design method of electric ducted fan
Technical field
The present invention relates to aero propulsion technical field more particularly to a kind of thermal coupling design methods of electric ducted fan.
Background technique
With being increasingly stringenter to the requirements such as aircraft safety, energy-saving and environmental protection, reliable, more electricity aircrafts, electric aircraft and mixed It closes motor plane and has gradually obtained the concern of people, and welcome rapid development.In the aircraft of these new types, connecting wing The mentality of designing of body fusion, so that electric ducted fan becomes a very crucial components.Traditional ducted fan is one Kind is in the widely used Promoting Form of aviation field, with its propulsive efficiency is high, noise is small, inclusiveness is good, unit power thrust is big The advantages that, become the mainstream propulsion mode in present airliner.Electric ducted fan is that traditional duct wind is substituted using motor Aero-engine in fan can obtain faster system responsiveness, lower noise pollution, more flexible legacy system cloth It sets.
Electric ducted fan includes blade, duct and motor, in aero propulsion field, power to weight ratio (power and quality it Than) parameter that be one extremely important and sensitive, because the weight of electric ducted fan directly affects the weight of commercial load With the aerial flight mileage of aircraft.If necessary to improve the power to weight ratio of the motor of aviation, need to optimize in terms of three: (1) reinforce the heat dissipation of motor;(2) optimize the design of motor electromagnetic structure;(3) lightweight of structure.It, can in order to improve power to weight ratio To use two kinds of means, first is that cooling down using liquid hydrogen to motor, it both can sufficiently meet the radiating requirements of motor, while very It can extremely make motor work in the case where low-temperature superconducting;Two are an attempt to some electromagnetic design schemes, use such as switching magnetic-resistance electricity Machine, axial air-gap magneto, super conduction synchronous electric motor etc. are used as motor.But in small-sized aero propulsion field, excessively complicated Radiating mode and structure (such as oil is cold, liquid hydrogen is cooling) increase the weight of electric ducted fan, while bringing sealing etc. Integrity problem.So a kind of volume for reducing motor as far as possible becomes numerous researchs with the motor for realizing higher power to weight ratio The target of person.
The matched design of current ducted fan and motor is mainly carried out by power and the two indexs of revolving speed, so The check and inspection for carrying out temperature rise afterwards, make in aircraft operational process, the temperature rise on operating condition line meets the safety of motor It is required that.But there are two main problems for this design method: first is the design process coupling not by motor and ducted fan Close consider, especially wheel hub than this index, be in entire design process first it needs to be determined that and to blade and motor All very big parameter is influenced, such as influences the power to weight ratio of motor;Second is not account for motor in ducted fan design process Influence of the hot property (such as radiating requirements of motor) to design process, keep the power to weight ratio of motor not ideal enough.
Summary of the invention
In view of the existing technical defect, the purpose of the present invention is to provide a kind of thermal couplings of electric ducted fan to set Meter method, the design by the wheel hub of motor than incorporating ducted fan with radiating requirements, improves the power to weight ratio of motor in ducted fan.
To achieve the goals above, the present invention provides a kind of thermal coupling design methods of electric ducted fan, for setting Meter include fan blade, motor, duct ducted fan, the thermal coupling design method of the electric ducted fan includes step S1, S2, S3, S4, S5, S6, S7, S8, S9, S10 and S11.S1, examination take the wheel hub ratio r of ducted fan to be designed, according to giving Thrust requirements T under an operating condition of the fixed ducted fan to be designed in multi-state environment|rust, size requirements, ducted fan go out The blade tip Mach number of mouth parameter and ducted fan, estimation obtain the estimated efficiency of ducted fan under the operating condition and are calculated The axial velocity V of duct exit flowout, size requirements include the axial length L of ducted fanduct, ducted fan radius Rduct, ducted fan outlet parameter includes the ratio between exit flow sectional area and inlet air flow sectional area of ducted fan and duct The current density ρ of fan outlet, multi-state environment include multiple operating conditions;S2, according to the axial velocity V of duct exit flowout、 The radius R of ducted fanductAnd ducted fan outlet parameter, and according to the sharp disk of perfect gas theory, duct is calculated The performance parameter of fan, performance parameter include thrust T, power consumption P;S3, according to the wheel hub ratio r of ducted fan and the axial direction of motor Length Lmotor, the volume V of motor is calculatedmotor;S4, the electricity obtained according to the rotational speed omega of given motor and step S3 The volume V of machinemotor, the power P of motor is calculatedmotor;S5 just estimates the efficiency value η for obtaining motormotor;S6, according to motor Efficiency value ηmotorWith the power consumption P of ducted fan, the calorific value W of motor is calculatedH;According to the axial length L of motormotor、 The flow velocity of air-flow, is calculated motor case surface at known motor case surface area, casing surface temperature difference and casing Heat dissipation capacity WC;Whether the heat dissipation capacity on motor case surface obtained in S7, judgment step S6 is greater than the calorific value of motor, if it is not, Then follow the steps S8;If so, thening follow the steps S9;S8 examines the efficiency value η of motormotorWhether can improve, if so, increasing electricity Engine efficiency value ηmotorAnd return step S6, execute step S6-S7;If it is not, increasing the wheel hub ratio and return step of ducted fan S3 executes step S3-S7;S9 