TWI656352B - Fault detection device for rotating electric machine - Google Patents
Fault detection device for rotating electric machine Download PDFInfo
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- TWI656352B TWI656352B TW106127071A TW106127071A TWI656352B TW I656352 B TWI656352 B TW I656352B TW 106127071 A TW106127071 A TW 106127071A TW 106127071 A TW106127071 A TW 106127071A TW I656352 B TWI656352 B TW I656352B
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L3/00—Electric devices on electrically-propelled vehicles for safety purposes; Monitoring operating variables, e.g. speed, deceleration or energy consumption
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60L—PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES; SUPPLYING ELECTRIC POWER FOR AUXILIARY EQUIPMENT OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES IN GENERAL; MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES; MONITORING OPERATING VARIABLES OF ELECTRICALLY-PROPELLED VEHICLES; ELECTRIC SAFETY DEVICES FOR ELECTRICALLY-PROPELLED VEHICLES
- B60L50/00—Electric propulsion with power supplied within the vehicle
- B60L50/10—Electric propulsion with power supplied within the vehicle using propulsion power supplied by engine-driven generators, e.g. generators driven by combustion engines
- B60L50/16—Electric propulsion with power supplied within the vehicle using propulsion power supplied by engine-driven generators, e.g. generators driven by combustion engines with provision for separate direct mechanical propulsion
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60W—CONJOINT CONTROL OF VEHICLE SUB-UNITS OF DIFFERENT TYPE OR DIFFERENT FUNCTION; CONTROL SYSTEMS SPECIALLY ADAPTED FOR HYBRID VEHICLES; ROAD VEHICLE DRIVE CONTROL SYSTEMS FOR PURPOSES NOT RELATED TO THE CONTROL OF A PARTICULAR SUB-UNIT
- B60W10/00—Conjoint control of vehicle sub-units of different type or different function
- B60W10/04—Conjoint control of vehicle sub-units of different type or different function including control of propulsion units
- B60W10/08—Conjoint control of vehicle sub-units of different type or different function including control of propulsion units including control of electric propulsion units, e.g. motors or generators
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60W—CONJOINT CONTROL OF VEHICLE SUB-UNITS OF DIFFERENT TYPE OR DIFFERENT FUNCTION; CONTROL SYSTEMS SPECIALLY ADAPTED FOR HYBRID VEHICLES; ROAD VEHICLE DRIVE CONTROL SYSTEMS FOR PURPOSES NOT RELATED TO THE CONTROL OF A PARTICULAR SUB-UNIT
- B60W20/00—Control systems specially adapted for hybrid vehicles
- B60W20/50—Control strategies for responding to system failures, e.g. for fault diagnosis, failsafe operation or limp mode
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02D—CONTROLLING COMBUSTION ENGINES
- F02D29/00—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto
- F02D29/06—Controlling engines, such controlling being peculiar to the devices driven thereby, the devices being other than parts or accessories essential to engine operation, e.g. controlling of engines by signals external thereto peculiar to engines driving electric generators
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P27/00—Arrangements or methods for the control of AC motors characterised by the kind of supply voltage
- H02P27/04—Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using variable-frequency supply voltage, e.g. inverter or converter supply voltage
- H02P27/06—Arrangements or methods for the control of AC motors characterised by the kind of supply voltage using variable-frequency supply voltage, e.g. inverter or converter supply voltage using dc to ac converters or inverters
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02P—CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS; CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS
- H02P29/00—Arrangements for regulating or controlling electric motors, appropriate for both AC and DC motors
- H02P29/02—Providing protection against overload without automatic interruption of supply
- H02P29/024—Detecting a fault condition, e.g. short circuit, locked rotor, open circuit or loss of load
- H02P29/0241—Detecting a fault condition, e.g. short circuit, locked rotor, open circuit or loss of load the fault being an overvoltage
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Transportation (AREA)
- Power Engineering (AREA)
- Combustion & Propulsion (AREA)
- Chemical & Material Sciences (AREA)
- Sustainable Energy (AREA)
- Sustainable Development (AREA)
- Life Sciences & Earth Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- Automation & Control Theory (AREA)
- General Health & Medical Sciences (AREA)
- Biomedical Technology (AREA)
- Hybrid Electric Vehicles (AREA)
- Electric Propulsion And Braking For Vehicles (AREA)
- Control Of Eletrric Generators (AREA)
- Control Of Electric Motors In General (AREA)
- Control Of Ac Motors In General (AREA)
- Inverter Devices (AREA)
Abstract
故障檢測裝置(70)適用於系統(10、110),該系統(10、110)具備:旋轉電機(30、130),與引擎(20)連結成為可以傳遞動力;逆變器(50),在旋轉電機與直流電源(40)之間進行電力轉換;及相位控制部(60),依據引擎之運轉狀態對電力轉換時開啟/斷開逆變器之各相的相位進行控制。故障檢測裝置具備記憶部(71)及故障判定部(72)。記憶部中記憶著旋轉電機之正常時,電力轉換時依據引擎之運轉狀態進行控制的相位。故障判定部,係依據透過相位控制部進行控制的電力轉換時的相位,與記憶部所記憶的旋轉電機之正常時之電力轉換時的相位之間的乖離量,對旋轉電機之故障進行判定。The fault detection device (70) is applicable to a system (10, 110). The system (10, 110) includes: a rotating electric machine (30, 130), which is connected to the engine (20) to transmit power; an inverter (50), Power conversion is performed between the rotating electric machine and the DC power supply (40); and the phase control section (60) controls the phase of each phase of the inverter on / off during power conversion according to the operating state of the engine. The failure detection device includes a memory section (71) and a failure determination section (72). The memory section stores the phases of the rotating electric machine that are controlled according to the operating state of the engine during power conversion. The failure determination unit determines the failure of the rotating electric machine based on the deviation between the phase at the time of power conversion controlled by the phase control unit and the phase at the time of normal power conversion of the rotating electrical machine memorized by the memory unit.
Description
[0001] 本揭示關於旋轉電機之故障檢測技術。[0001] The present disclosure relates to fault detection technology for rotating electrical machines.
[0002] 例如專利文獻1揭示以下之故障檢測。交流馬達之輸出轉矩小於轉矩指令值之情況下,使矩形波電壓之電壓相位在事先決定的上限相位以下之範圍內增加。當電壓相位與上限相位在規定時間持續保持一致之情況下,檢測逆變器(Inverter)之異常。專利文獻1記載之技術中,係將上限相位事先設定為一定值。此乃因為,在交流馬達中,輸出轉矩成為最大的電壓相位係成為一定值。 [先前技術文獻] [專利文獻] [0003] [專利文獻1]特開2010-119268號公報[0002] For example, Patent Document 1 discloses the following failure detection. When the output torque of the AC motor is less than the torque command value, the voltage phase of the rectangular wave voltage is increased within a range below a predetermined upper limit phase. When the voltage phase and the upper limit phase are kept consistent for a predetermined time, the abnormality of the inverter is detected. In the technique described in Patent Document 1, the upper limit phase is set to a predetermined value in advance. This is because in the AC motor, the voltage phase system in which the output torque becomes maximum becomes a constant value. [Prior Art Document] [Patent Document] [0003] [Patent Document 1] JP 2010-119268
[發明所欲解決之課題] [0004] 但是,專利文獻1記載之技術中,若不是電壓相位與上限相位一致,而且,該狀態持續規定時間,則無法檢測出逆變器之異常。亦即,習知中,為了檢測逆變器之異常而具有規定時間。因此無法早期檢測出逆變器之異常,乃有改善之空間。 [0005] 本揭示提供可以早期、且正確地檢測故障的旋轉電機的故障檢測技術。 [解決課題之手段] [0006] 本揭示之技術之一態樣的故障檢測裝置具有以下之構成。 [0007] 本揭示之故障檢測裝置(70)適用於具備引擎(20)、旋轉電機(30、130)、直流電源(40)、逆變器(50)及相位控制部(60)的系統者。 旋轉電機,係與引擎連結成為可以傳遞動力。 逆變器,係在旋轉電機與直流電源之間進行電力轉換。 相位控制部,係依據引擎之運轉狀態對電力轉換時開啟(turn-on)/斷開(turn-off)逆變器之各相的相位進行控制。 故障檢測裝置具備記憶部(71)與故障判定部(72)。記憶部中記憶著在旋轉電機之正常時,電力轉換時依據引擎之運轉狀態進行控制的相位。 故障判定部,係依據通過相位控制部進行控制的電力轉換時的相位,與記憶部所記憶的旋轉電機之正常時之電力轉換時的相位之間的乖離量,對旋轉電機之故障進行判定。 [0008] 依據上述構成,本揭示之系統中,引擎與旋轉電機連結成為可以傳遞動力。因此例如可以藉由引擎之驅動力使旋轉電機發電,或藉由旋轉電機之驅動力來助推引擎之驅動力。又,藉由逆變器在旋轉電機與直流電源之間進行電力轉換。本揭示之系統中,係藉由相位控制部,依據引擎之運轉狀態,對電力轉換時開啟逆變器之各相的相位進行控制。 [0009] 此時,旋轉電機故障之情況下,通過逆變器的電力轉換時被控制的相位,會與正常時之相位呈現乖離。因此本揭示之故障檢測裝置中,依據通過相位控制部進行控制的電力轉換時的相位與記憶部所記憶的旋轉電機之正常時之電力轉換時的相位之乖離量,可以判定旋轉電機之故障。進一步,記憶部記憶著在旋轉電機之正常時,電力轉換時依據引擎之運轉狀態被控制的相位。因此本揭示之故障檢測裝置,可以反映引擎之運轉狀態,旋轉電機之故障進行判定,可以早期且正確地檢測出旋轉電機之故障。 [0010] 又,開啟/斷開逆變器之各相的相位,係包含對相位進行補正的補正量(控制量)。旋轉電機只要是進行發電及驅動之至少一方者即可。[Problems to be Solved by the Invention] 0004 [0004] However, in the technology described in Patent Document 1, unless the voltage phase and the upper limit phase agree, and the state continues for a predetermined time, an abnormality of the inverter cannot be detected. That is, conventionally, a predetermined period of time is required to detect an abnormality of the inverter. Therefore, the abnormality of the inverter cannot be detected early, and there is room for improvement. [0005] The present disclosure provides a fault detection technique for a rotating electric machine that can detect a fault early and correctly. [Means for Solving the Problems] [0006] A fault detection device according to one aspect of the technology of the present disclosure has the following configuration. [0007] The fault detection device (70) of the present disclosure is suitable for a system person having an engine (20), a rotating electric machine (30, 130), a DC power supply (40), an inverter (50), and a phase control unit (60) . The rotating electric machine is connected to the engine to transmit power. Inverter is used to convert power between rotating electric machine and DC power supply. The phase control unit controls the phase of each phase of the turn-on / turn-off inverter during power conversion according to the running state of the engine. The failure detection device includes a memory unit (71) and a failure determination unit (72). The memory section memorizes the phase that is controlled in accordance with the operating state of the engine during power conversion when the rotating electrical machine is normal. The failure determination unit determines the failure of the rotating electric machine based on the deviation between the phase at the time of power conversion controlled by the phase control unit and the phase at the time of normal power conversion of the rotating electric machine memorized by the memory unit. [0008] According to the above configuration, in the system of the present disclosure, the engine is connected to the rotating electric machine so as to transmit power. Therefore, for example, the rotating electric machine can be powered by the driving force of the engine, or the driving force of the engine can be boosted by the driving force of the rotating electric machine. In addition, the inverter performs power conversion between the rotating electrical machine and the DC power source. In the disclosed system, the phase control unit controls the phase of each phase of the inverter during power conversion according to the operating state of the engine. [0009] At this time, in the case of a rotating electrical machine failure, the phase that is controlled during the power conversion by the inverter will deviate from the normal phase. Therefore, in the fault detection device of the present disclosure, the failure of the rotating electric machine can be determined based on the deviation between the phase at the time of power conversion controlled by the phase control section and the phase at the time of normal power conversion of the rotating electrical machine memorized by the memory section. Furthermore, the memory unit memorizes the phase that is controlled in accordance with the operating state of the engine during power conversion when the rotating electric machine is normal. Therefore, the fault detection device disclosed in this disclosure can reflect the running state of the engine, determine the failure of the rotating electric machine, and detect the failure of the rotating electric machine early and correctly. [0010] The phase of each phase of the inverter is turned on / off, and includes a correction amount (control amount) for correcting the phase. The rotating electric machine may be at least one of generating power and driving.