examines the power P of motormotorWhether redundancy is had, if so, reducing the wheel hub ratio of ducted fan And return step S3, step S3-S7 is executed, if it is not, the wheel hub ratio of the ducted fan under the operating condition, ducted fan are pushed away Power demand T|rust, thrust T substitute into fan design program and carry out fan blade design and simulation calculation, obtain the duct of Preliminary design Blade profile, performance data and the 3D simulation model of the fan blade of fan simultaneously execute step S10;Performance data includes ducted fan Actual efficiency, actual thrust;S10 gives an efficiency error amount and a thrust error value, judges the ducted fan of Preliminary design Actual efficiency it is whether excessively high, i.e., whether compared estimate is high-efficient and actual efficiency and estimated efficiency for the actual efficiency of ducted fan Whether difference is greater than efficiency error amount, if so, reducing the wheel hub ratio and return step S3 of ducted fan, executes step S3- S7, if it is not, judging whether the actual efficiency of the ducted fan of Preliminary design is too low, i.e., the actual efficiency compared estimate of ducted fan is imitated Rate is low and whether the absolute value of actual efficiency and the difference of estimated efficiency is greater than efficiency error amount, if so, increasing ducted fan Wheel hub ratio and return step S3 and execute step S3-S7, if it is not, judging the actual thrust of the ducted fan of Preliminary design is It is no excessively high, i.e., the actual thrust of ducted fan whether specific thrust demand T|rustHigh and actual thrust and thrust requirements T|rustDifference Whether value is greater than thrust error value, if so, reducing the wheel hub ratio and return step S3 of ducted fan, executes step S3-S7, If it is not, judge whether the actual thrust of the ducted fan of Preliminary design too low, i.e. the actual thrust specific thrust demand of ducted fan T|rustLow and actual thrust and thrust requirements T|rustDifference absolute value be greater than thrust error value, if so, increase duct wind The wheel hub ratio and return step S3 of fan, execute step S3-S7, if it is not, the actual efficiency and actual thrust of output ducted fan And execute step S11;S11, judges whether actual thrust of the ducted fan of Preliminary design under the operating condition is greater than ducted fan Thrust requirements under other operating conditions in given multi-state environment, if so, the fan of the ducted fan of output Preliminary design Blade profile, performance data and the 3D simulation model of blade, the final design result as the ducted fan for meeting all operating conditions;If It is no, using ducted fan in the thrust requirements under other operating conditions as the thrust requirements T in step S1|rust, return step S1, again Step S1-S7 is executed, until the actual thrust for the ducted fan that Preliminary design obtains is greater than remaining other works in multi-state environment Thrust requirements under condition, output meet the final design result of the ducted fan of all operating conditions.
In one embodiment, the value range of the wheel hub ratio r for the ducted fan that the examination in step S1 takes 0.2~0.4 it Between.
In one embodiment, the axial velocity V of the duct exit flow in step S1outCalculating process include step S111, S112 and S113.S111, according to the radius R of ducted fanductWith the wheel hub ratio r of ducted fan, pass through following formula:Wherein r indicates the wheel hub ratio of ducted fan, AinIndicate ducted fan enters implication Flow section product, is calculated the inlet air flow sectional area A of ducted fanin;S112, according to the inlet air flow sectional area of ducted fan AinThe ratio between with the exit flow sectional area of ducted fan and inlet air flow sectional area, the exit flow that ducted fan is calculated is cut Area Aout;S113, according to the exit flow sectional area A of ducted fanout, thrust requirements T|rustAnd the gas of ducted fan outlet Current density ρ, passes through following formula:Wherein ρ indicates the current density of ducted fan outlet, AoutIt indicates The axial velocity V of duct exit flow is calculated in the exit flow sectional area of ducted fanout
In one embodiment, the calculating process of the fan performance parameter in step S2 includes step S21, S22 and S23. S21, according to the current density ρ of ducted fan outlet, the exit flow sectional area A of ducted fanoutAnd duct exit flow Axial velocity Vout, pass through following formula: m=Vout·Aoutρ, wherein m indicates gas mass flow, and gas mass flow is calculated Measure m;S22, according to the axial velocity V of gas mass flow m and duct exit flowout, the thrust T of ducted fan is calculated =m × Vout;S23, according to working off one's feeling vent one's spleen for the thrust T of ducted fan, the current density ρ of ducted fan outlet and ducted fan Flow section accumulates Aout, the power consumption of ducted fan is calculated
In one embodiment, the volume V of the motor in step S3motorCalculating process are as follows: according to the wheel hub of ducted fan The radius R of ratio r and ducted fanduct, hub radius relationship, obtain hub radius, it is assumed that the half of hub radius and motor Diameter RmotorIt is identical, according to the axial length L of hub radius and motormotor, the volume V of motor is calculatedmotor
In one embodiment, the power P of the motor in step S4motorCalculating process are as follows: Pmotor=ω kτVmotor, Wherein, kτFor motor torque coefficient.
In one embodiment, the efficiency value η of motormotorValue range between 85%~90%.
In one embodiment, the calorific value W of the motor in step S6HCalculating process are as follows: WH=P/ ηmotor(1-ηmotor)。
In one embodiment, the heat dissipation capacity W on the motor case surface in step S6CCalculating process are as follows: WC=hA Δ T,In formula, h indicates that convection transfer rate, A indicate that motor case surface area, Δ T indicate casing surface The temperature difference, v indicate the flow velocity of air-flow at casing, and the flow velocity v of air-flow is by casing volumetric flow of gas and motor case table at casing The quotient of area obtains, at casing volumetric flow of gas by ducted fan exit flow sectional area AoutWith duct exit flow Axial velocity VoutProduct obtains.