[0012] 以下參照圖面詳細說明實施本揭示之技術之形態。 <第1實施形態> 本實施形態中說明將本揭示之技術適用於摩托車(車輛)等之系統的事例。 [0013] 如圖1之例示,系統10具備引擎20,MG(電動發電機,Motor Generator)30,直流電源40,逆變器50,電壓相位控制量運算部(以下稱為「控制量運算部」)60,故障檢測裝置70,1或複數個補機80等。 [0014] 引擎20藉由燃燒燃料來產生動力。引擎20例如可以採用汽油引擎、柴油引擎或其他引擎。 [0015] MG30係帶啟動器功能的發電機。本實施形態之MG30相當於三相旋轉電機。因此,本實施形態之MG30具備三相交流馬達及三相交流發電機之功能。MG30具備作為定子繞組的U相之繞組31、V相之繞組32及W相之繞組33。各相之繞組31、32、33之一端共通連接於中性點。MG30之轉子具備磁鐵。轉子直接連結於引擎20之曲柄軸。亦即,引擎20與MG30連結成為可以傳遞動力。於MG30安裝有對轉子之角度位置進行檢測的角度位置感測器36。 [0016] 直流電源40係由Pb電池、Li離子電池、NiH電池等形成的二次電池或電容器等。直流電源40之電壓Vdc由電壓感測器(未圖示)進行檢測。MG30之發電時,電壓感測器檢測MG30之發電電壓。 [0017] 在MG30與直流電源40之間連接有逆變器50。本實施形態之逆變器50係包含U相臂、V相臂及W相臂的三相逆變器。各相臂包含在直流電源40之正極與負極之間被串聯連接的2個開關元件。二極體相對於開關元件分別被逆並聯連接。開關元件之開啟/斷開(on/off)係由來自控制量運算部60之施加電壓Vu、Vv、Vw(施加電壓指令值)控制。又,施加電壓Vu、Vv、Vw係依據控制量運算部60所運算的電壓相位控制量被算出。各相臂連接於各相之繞組31、32、33之另一端。 [0018] 於直流電源40及逆變器50連接有1或複數個補機80。補機80例如包含車頭燈、調光開關、方向燈、剎車燈、喇叭(警笛機)等。又,調光開關係用於將車頭燈之光軸切換為向下(切換為遠距離光束與近距離光束)之開關。 [0019] 控制量運算部60及故障檢測裝置70係由具備CPU、ROM、RAM、I/O(輸出入介面)等的ECU構成。作為ECU例如可以採用MGECU、引擎ECU、混合ECU等。MGECU控制MG30。引擎ECU對引擎20進行控制。混合ECU係對MGECU及引擎ECU進行控制的上位之ECU。 [0020] 控制量運算部60被輸入與MG30之轉子直接連結的曲柄軸之旋轉速度Ne。對MG30之轉子之角度位置θ進行時間微分即可算出角速度ω。該角速度ω相當於與MG30之轉子直接連結的曲柄軸之旋轉速度(引擎20之旋轉速度)Ne。又,控制量運算部60被輸入藉由電壓感測器檢測出的電壓Vdc。 [0021] 本實施形態之控制量運算部60具備相位控制部,該相位控制部依據引擎20之運轉狀態對電力轉換時開啟/斷開逆變器50之各相的相位進行控制。控制量運算部60依據圖2之流程圖所例示的處理順序,執行電壓相位控制量之運算(執行電壓相位控制量之超前/滯後相位控制)。該一連串之處理係由控制量運算部60按照規定之週期重複執行。本實施形態中說明MG30執行發電之情況之例。具體而言,MG30執行發電之情況下,控制量運算部60將逆變器50之各相按照轉子之旋轉角度(電氣角度)重複設為180°之期間導通(on)、180°之期間斷開(off)。 [0022] 本實施形態之控制量運算部60係對電壓相位控制量設定初期值(步驟S11)。電壓相位控制量係施加電壓Vu、Vv、Vw相對於磁極位置感測器信號的超前相位量/滯後相位量。初期值係MG30正常時引擎20之怠速時之電壓相位控制量。亦即,初期值為怠速時之正常值。 [0023] 接著,控制量運算部60判定目標發電電壓是否高於現在之發電電壓(步驟S12)。目標發電電壓依據1個以上之補機80之動作狀態(補機80之電氣負載)被設定。例如動作的補機80之數目越多,電氣負載越大。因此,目標發電電壓設為較高。又,發電電壓由上述電壓感測器檢測出。 [0024] 控制量運算部60判定目標發電電壓高於現在之發電電壓之情況下(步驟S12:是),對滯後相位加算量進行運算(步驟S13)。滯後相位加算量係使施加電壓Vu、Vv、Vw之相位相對於磁極位置感測器信號滯後的量。本實施形態中,藉由將開關之相位設為滯後,可以增加發電量。又,本實施形態中,將目標發電電壓與現在之發電電壓之差ΔV(ΔV=目標發電電壓-現在之發電電壓),和滯後相位加算量間之關係事先設定於表格。亦即,本實施形態中,將差ΔV與滯後相位加算量間之對應關係建立成為映射數據(map data),並將該映射數據事先記憶於記憶控制量運算部60具備的記憶裝置。因此,控制量運算部60參照該表格並根據差ΔV運算出滯後相位加算量。又,該表格亦可以對應於引擎20之旋轉速度Ne被設定。 [0025] 接著,控制量運算部60將滯後相位加算量相加於步驟S11之處理所設定的電壓相位控制量,進行電壓相位控制量之運算(步驟S14)。控制量運算部60一度結束(結束)該一連串之處理。 [0026] 另一方面,當控制量運算部60判定目標發電電壓在現在之發電電壓以下之情況下(步驟S12:否),對超前相位加算量進行運算(步驟S15)。超前相位加算量係使施加電壓Vu、Vv、Vw之相位超前磁極位置感測器信號的量(相位角)。本實施形態中,藉由使開關之相位超前,據此可以減少發電量。又,本實施形態中,目標發電電壓與現在之發電電壓之差ΔV和超前相位加算量之關係,係事先被設定於表格。控制量運算部60參照該表格並根據差ΔV運算出超前相位加算量。又,該表格亦可以對應於引擎20之旋轉速度Ne進行設定。 [0027] 接著,控制量運算部60由步驟S11之處理所設定的電壓相位控制量減去超前相位加算量,算出電壓相位控制量(步驟S16)。控制量運算部60一度結束(結束)該一連串之處理。 [0028] 故障檢測裝置70具備記憶部71及故障判定部72。記憶部71為非揮發性之記憶體。記憶部71由ROM、可改寫的非揮發性記憶體、備份RAM等構成。在記憶部71記憶著MG30之正常時基於逆變器50的電力轉換時依據引擎20之運轉狀態進行控制的電壓相位(正常時之電壓相位控制量)。具體而言,如圖3之例示,在記憶部71中,將MG30正常時的電氣負載之大小與引擎20之旋轉速度Ne之快慢與逆變器50之電壓相位控制量之關係作為映射數據並記憶之。所記憶的數據係在MG30之正常時例如透過進行規定之實驗等而測定的值。映射數據係將電氣負載之值與引擎20之旋轉速度Ne之值與逆變器50之電壓相位控制量之值建立對應關聯。亦即用於表示引擎20之運轉狀態的資訊,係包含補機80之電氣負載與引擎20之旋轉速度Ne。又,記憶部71中係將後述的電壓相位控制量之乖離量及/或電壓相位控制量之乖離量相對於變化速度的故障判定臨限值(用於判定故障之基準值)作為數據並記憶之。 [0029] 圖3之例示關係係設想MG30執行發電之情況。例如電氣負載變大,而且引擎20之旋轉速度Ne越慢,逆變器50之電壓相位控制量為滯後相位。又,電壓相位控制量(電壓相位)針對U相、V相、W相之至少1個記憶亦可。 [0030] 故障判定部72依據圖4之流程圖之例示順序對MG30之故障進行檢測。該一連串之處理在MG30的發電時係透過故障判定部72按照規定之週期重複被執行。