Beneficial effects of the present invention are as follows:
In the thermal coupling design method of electric ducted fan of the invention, consider that wheel hub compares fan leaf in ducted fan The influence of the actual efficiency and actual thrust of piece and (heat dissipation capacity on motor case surface is greater than motor to the radiating requirements of motor Calorific value) and motor power influence, the design process by the wheel hub of motor than being integrated into ducted fan with radiating requirements In, it can make while the design result of ducted fan meets the requirement of multi-state environment, motor is made to meet heat dissipation need It asks (calorific value that the heat dissipation capacity on motor case surface is greater than motor) and makes the volume minimization of motor, to improve in ducted fan The power to weight ratio of motor.
Detailed description of the invention
Fig. 1 is the flow chart of the thermal coupling design method of electric ducted fan of the invention.
Fig. 2 is the schematic diagram of the ducted fan in the thermal coupling design method of electric ducted fan of the invention.
Wherein, the reference numerals are as follows:
1 fan blade
2 motors
3 ducts
Specific embodiment
Attached drawing shows the embodiment of the present invention, and will be appreciated that the disclosed embodiments are only example of the invention, The present invention can be implemented in a variety of manners, and therefore, detail disclosed herein is not necessarily to be construed as limiting, but only as power Basis that benefit requires and as the basis of representative for instructing those of ordinary skill in the art to implement the present invention in various ways.
It is described in detail the thermal coupling design method of electric ducted fan according to the present invention with reference to the accompanying drawings.
Referring to Figures 1 and 2, the thermal coupling design method of electric ducted fan of the invention includes fan blade for designing 1, the ducted fan of motor 2, duct 3, the thermal coupling design method of the electric ducted fan include step S1, S2, S3, S4, S5, S6, S7, S8, S9, S10 and S11.
S1, examination takes the wheel hub ratio r of ducted fan to be designed, according to given ducted fan to be designed in multi-state environment In an operating condition under thrust requirements T|rust, size requirements, ducted fan outlet parameter and ducted fan blade tip Mach number, Estimation obtains under the operating condition estimated efficiency of ducted fan and the axial velocity V of duct exit flow is calculatedout, size Demand includes the axial length L of ducted fanduct, ducted fan radius Rduct, ducted fan outlet parameter includes ducted fan Exit flow sectional area and the ratio between inlet air flow sectional area and the current density ρ of ducted fan outlet, multi-state environment packet Include multiple operating conditions.
Ducted fan is applied in aircraft in complicated multi-state environment, at the beginning of ducted fan design, need by Master-plan personnel determine each operating condition stage to the thrust requirements T of ducted fan according to aerial mission and flight envelope|rustAnd ruler Very little demand etc..Multiple operating conditions include take off operating condition, operating condition of climbing, decline operating condition and landing operating condition, under operating condition of taking off, duct The heat dissipation difficulty of fan is maximum, therefore preferably designs ducted fan under operating condition of taking off first.Before designing ducted fan, according to Given thrust requirements T of the ducted fan under all operating conditions is actually needed|rust, size requirements, ducted fan outlet parameter and The blade tip Mach number of ducted fan.The performance of ducted fan is tentatively understood by blade tip Mach number.The wheel hub ratio of ducted fan On the one hand value will consider the size that the motor 2 that wheel hub can accommodate waits, on the other hand to consider the thick of the blade root of fan blade 1 Degree should not be excessive.The wheel hub of fan than typically small, the wheel hub of ducted fan than generally can between 0.2~0.4 value.Contain The current density ρ of ducted fan outlet in road fan outlet parameter can be assumed that as the environmental density under corresponding operating condition.
The axial velocity V of duct exit flow in step S1outCalculating process include step S111, S112 and S113.S111, according to the radius R of ducted fanductWith the wheel hub ratio r of ducted fan, pass through following formula:Wherein r indicates the wheel hub ratio of ducted fan, AinIndicate the inlet air flow of ducted fan The inlet air flow sectional area A of ducted fan is calculated in sectional areain;S112, according to the inlet air flow sectional area of ducted fan AinThe ratio between with the exit flow sectional area of ducted fan and inlet air flow sectional area, the exit flow that ducted fan is calculated is cut Area Aout;S113, according to the exit flow sectional area A of ducted fanout, thrust requirements T|rustAnd the gas of ducted fan outlet Current density ρ, passes through following formula:Wherein ρ indicates the current density of ducted fan outlet, AoutIt indicates The axial velocity V of duct exit flow is calculated in the exit flow sectional area of ducted fanout
S2, according to the axial velocity V of duct exit flowout, ducted fan radius RductAnd ducted fan outlet ginseng Number, and according to the sharp disk of perfect gas theory, the performance parameter of ducted fan is calculated, performance parameter includes thrust T, power consumption P。
The calculating process of fan performance parameter in step S2 includes step S21, S22 and S23.S21, according to duct wind It is fanned out to the current density ρ of mouth, the exit flow sectional area A of ducted fanoutAnd the axial velocity V according to duct exit flowout, Pass through following formula: m=Vout·Aoutρ, wherein m indicates gas mass flow, and gas mass flow m is calculated;S22, according to The axial velocity V of gas mass flow m and duct exit flowout, thrust T=m × V of ducted fan is calculatedout;S23, According to the exit flow sectional area A of the thrust T of ducted fan, the current density ρ that ducted fan exports and ducted fanout, meter Calculation obtains the power consumption of ducted fan
Sharp disk theory in step S2, which refers to, thinks into a kind of sharp disk for wind energy conversion system (i.e. ducted fan), is mentioned by swashing disk Take wind energy, it is believed that sharp disk be it is incompressible, the flow by ducted fan is modeled and makes following hypothesis: 1) assume Mach number is low, so that flowing shows as incompressible fluid;2) it is constant to assume that the flowing outside ducted fan flow tube has Stagnation pressure (does not apply any effect) to it;3) assume stability of flow;(4) on swashing disk, it is assumed that pressure discontinuously changes, but Speed changes in a continuous manner.And assume that the internal-and external diameters such as ducted fan inlet and outlet design, so that gas can be obtained by modeling Mass flow m=ρ Adisk[(Vout+Vin)/2] and thrustWherein, VinEnter implication for duct The axial velocity of stream, AdiskIt indicates to swash disc area (area i.e. at fan blade 1), therefore is able to obtain duct wind by modeling The approximate formula of the gas mass flow m and thrust T of fan are respectively m=Vout·Aoutρ and T=m × Vout
S3, according to the axial length L of the wheel hub ratio r of ducted fan and motor 2motor, the volume of motor 2 is calculated Vmotor
The volume V of motor 2 in step S3motorCalculating process are as follows: according to the wheel hub ratio r of ducted fan and duct wind The radius R of fanduct, hub radius relationship, obtain hub radius, it is assumed that the radius R of hub radius and motor 2motorIt is identical, root According to the axial length L of hub radius and motor 2motor, the volume V of motor 2 is calculatedmotor.Wherein, motor 2 is assumed to be cylinder Body, so the outer diameter of motor is identical as the hub radius of motor, so according to the axial length L of hub radius and motor 2motorMeter Calculation obtains the volume V of motor 2motor
S4, according to the volume V for the motor 2 that the rotational speed omega of given motor 2 and step S3 obtainmotor, electricity is calculated The power P of machine 2motor
The power P of motor 2 in step S4motorCalculating process are as follows: Pmotor=ω kτVmotor, wherein kτFor motor Torque coefficient.In the case where motor 2 and fan blade 1 are direct-connected, the rotational speed omega of motor 2 and the revolving speed of ducted fan are identical.
S5 just estimates the efficiency value η for obtaining motor 2motor.The efficiency value η of motor 2motorRule of thumb estimation obtains, motor 2 It can be magneto, the efficiency of a kind of magneto is more close, then can just estimate the efficiency value η of motor 2motorValue range Between 85%~90%.S6, according to the efficiency value η of motor 2motorWith the power consumption P of ducted fan, the hair of motor 2 is calculated Heat WH;According to the axial length L of motor 2motor, known motor case surface area, gas at casing surface temperature difference and casing The heat dissipation capacity W on motor case surface is calculated in the flow velocity of streamC
The calorific value W of motor 2 in step S6HCalculating process are as follows: WH=P/ ηmotor(1-ηmotor)。
The heat dissipation capacity W on the motor case surface in step S6CCalculating process are as follows:
WC=hA Δ T,In formula, h indicates that convection transfer rate, A indicate motor case surface Product, Δ T indicate that casing surface temperature difference, v indicate the flow velocity of air-flow at casing, and the flow velocity v of air-flow is by casing gas body at casing Product flow and the quotient of motor case surface area obtain, at casing volumetric flow of gas by ducted fan exit flow sectional area AoutWith the axial velocity V of duct exit flowoutProduct obtains.Wherein, casing surface temperature difference Δ T is motor case surface highest The temperature difference between temperature and ambient air temperature, motor case hot face temperature can pass through the world according to the different brackets of motor Standard queries obtain.
Whether the heat dissipation capacity on motor case surface obtained in S7, judgment step S6 is greater than the calorific value of motor 2, if it is not, Then follow the steps S8;If so, thening follow the steps S9.
S8 examines the efficiency value η of motor 2motorWhether can improve, if so, increasing electric efficiency value ηmotorAnd return step S6 executes step S6-S7;If it is not, increasing the wheel hub ratio and return step S3 of ducted fan, step S3-S7 is executed.
S9 examines the power P of motor 2motorWhether redundancy is had, if so, reducing the wheel hub ratio of ducted fan and returning to step Rapid S3 executes step S3-S7, if it is not, by the thrust requirements of the wheel hub ratio of the ducted fan under the operating condition, ducted fan T|rust, thrust T substitutes into fan design program and carries out fan blade design and simulation calculation, the duct wind that output Preliminary design obtains Blade profile, performance data and the 3D simulation model of the fan blade 1 of fan simultaneously execute step S10;Performance data includes ducted fan Actual efficiency, actual thrust.
Fan design in step S9 has had the design method of various maturations in known technology.Electronic culvert of the invention Fan design program in the thermal coupling design method of road fan is used based on the fan write along the circular rectors design method such as leaf height It program is designed, to carry out ducted fan design, obtains the design result of fan blade 1, such as the fan blade 1 of ducted fan Blade profile, and according to the design result of fan blade 1, grid division, setting basin are carried out, such as NUMECA software, ANSYS are used The business fluid software for calculation of software carries out three-dimensional artificial calculating, to obtain the 3D simulation model and performance number of ducted fan It further include that volumetric flow of gas, stagnation pressure rise etc. according to, performance data other than including the actual efficiency of ducted fan, actual thrust The related data of ducted fan.The method that fan design program uses is not limited to based on along the circular rectors design method such as leaf height, fan Design program can also be used other fan design methods to realize.Step S7 to step S9 is by the heat dissipation of the motor 2 of ducted fan Demand and wheel hub compare fan blade 1 and the influence of motor 2 is fused to the process that ducted fan designs, so that ducted fan Motor 2 meets radiating requirements (calorific value that the heat dissipation capacity on motor case surface is greater than motor 2) and the power-efficient of motor utilizes, And by reducing wheel hub than come the volume that reduces motor 2 as far as possible, thus by making motor 2 meet radiating requirements and reduction The volume of motor 2 is to realize higher power to weight ratio.