本實施形態中以MG30執行發電之情況為例進行說明。 [0031] 本實施形態之故障判定部72對現在之電壓相位控制量(實際之控制量)與該時之引擎20之運轉狀態所對應的正常時之電壓相位控制量(記憶部71之正常時數據)之乖離量進行運算(步驟S21)。正常時之電壓相位控制量,可以藉由參照記憶部71記憶的圖3之映射數據,讀出引擎20之現在之運轉狀態所對應的電壓相位控制量而取得。現在之電壓相位控制量係引擎20之現在之運轉狀態中使用於逆變器50之控制的電壓相位控制量,其可以由控制量運算部60輸入而取得。故障判定部72由現在之電壓相位控制量減去正常時之電壓相位控制量。據此,故障判定部72算出乖離量(乖離量=現在之電壓相位控制量-正常時之電壓相位控制量)。 [0032] 接著,故障判定部72判定步驟S21之處理所算出的乖離量是否大於故障判定臨限值(步驟S22)。故障判定臨限值(相當於規定量)被設定為MG30之正常時不會發生的規定之乖離量。當故障判定部72判定乖離量大於故障判定臨限值之情況下(步驟S22:是),確定MG30為異常(步驟S23)。亦即,故障判定部72判定MG30故障。具體而言,步驟S23之處理係將故障判定旗標設為高位準(1)。又,MG30之故障可以考慮是各相之繞組31、32、33之任一之斷線、短路等。故障判定部72一度結束(結束)該一連串之處理。 [0033] 另一方面,步驟S22之判定處理中,故障判定部72判定乖離量在故障判定臨限值以下之情況下(步驟S22:否),確定MG30無異常(步驟S24)。亦即,故障判定部72判定MG30無故障。具體而言,步驟S24之處理係將故障判定旗標設為低位準(0)。又,該情況下,故障判定部72對應於乖離量之大小而判定MG30存在異常之可能性,或暫時性判定MG30為異常亦可。故障判定部72一度結束(結束)該一連串之處理。 [0034] 圖5係本實施形態之故障檢測之一例的時序圖。 [0035] 在早於時刻t1之前,依據補機80之電氣負載計算此時之電壓相位控制量(實際之電壓相位控制量)。於該時序中,實際之電壓相位控制量與正常時之電壓相位控制量(正常時數據)一致。因此實際之電壓相位控制量與正常時之電壓相位控制量之乖離量大致為0。故障判定旗標被設定為低位準(0)。 [0036] 於時刻t1,例如假設MG30之U相之繞組31發生斷線。據此,現在之發電電壓變為較目標發電電壓低,滯後相位加算量增加。滯後相位加算量被加於電壓相位控制量之初期值,電壓相位控制量增加。其結果,實際之電壓相位控制量與正常時之電壓相位控制量之乖離量增加。 [0037] 之後,於時刻t2,實際之電壓相位控制量與正常時之電壓相位控制量之乖離量大於故障判定臨限值。據此,確定MG30異常。故障判定旗標被設定為on。 [0038] 以上詳述之本實施形態具有以下之優點。 [0039] MG30故障之情況下,逆變器50執行電力轉換時所控制的相位會與正常時之相位呈現乖離。因此本實施形態之故障檢測裝置70,係依據經由控制量運算部60控制的電力轉換時的相位與記憶部71中被建立關聯並記憶的MG30之正常時之電力轉換時的相位之間的乖離量,可以判定MG30之故障。進一步,在故障檢測裝置70之記憶部71中記憶著MG30之正常時執行電力轉換時依據引擎20之運轉狀態進行控制的相位。因此故障檢測裝置70可以反映引擎20之運轉狀態來判定MG30之故障,可以早期且正確地檢測出MG30之故障。 [0040] 本實施形態之故障檢測裝置70具有故障判定部72。當透過控制量運算部60控制的電力轉換時的相位與記憶部71所記憶的MG30之正常時之電力轉換時的相位之間之乖離量大於故障判定臨限值之情況下,故障判定部72判定MG30故障。據此,故障檢測裝置70可以簡易地檢測出MG30之故障。 [0041] MG30發電的發電電壓對應於引擎20之旋轉速度Ne而變化。因此電力轉換時用來設定逆變器50之各相成為開啟(導通)的相位,亦對應於引擎20之旋轉速度Ne而變化。於此,本實施形態之故障檢測裝置70之記憶部71,係將MG30之正常時電力轉換時被控制的相位與引擎20之旋轉速度Ne建立關聯並記憶之。據此,故障檢測裝置70可以反映引擎20之旋轉速度Ne,正確地判定MG30之故障。 [0042] MG30發電時之目標發電電壓係對應於補機80之電氣負載而變化。因此電力轉換時設定逆變器50之各相成為導通的相位亦對應於補機80之電氣負載而變化。於此,本實施形態之故障檢測裝置70之記憶部71中,係將MG30之正常時電力轉換時被控制的相位與補機80之電氣負載建立關聯並記憶。據此,故障檢測裝置70可以反映補機80之電氣負載,正確地判定MG30之故障。 [0043] 又,第1實施形態可以如下變更實施。 [0044] 第1實施形態之變形例中,當電力轉換時所控制的相位與MG30之正常時之相位之間的乖離量之變化速度大於故障判定臨限值之情況下(變化速度較正常時不會發生的速度快的情況下),故障判定部72判定MG30故障亦可。 [0045] 圖6表示第1實施形態之變形例中的故障檢測之處理順序的流程圖。故障判定部72針對藉由和圖4之步驟S21之處理同樣之方法所算出的乖離量之變化速度進行運算(步驟S31)。乖離量之變化速度例如可由這次算出的乖離量減去前次算出的乖離量而算出。接著,故障判定部72判定步驟S31之處理所算出的乖離量之變化速度是否大於故障判定臨限值(步驟S32)。和乖離量之變化速度相關的故障判定臨限值(相當於規定的變化速度),係設定為MG30之正常時不會發生的規定之變化速度。故障判定部72判定乖離量之變化速度大於故障判定臨限值之情況下(步驟S32:是)執行步驟S33之處理。另一方面,故障判定部72判定乖離量之變化速度在故障判定臨限值以下之情況下(步驟S32:否)下執行步驟S34之處理。又,步驟S33、S34之處理分別和圖4之步驟S23、S24之處理相同。 [0046] 圖7表示第1實施形態之變形例中的故障檢測之一例的時序圖。時刻t1為止之動作係和圖5相同。在較時刻t2之前的時刻t3,假設乖離量之變化速度變為大於故障判定臨限值。據此,確定MG30為異常。故障判定旗標被設定為on。依據上述構成,本變形例中,當電力轉換時所控制的相位與MG30之正常時之相位之間的乖離量,急速變大時,可以早期檢測出MG30之故障。 [0047] <第2實施形態> 以下,關於第2實施形態,以其和第1實施形態之差異點為中心進行說明。和第1實施形態相同之構件附加和第1實施形態相同之符號並省略說明。 [0048] 圖8表示本實施形態之系統110之概略的方塊圖。 [0049] MG130具備繞組31A、32A、33A之第1組及繞組31B、32B、33B之第2組。繞組31A、32A、33A(第1組之三相繞組)之捲繞數多於繞組31B、32B、33B(第2組之三相繞組)之捲繞數。MG130可以將連接於逆變器50的三相繞組(與U相、V相、W對應的各相之繞組)之組切換為第1組與第2組。具體而言,MG130具備切換部37、38、39。切換部37在繞組31A與繞組31B之間進行切換。切換部38在繞組32A與繞組32B之間進行切換。切換部39在繞組33A與繞組33B之間進行切換。切換部37、38、39之動作由繞組切換控制部(以下稱為「切換控制部」)65進行控制。 [0050] 切換控制部65,係和控制量運算部60及故障檢測裝置70同樣,例如由MGECU、引擎ECU、混合ECU等構成。