S10 gives an efficiency error amount and a thrust error value, judges that the actual efficiency of the ducted fan of Preliminary design is No excessively high, i.e., whether compared estimate is high-efficient and whether actual efficiency and the difference of estimated efficiency are greater than for the actual efficiency of ducted fan Efficiency error amount executes step S3-S7 if so, reducing the wheel hub ratio and return step S3 of ducted fan, if it is not, judgement Whether the actual efficiency of the ducted fan of Preliminary design is too low, i.e. the actual efficiency compared estimate low efficiency of ducted fan and practical effect Whether the absolute value of rate and the difference of estimated efficiency is greater than efficiency error amount, if so, increasing the wheel hub ratio of ducted fan simultaneously Return step S3 simultaneously executes step S3-S7, if it is not, judging whether the actual thrust of the ducted fan of Preliminary design is excessively high, that is, contains The actual thrust of road fan whether specific thrust demand T|rustHigh and actual thrust and thrust requirements T|rustDifference whether be greater than and push away Power error amount executes step S3-S7 if so, reducing the wheel hub ratio and return step S3 of ducted fan, if it is not, judgement is just Whether the actual thrust for walking the ducted fan of design is too low, i.e. the actual thrust specific thrust demand T of ducted fan|rustIt is low and practical Thrust and thrust requirements T|rustDifference absolute value be greater than thrust error value, if so, increase ducted fan wheel hub ratio And return step S3, step S3-S7 is executed, if it is not, the actual efficiency of output ducted fan and actual thrust and executing step S11.Wherein, the value can be arranged according to specific design objective in efficiency error amount and thrust error value, efficiency error amount and push away here Power error amount can value be 2%.
After the blade profile, performance data and 3D simulation model of the fan blade 1 for the ducted fan for obtaining Preliminary design, need Judge the actual efficiency and actual thrust and estimated efficiency and thrust requirements T of the ducted fan of Preliminary design|rustWhether deviation It is excessive, if deviation is excessive, the leaf of the fan blade 1 of the ducted fan of Preliminary design is regenerated by adjusting wheel hub ratio Type, performance data and 3D simulation model.So as to embody importance of the wheel hub ratio in ducted fan design, it is also intended to The element that emphasis considers.
S11, judges whether actual thrust of the ducted fan of Preliminary design under the operating condition is greater than ducted fan given Multi-state environment in other operating conditions under thrust requirements, if so, output Preliminary design ducted fan fan blade (1) Blade profile, performance data and 3D simulation model, the final design result as the ducted fan for meeting all operating conditions;If it is not, Using ducted fan in the thrust requirements under other operating conditions as the thrust requirements T in step S1|rust, return step S1 holds again Row step S1-S7, until the actual thrust for the ducted fan that design obtains is greater than in multi-state environment under remaining other operating conditions Thrust requirements, output meet the final design result of the ducted fan of all operating conditions.
After design obtains the blade profile, performance data and 3D simulation model of the fan blade 1 of the ducted fan under the operating condition, Need to judge whether the ducted fan under the operating condition that design obtains is able to use under other operating conditions, so to judge tentatively to set It counts obtained ducted fan and whether is greater than its in given multi-state environment of ducted fan in the actual thrust under the operating condition Thrust requirements under its operating condition, if conditions are not met, it is of the invention to recirculate execution according to the thrust requirements under other operating conditions The step of thermal coupling design method of electric ducted fan, until obtaining the fan for the final ducted fan for meeting all operating conditions Blade profile, performance data and the 3D simulation model of blade 1.
In the thermal coupling design method of electric ducted fan of the invention, consider that wheel hub compares fan leaf in ducted fan The influence of the actual efficiency and actual thrust of piece 1 and (heat dissipation capacity on motor case surface is greater than electricity to the radiating requirements of motor 2 The calorific value of machine 2) and motor 2 power influence, the design by the wheel hub of motor 2 than being integrated into ducted fan with radiating requirements In the process, it can make while the design result of ducted fan meets the requirement of multi-state environment, meet motor 2 and dissipate Heat demand (calorific value that the heat dissipation capacity on motor case surface is greater than motor 2) and the volume minimization for making motor 2, to improve duct The power to weight ratio of motor 2 in fan.
Detailed description describes multiple exemplary embodiments above, but is not intended to be limited to clearly disclosed combination herein. Therefore, unless otherwise indicated, various features disclosed herein can be combined and be formed and not shown for clarity and Multiple other combinations out.
The foregoing is merely preferred embodiment of the present application, are not intended to limit this application, for the skill of this field For art personnel, various changes and changes are possible in this application.Within the spirit and principles of this application, made any to repair Change, equivalent replacement, improvement etc., should be included within the scope of protection of this application.

Claims (9)

1. a kind of thermal coupling design method of electric ducted fan includes fan blade (1), motor (2), duct for designing (3) ducted fan, which is characterized in that the thermal coupling design method of the electric ducted fan comprising steps of
S1, examination takes the wheel hub ratio r of ducted fan to be designed, according to given ducted fan to be designed in multi-state environment Thrust requirements T under one operating condition|rust, size requirements, ducted fan outlet parameter and ducted fan blade tip Mach number, estimation It obtains under the operating condition estimated efficiency of ducted fan and the axial velocity V of duct exit flow is calculatedout, size requirements Axial length L including ducted fanduct, ducted fan radius Rduct, ducted fan outlet parameter includes going out for ducted fan The ratio between implication flow section product and inlet air flow sectional area and the current density ρ of ducted fan outlet, multi-state environment include more A operating condition;
S2, according to the axial velocity V of duct exit flowout, ducted fan radius RductAnd ducted fan outlet parameter, and Sharp disk according to perfect gas is theoretical, the performance parameter of ducted fan is calculated, performance parameter includes thrust T, power consumption P;
S3, according to the axial length L of the wheel hub ratio r and motor (2) of ducted fanmotor, the volume of motor (2) is calculated Vmotor
S4, according to the volume V for the motor (2) that the rotational speed omega of given motor (2) and step S3 obtainmotor, electricity is calculated The power P of machine (2)motor
S5 just estimates to obtain the efficiency value η of motor (2)motor
S6, according to the efficiency value η of motor (2)motorWith the power consumption P of ducted fan, the calorific value W of motor (2) is calculatedH;Root According to the axial length L of motor (2)motor, known motor case surface area, at casing surface temperature difference and casing air-flow stream The heat dissipation capacity W on motor case surface is calculated in speedC
Whether the heat dissipation capacity on motor case surface obtained in S7, judgment step S6 is greater than the calorific value of motor (2), if it is not, then Execute step S8;If so, thening follow the steps S9;
S8 examines the efficiency value η of motor (2)motorWhether can improve, if so, increasing electric efficiency value ηmotorAnd return step S6, Execute step S6-S7;If it is not, increasing the wheel hub ratio and return step S3 of ducted fan, step S3-S7 is executed;
S9 examines the power P of motor (2)motorWhether redundancy is had, if so, reducing the wheel hub ratio and return step of ducted fan S3 executes step S3-S7, if it is not, by the thrust requirements of the wheel hub ratio of the ducted fan under the operating condition, ducted fan T|rust, thrust T substitute into fan design program and carry out fan blade design and simulation calculation, obtain the ducted fan of Preliminary design Blade profile, performance data and the 3D simulation model of fan blade (1) simultaneously execute step S10;Performance data includes ducted fan Actual efficiency, actual thrust;
S10 gives an efficiency error amount and a thrust error value, judge the ducted fan of Preliminary design actual efficiency whether mistake Whether compared estimate is high-efficient and whether actual efficiency and the difference of estimated efficiency are greater than efficiency for height, the i.e. actual efficiency of ducted fan Error amount executes step S3-S7 if so, reducing the wheel hub ratio and return step S3 of ducted fan, if it is not, judgement is preliminary Whether the actual efficiency of the ducted fan of design too low, i.e., the actual efficiency compared estimate low efficiency and actual efficiency of ducted fan with Whether the absolute value of the difference of estimated efficiency is greater than efficiency error amount, if so, increasing the wheel hub ratio of ducted fan and returning Step S3 simultaneously executes step S3-S7, if it is not, judge whether the actual thrust of the ducted fan of Preliminary design excessively high, i.e. duct wind The actual thrust of fan whether specific thrust demand T|rustHigh and actual thrust and thrust requirements T|rustDifference whether be greater than thrust mistake Difference executes step S3-S7 if so, reducing the wheel hub ratio and return step S3 of ducted fan, if it is not, judgement is tentatively set Whether the actual thrust of the ducted fan of meter is too low, i.e. the actual thrust specific thrust demand T of ducted fan|rustLow and actual thrust With thrust requirements T|rustDifference absolute value be greater than thrust error value, if so, increase ducted fan wheel hub ratio and return Step S3 is returned, step S3-S7 is executed, if it is not, the actual efficiency of output ducted fan and actual thrust and executing step S11;