MGECU對MG130進行控制。引擎ECU對引擎20進行控制。混合ECU係對MGECU及引擎ECU進行控制的上位之ECU。當引擎20之旋轉速度Ne較規定旋轉速度慢之情況下,切換控制部65使切換部37、38、39動作,將與逆變器50連接的三相繞組切換為繞組31A、32A、33A。具體而言,當引擎20之旋轉速度Ne較規定旋轉速度慢之情況下,切換部37、38、39分別由繞組31B、32B、33B(第2組)切換至繞組31A、32A、33A(第1組)。當引擎20之旋轉速度Ne較規定旋轉速度快之情況下,切換控制部65使切換部37、38、39動作,將與逆變器50連接的三相繞組切換為繞組31B、32B、33B。具體而言,當引擎20之旋轉速度Ne較規定旋轉速度快之情況下,切換部37、38、39分別由繞組31A、32A、33A(第1組)切換至繞組31B、32B、33B(第2組)。 [0051] 記憶部71將MG130之正常時透過逆變器50的電力轉換時依據引擎20之運轉狀態進行控制的電壓相位(正常時之電壓相位控制量),按照三相繞組之每一組進行記憶。具體而言,如圖10之例示般,記憶部71中係將MG130之正常時逆變器50中連接的繞組31A、32A、33A(第1組之三相繞組)之狀態中的電氣負載之大小與引擎20之旋轉速度Ne之快慢與逆變器50之電壓相位控制量之間的關係作為映射數據並記憶之。又,如圖11之例示般,記憶部71中係將MG130之正常時逆變器50中連接的繞組31B、32B、33B(第2組之三相繞組)之狀態中的電氣負載之大小與引擎20之旋轉速度Ne之快慢與逆變器50之電壓相位控制量之間的關係作為映射數據並記憶之。所記憶的數據係和第1實施形態同樣在MG130之正常時例如透過進行規定之實驗等所測定的值。映射數據諸係將電氣負載之值與引擎20之旋轉速度Ne之值與逆變器50之電壓相位控制量之值建立關聯對應。亦即,表示引擎運轉狀態的資訊,係包含補機80之電氣負載及引擎20之旋轉速度Ne。 [0052] 本實施形態中,故障判定部72如下確定執行圖4、6之例示的故障檢測處理時參照的正常時之電壓相位控制量。故障判定部72係對應於逆變器50所連接的三相繞組之組,從記憶部71所記憶的正常時之電壓相位控制量之數據之中確定參照數據。圖9係確定正常時之參照數據之處理順序的流程圖。該一連串之處理係由故障判定部72按照規定之週期重複執行。 [0053] 本實施形態之故障判定部72判定逆變器50所連接的三相繞組之組是否為切換前(步驟S41)。具體而言,故障判定部72判定三相繞組之組是否透過切換控制部65而由繞組31A、32A、33A(第1組)被切換為繞組31B、32B、33B(第2組)。當故障判定部72判定三相繞組之組為切換前之情況下(步驟S41:是),將三相繞組之組的參照數據確定為切換前之正常時之電壓相位控制量(步驟S42)。亦即,在步驟S41之判定為肯定之情況下,故障判定部72係將記憶著MG130之正常時與逆變器50連接的繞組31A、32A、33A(第1組之三相繞組)之狀態中的電氣負載之大小與引擎20之旋轉速度Ne之快慢與逆變器50之電壓相位控制量之間的關係之數據(參照圖10)確定為參照數據。之後,故障判定部72一度結束(結束)該一連串之處理。 [0054] 另一方面,在步驟S41之判定處理中,若故障判定部72判定三相繞組之組並非切換前之情況下(步驟S41:否),將三相繞組之組的參照數據確定為切換後之正常時之電壓相位控制量(步驟S43)。亦即,在步驟S41之判定為否定之情況下,故障判定部72將記憶著MG130之正常時逆變器50所連接的繞組31B、32B、33B(第2組之三相繞組)的狀態中的電氣負載之大小與引擎20之旋轉速度Ne之快慢與逆變器50之電壓相位控制量之關係的數據(參照圖11)確定為參照數據。之後,故障判定部72一度結束(結束)該一連串之處理。 [0055] 依據本實施形態,MG130具備繞組31A、32A、33A之第1組及繞組31B、32B、33B之第2組。MG130透過切換部37、38、39可以切換逆變器50所連接的三相繞組之組。於故障檢測裝置70之記憶部71按照三相繞組之每一組記憶著MG130之正常時逆變器50執行電力轉換時依據引擎20之運轉狀態進行控制的相位。故障檢測裝置70之故障判定部72,係對應於逆變器50所連接的三相繞組之組,從記憶部71所記憶的正常時之電壓相位控制量之數據之中,確定故障檢測處理時使用的參照數據。故障判定部72依據透過控制量運算部60控制的電力轉換時的相位與記憶部71所記憶的MG130之正常時之電力轉換時的相位之間的乖離量,來判定MG130之故障。據此,故障檢測裝置70可以按照MG130具備的三相繞組之每一組早期且正確地檢測出其之故障。 [0056] 又,第1及第2實施形態可以如下變更實施。 [0057] 第1及第2實施形態之變形例中,依據對引擎20之曲柄角進行檢測的曲柄角感測器之檢測值來運算引擎20之旋轉速度Ne亦可。又,作為顯示引擎20之運轉狀態的資訊,亦可以取代引擎20之旋轉速度Ne,改用對旋轉速度Ne進行運算處理後的值或引擎20具備的凸輪軸(未圖示)之旋轉速度等。 [0058] 第1實施形態之變形例中,故障判定部72自圖4之步驟S22或圖6之步驟S32之判定為肯定之時點起對計數器進行加算。故障判定部72以計數器值大於規定的計數器值為條件而確定MG30為異常。亦即,故障判定部72以圖4之步驟S22或圖6之步驟S32之判定在規定時間內為肯定作為條件而確定MG30為異常亦可。第2實施形態中,執行圖4、6之例示的故障檢測處理時參照的正常時之電壓相位控制量之數據,係對應於逆變器50所連接的三相繞組之組被切換。於此,第2實施形態之變形例中,故障判定部72按照三相繞組之每一組設定計數器亦可。依據此一構成,故障判定部72即使在計數器的計數中逆變器50所連接的三相繞組之組被切換之情況下,計數器值亦可以保持於切換前之計數器中。故障判定部72可以依據三相繞組之各組之計數器的計數器值檢測出三相繞組之每一組之斷線等。 [0059] 第1及第2實施形態中說明在MG30或MG130執行發電之情況下檢測MG30或MG130之故障的例。相對於此,本變形例中,透過直流電源40所供給的電力,由MG30或MG130來助推引擎20之驅動力之情況下,對MG30或MG130之故障進行檢測亦可。亦即,MG30或MG130執行驅動(動力運轉)之情況下,對MG30或MG130之故障進行檢測亦可。該情況下,作為圖2之超前/滯後相位控制之取代,控制量運算部60改為執行基於目標驅動轉矩的電壓相位控制量之超前/滯後相位控制。具體而言,MG30執行驅動之情況下,控制量運算部60將逆變器50之各相按轉子之旋轉角度(電氣角度)重複設為180°之期間導通(on)、180°之期間斷開(off)。稱呼此種控制為矩形波電壓控制。又,作為矩形波電壓控制之取代,控制量運算部60亦可以使用在轉子之旋轉角度(電氣角度)180°之間重複導通/斷開的正弦波驅動控制、過調變驅動控制或導通期間(on-period)為120°的120度通電控制。在目標驅動轉矩大於現在之MG30之驅動轉矩之情況下,控制量運算部60使電壓相位控制量成為超前相位。又,在目標驅動轉矩小於現在之MG30之驅動轉矩之情況下,控制量運算部60使電壓相位控制量成為滯後相位。又,本變形例中,事先測定以圖3之電氣負載取代電源電壓,以滯後相位量取代超前相位量而得之關係,並將測定結果記憶。控制量運算部60使用該測定結果執行圖4及圖6之至少一方之故障檢測處理亦可。 [0060] 馬達之轉矩T可由T=p・Φ・iq之計算式算出。p係磁極對數,Φ係感應電壓常數,iq係q軸電流。p、Φ為固定值。因此,轉矩T可以使用iq簡單地算出。iq可以透過參照根據電壓相位控制量、電源電壓、馬達旋轉速度而被事先設定的映射數據來取得。 [0061] 使用圖12之流程圖具體說明本變形例中的電壓相位控制量之超前/滯後相位控制。本變形例之控制量運算部60對電壓相位控制量設定初期值(步驟S51)。初期值係MG30或MG130之正常時之引擎20之怠速時的電壓相位控制量(怠速時之正常值)。 [0062] 接著,控制量運算部60判定目標轉矩是否大於現在之轉矩(步驟S52)。控制量運算部60判定目標轉矩大於現在之轉矩之情況下(步驟S52:是),運算超前相位加算量(步驟S53)。超前相位加算量係使施加電壓Vu、Vv、Vw之相位超前磁極位置感測器信號之相位的量。本變形例中,將目標轉矩與現在之轉矩之差ΔT(ΔT=目標轉矩-現在轉矩)和超前相位加算量之間的關係事先設定於表格。亦即,本實施形態中,將設定有差ΔT與超前相位加算量之對應關係的映射數據,事先記憶於控制量運算部60所具備的記憶裝置。因此,控制量運算部60參照該表格並依據差ΔT來運算超前相位加算量。又,該表格可以對應於引擎20之旋轉速度Ne而設定。 [0063] 接著,控制量運算部60將超前相位加算量相加於步驟S51之處理所設定的電壓相位控制量,計算電壓相位控制量(步驟S54)。控制量運算部60一度結束(結束)該一連串之處理。 [0064] 另一方面,當控制量運算部60判定目標轉矩在現在之轉矩以下之情況下(步驟S52:否),算出滯後相位加算量(步驟S55)。滯後相位加算量係使施加電壓Vu、Vv、Vw之相位滯後磁極位置感測器信號之相位的量。本變形例中,目標轉矩與現在之轉矩之差ΔT和滯後相位加算量之間之關係被事先記憶於表格。控制量運算部60參照該表格並依據差ΔT算出滯後相位加算量。又,該表格可以對應於引擎20之旋轉速度Ne被設定。 [0065] 接著,控制量運算部60由步驟S51之處理所設定的電壓相位控制量減去滯後相位加算量,算出電壓相位控制量(步驟S56)。控制量運算部60一度結束(結束)該一連串之處理。 [0066] 如以上之說明,本變形例中設想MG30或MG130執行驅動(動力運轉)之情況。該情況下,電源電壓低、而且,引擎20之旋轉速度Ne越快,逆變器50之電壓相位控制量越是超前。 [0067] 和MG30或MG130執行發電之情況同樣,本變形例中,故障檢測裝置70之故障判定部72依據圖4或圖6之流程圖之例示的處理順序對MG30或MG130之故障進行檢測。 [0068] 例如假設MG30之U相之繞組31發生斷線。據此,現在之轉矩變為小於目標轉矩,超前相位加算量增加。於此,超前相位加算量被加算於電壓相位控制量之初期值,電壓相位控制量增加。結果,實際之電壓相位控制量與正常時之電壓相位控制量之間的乖離量呈現增加。之後,實際之電壓相位控制量與正常時之電壓相位控制量之間的乖離量變為大於故障判定臨限值。據此,確定MG30為異常。故障判定旗標被設定為高位準(1)。 [0069] 三相旋轉電機執行發電時對三相旋轉電機之故障進行檢測的情況下,作為三相旋轉電機可以採用MG或交流發電機(alternator)。又,三相旋轉電機執行驅動(動力運轉)時對三相旋轉電機之故障進行檢測的情況下,三相旋轉電機可以採用MG或馬達。 [0070] 以上,說明本揭示之技術之實施形態,但本揭示之技術不限定於上述實施形態。本揭示之技術在不脫離本揭示之要旨之範圍內適用於各種之實施形態。 [0071] 例如作為其他實施形態[1],當現在之電壓相位控制量與正常時之電壓相位控制量之間的乖離量大於故障判定臨限值(規定量)之情況下,故障判定部72對MG30之故障判定進行暫時判定並一度保留。接著,當電力轉換時所控制的相位與MG30之正常時之相位之間的乖離量之變化速度變為大於故障判定臨限值(規定速度)時,故障判定部72判定MG30為真故障亦可。 [0072] 記憶部71中記憶著MG30之正常時基於逆變器50的電力轉換時依據引擎20之運轉狀態被控制的電壓相位,和該電壓相位之變化速度。 [0073] 其他實施形態[1]中,依據該記憶部71所記憶的電壓相位及電壓相位之變化速度來確定上述故障判定臨限值。上述判定係依據圖4及圖6例示的流程圖之處理順序被執行。 [0074] 又,作為其他實施形態[2],故障判定部72可以將上述其他實施形態[1]之暫時判定與真判定之執行順序相反。亦即,當乖離量之變化速度大於故障判定臨限值之情況下,故障判定部72將MG30之故障判定設為暫時判定並一度保留。當現在之電壓相位控制量與正常時之電壓相位控制量之間的乖離量大於故障判定臨限值時,故障判定部72判定MG30之故障為真故障亦可。 [0075] 其他實施形態[2]中,當乖離量之變化速度變大,瞬間大於故障判定臨限值時,故障判定部72並不立即確定MG30為異常。當現在之電壓相位控制量與正常時之電壓相位控制量之間的乖離量變為大於故障判定臨限值時,故障判定部72判定MG30之故障為真故障。因此,其他實施形態[2]中,可以進行更高精度的故障判定。 [0076] 據此,其他實施形態[2]中,可以抑制對乘客傳遞非故意性的異常,可以正確地檢測出旋轉電機之故障。[0012] The form of implementing the technology of the present disclosure will be described in detail below with reference to the drawings. <First Embodiment> This embodiment describes an example in which the technology of the present disclosure is applied to a system such as a motorcycle (vehicle). [0013] As illustrated in FIG. 1, the system 10 includes an engine 20, an MG (Motor Generator) 30, a DC power source 40, an inverter 50, a voltage phase control amount calculation unit (hereinafter referred to as a "control amount calculation unit" ") 60, fault detection device 70, 1 or a plurality of supplementary machines 80, etc. [0014] The engine 20 generates power by burning fuel. The engine 20 may be, for example, a gasoline engine, a diesel engine, or another engine. [0015] MG30 is a generator with starter function. The MG30 