It is more what is given to judge whether actual thrust of the ducted fan of Preliminary design under the operating condition is greater than ducted fan by S11 The thrust requirements under other operating conditions in work condition environment, if so, the leaf of the fan blade (1) of the ducted fan of output Preliminary design Type, performance data and 3D simulation model, the final design result as the ducted fan for meeting all operating conditions;If it is not, to contain Road fan is in the thrust requirements under other operating conditions as the thrust requirements T in step S1|rust, return step S1 re-executes step Rapid S1-S7, until the actual thrust for the ducted fan that Preliminary design obtains is greater than in multi-state environment under remaining other operating conditions Thrust requirements, output meet the final design result of the ducted fan of all operating conditions.
2. the thermal coupling design method of electric ducted fan according to claim 1, which is characterized in that the examination in step S1 The value range of the wheel hub ratio r of the ducted fan taken is between 0.2~0.4.
3. the thermal coupling design method of electric ducted fan according to claim 1, which is characterized in that the culvert in step S1 The axial velocity V of road exit flowoutCalculating process comprising steps of
S111, according to the radius R of ducted fanductWith the wheel hub ratio r of ducted fan, pass through following formula:Wherein r indicates the wheel hub ratio of ducted fan, AinIndicate ducted fan enters implication Flow section product, is calculated the inlet air flow sectional area A of ducted fanin
S112, according to the inlet air flow sectional area A of ducted faninIt is cut with the exit flow sectional area and inlet air flow of ducted fan The exit flow sectional area A of ducted fan is calculated in area ratioout
S113, according to the exit flow sectional area A of ducted fanout, thrust requirements T|rustAnd the air-flow of ducted fan outlet is close ρ is spent, following formula is passed through:Wherein ρ indicates the current density of ducted fan outlet, AoutIndicate duct The axial velocity V of duct exit flow is calculated in the exit flow sectional area of fanout
4. the thermal coupling design method of electric ducted fan according to claim 3, which is characterized in that the wind in step S2 Fan performance parameter calculating process comprising steps of
S21, according to the current density ρ of ducted fan outlet, the exit flow sectional area A of ducted fanoutAnd duct is worked off one's feeling vent one's spleen The axial velocity V of streamout, pass through following formula: m=Vout·Aoutρ, wherein m indicates gas mass flow, and gas matter is calculated Measure flow m;
S22, according to the axial velocity V of gas mass flow m and duct exit flowout, the thrust T of ducted fan is calculated =m × Vout
S23, according to the exit flow section of the thrust T of ducted fan, the current density ρ that ducted fan exports and ducted fan Product Aout, the power consumption of ducted fan is calculated
5. the thermal coupling design method of electric ducted fan according to claim 1, which is characterized in that the electricity in step S3 The volume V of machine (2)motorCalculating process are as follows:
According to the radius R of the wheel hub ratio r of ducted fan and ducted fanduct, hub radius relationship, obtain hub radius, it is false If the radius R of hub radius and motor (2)motorIt is identical, according to the axial length L of hub radius and motor (2)motor, calculate To the volume V of motor (2)motor
6. the thermal coupling design method of electric ducted fan according to claim 1, which is characterized in that the electricity in step S4 The power P of machine (2)motorCalculating process are as follows:
Pmotor=ω kτVmotor, wherein kτFor motor torque coefficient.
7. the thermal coupling design method of electric ducted fan according to claim 1, which is characterized in that the effect of motor (2) Rate value ηmotorValue range between 85%~90%.
8. the thermal coupling design method of electric ducted fan according to claim 1, which is characterized in that the electricity in step S6 The calorific value W of machine (2)HCalculating process are as follows: WH=P/ ηmotor(1-ηmotor)。
9. the thermal coupling design method of electric ducted fan according to claim 3, which is characterized in that the electricity in step S6 The heat dissipation capacity W on machine casing surfaceCCalculating process are as follows:
WC=hA Δ T,
In formula, h indicates that convection transfer rate, A indicate that motor case surface area, Δ T indicate that casing surface temperature difference, v indicate casing Locate the flow velocity of air-flow, the flow velocity v of air-flow is obtained by the quotient of casing volumetric flow of gas and motor case surface area at casing, machine At shell volumetric flow of gas by ducted fan exit flow sectional area AoutWith the axial velocity V of duct exit flowoutProduct It obtains.
CN201910403121.3A 2019-05-15 2019-05-15 Thermal coupling design method of electric ducted fan Active CN110162863B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201910403121.3A CN110162863B (en) 2019-05-15 2019-05-15 Thermal coupling design method of electric ducted fan