in this embodiment is equivalent to a three-phase rotary electric machine. Therefore, the MG30 of this embodiment has the functions of a three-phase AC motor and a three-phase AC generator. The MG 30 includes a U-phase winding 31, a V-phase winding 32, and a W-phase winding 33 as stator windings. One end of the windings 31, 32, and 33 of each phase is connected to the neutral point in common. The rotor of MG30 is equipped with a magnet. The rotor is directly connected to a crank shaft of the engine 20. That is, the engine 20 and the MG30 are connected so that power can be transmitted. An angular position sensor 36 that detects the angular position of the rotor is mounted on the MG 30. [0016] The DC power source 40 is a secondary battery or a capacitor formed of a Pb battery, a Li-ion battery, a NiH battery, or the like. The voltage Vdc of the DC power source 40 is detected by a voltage sensor (not shown). When the MG30 generates power, the voltage sensor detects the MG30's power generation voltage. [0017] An inverter 50 is connected between the MG 30 and the DC power source 40. The inverter 50 of this embodiment is a three-phase inverter including a U-phase arm, a V-phase arm, and a W-phase arm. Each phase arm includes two switching elements connected in series between a positive electrode and a negative electrode of the DC power source 40. The diodes are connected in antiparallel to the switching elements, respectively. The on / off of the switching element is controlled by the applied voltages Vu, Vv, and Vw (applied voltage command values) from the control amount calculation section 60. The applied voltages Vu, Vv, and Vw are calculated based on the voltage phase control amounts calculated by the control amount calculation section 60. Each phase arm is connected to the other ends of the windings 31, 32, 33 of each phase. [0018] The DC power source 40 and the inverter 50 are connected with one or more supplementary machines 80. The supplementary machine 80 includes, for example, a headlight, a dimmer switch, a turn signal, a brake light, a horn (siren), and the like. In addition, the dimming on relationship is used to switch the optical axis of the headlight to a downward direction (switching to a long distance beam and a short distance beam). [0019] The control amount calculation unit 60 and the failure detection device 70 are configured by an ECU including a CPU, a ROM, a RAM, an I / O (input / output interface), and the like. Examples of the ECU include MGECU, engine ECU, and hybrid ECU. MGECU controls MG30. The engine ECU controls the engine 20. Hybrid ECU is a higher-level ECU that controls MGECU and engine ECU. [0020] The control amount calculation unit 60 is input with the rotation speed Ne of the crank shaft directly connected to the rotor of the MG 30. The angular velocity ω can be calculated by time-differentiating the angular position θ of the rotor of MG30. This angular velocity ω corresponds to the rotation speed (the rotation speed of the engine 20) Ne of the crank shaft directly connected to the rotor of the MG30. The control amount calculation unit 60 receives a voltage Vdc detected by the voltage sensor. [0021] The control amount calculation unit 60 of this embodiment includes a phase control unit that controls the phase of each phase of the inverter 50 on / off during power conversion according to the operating state of the engine 20. The control amount calculation unit 60 executes the calculation of the voltage phase control amount (performs the lead / lag phase control of the voltage phase control amount) according to the processing sequence illustrated in the flowchart of FIG. 2. This series of processing is repeatedly executed by the control amount calculation unit 60 at a predetermined cycle. In this embodiment, an example of a case where MG30 performs power generation will be described. Specifically, in the case where MG30 performs power generation, the control amount calculation unit 60 repeatedly sets each phase of the inverter 50 according to the rotation angle (electrical angle) of the rotor to be turned on during 180 ° and turned off during 180 ° Off. [0022] The control amount calculation unit 60 of this embodiment sets an initial value for the voltage phase control amount (step S11). The voltage phase control amount is a lead phase amount / lag phase amount of the applied voltages Vu, Vv, and Vw relative to the magnetic pole position sensor signal. The initial value is the voltage phase control amount at the idle speed of the engine 20 when the MG30 is normal. That is, the initial value is a normal value at idle. [0023] Next, the control amount calculation unit 60 determines whether the target power generation voltage is higher than the current power generation voltage (step S12). The target power generation voltage is set according to the operation state of one or more supplementary machines 80 (electrical load of the supplementary machine 80). For example, the greater the number of supplementary machines 80 in operation, the greater the electrical load. Therefore, the target power generation voltage is set to be high. The generated voltage is detected by the voltage sensor. [0024] When the control amount calculation unit 60 determines that the target power generation voltage is higher than the current power generation voltage (step S12: YES), it calculates the lag phase addition amount (step S13). The hysteresis phase addition amount is an amount that lags the phases of the applied voltages Vu, Vv, and Vw with respect to the signal of the magnetic pole position sensor. In this embodiment, by setting the phase of the switch to lag, the amount of power generation can be increased. In the present embodiment, the relationship between the difference ΔV between the target power generation voltage and the current power generation voltage (ΔV = target power generation voltage-current power generation voltage) and the lag phase addition amount is set in advance in a table. That is, in this embodiment, the correspondence between the difference ΔV and the lag phase addition amount is established as map data, and the map data is stored in advance in a memory device provided in the memory control amount