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201910403121.3A CN110162863B (en) 2019-05-15 2019-05-15 Thermal coupling design method of electric ducted fan

Publications (2)

Publication Number Publication Date
CN110162863A true CN110162863A (en) 2019-08-23
CN110162863B CN110162863B (en) 2021-07-13

Family

ID=67634882

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201910403121.3A Active CN110162863B (en) 2019-05-15 2019-05-15 Thermal coupling design method of electric ducted fan

Country Status (1)

Country Link
CN (1) CN110162863B (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202006875U (en) * 2011-01-21 2011-10-12 许群伟 Ducted fan
CN104675556A (en) * 2014-12-26 2015-06-03 南京航空航天大学 Large-bypass-ratio turbofan engine of vane tip jet driven fan
US20170300612A1 (en) * 2014-10-08 2017-10-19 Safran Aircraft Engines Method for modeling a blade of a non-ducted propeller
CN107315875A (en) * 2017-06-26 2017-11-03 南京航空航天大学 Separately it is vented three duct fanjet simulation models
CN107885891A (en) * 2016-09-29 2018-04-06 中国航发商用航空发动机有限责任公司 A kind of aero-engine overall performance optimization method
CN108518348A (en) * 2018-03-23 2018-09-11 北京航空航天大学 Model plane axis stream ducted fan design method
US20190048826A1 (en) * 2017-08-14 2019-02-14 Rolls-Royce Plc Gas turbine engine
JP2019064541A (en) * 2017-10-05 2019-04-25 国立研究開発法人宇宙航空研究開発機構 Ducted fan, multi-copter, vertical takeoff and landing aircraft, cpu cooling fan and radiator cooling fan

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN202006875U (en) * 2011-01-21 2011-10-12 许群伟 Ducted fan
US20170300612A1 (en) * 2014-10-08 2017-10-19 Safran Aircraft Engines Method for modeling a blade of a non-ducted propeller
CN104675556A (en) * 2014-12-26 2015-06-03 南京航空航天大学 Large-bypass-ratio turbofan engine of vane tip jet driven fan
CN107885891A (en) * 2016-09-29 2018-04-06 中国航发商用航空发动机有限责任公司 A kind of aero-engine overall performance optimization method
CN107315875A (en) * 2017-06-26 2017-11-03 南京航空航天大学 Separately it is vented three duct fanjet simulation models
US20190048826A1 (en) * 2017-08-14 2019-02-14 Rolls-Royce Plc Gas turbine engine
JP2019064541A (en) * 2017-10-05 2019-04-25 国立研究開発法人宇宙航空研究開発機構 Ducted fan, multi-copter, vertical takeoff and landing aircraft, cpu cooling fan and radiator cooling fan
CN108518348A (en) * 2018-03-23 2018-09-11 北京航空航天大学 Model plane axis stream ducted fan design method

Non-Patent Citations (6)

* Cited by examiner, † Cited by third party
Title
MILAN B. ŠEKULARAC: "EXPERIMENTAL DETERMINATION OF TUNNEL VENTILATION AXIAL DUCTED FAN PERFORMANCE", 《THERMAL SCIENCE》 *
YUZHI JIN 等: "Modeling of Ducted-Fan and Motor in an Electric Aircraft and a Preliminary Integrated Design", 《SAE INTERNATIONAL JOURNAL OF AEROSPACE》 *
丛伟: "涵道风扇的气动特性与优化研究", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》 *
刘晓锋 等: "某大涵道比风扇轮毂型线数值计算", 《航空发动机》 *
张金环 等: "大涵道比风扇叶片气动优化设计", 《航空动力学报》 *
贺卫晋: "非稳定工况下对旋风机噪声数值模拟及实验研究", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》 *

Also Published As

Publication number Publication date
CN110162863B (en) 2021-07-13

Similar Documents

Publication Publication Date Title
Holland et al. Rotor blade cooling in high pressure turbines
Plas et al. Performance of a boundary layer ingesting (BLI) propulsion system
Liu et al. Performance calculation and design of stratospheric propeller
Liu et al. Design of high altitude propeller using multilevel optimization
Fakhre et al. Helicopter mission analysis for a regenerated turboshaft
Liu et al. Three-dimensional integrated thermodynamic simulation for wing anti-icing system
Koch Design and performance calculations of a propeller for very high altitude flight
Kim et al. Small-scale airfoil aerodynamic efficiency improvement by surface temperature and heat transfer
CN110162863A (en) The thermal coupling design method of electric ducted fan
Mollahosseini et al. 3D unsteady multi-stage cfd analysis of combustor-turbine hot streak migration
CN106650081B (en) Impact-hot gas film combined type ice prevention structure design method
Lück et al. Propeller design and performance evaluation with partially prescribed velocity distribution
Zhang et al. Development of simulation tools for high fidelity analysis of compound rotorcraft
Rajagopalan et al. Detailed Aerodynamic Analysis of the RAH‐66 FANTAIL™ Using CFD
El-Okda et al. Design of a small horizontal axis wind turbine
Gundy-Burlet et al. Effects of radial location on the migration of hot streaks in a turbine
Dorney Numerical investigation of hot streak temperature ratio scaling effects
Sheen et al. Modeling of hovering intermeshing rotor using blade element momentum theory
Avital et al. Low Reynolds number proprotor aerodynamic performance improvement using the continuous surface curvature design approach
Beaumier et al. Applied CFD for analysing aerodynamic flows around helicopters
Li et al. Experimental and Numerical Investigation of Propeller Shape Effect on Aircraft Aerodynamic Performance.
Yang et al. Aerodynamic design of key components of the large-discharge axial fan at high altitude
Hanås et al. Off-design performance modelling of a propfan aero engine. An off-design performance evaluation of a notional engine design for future reductions in fuel consumption and emissions
Vouros et al. Impact of Boundary Layer Ingestion on the Performance of Propeller Systems for Hybrid Electric Aircraft
Dorange Study and Design of an Axial Fan

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant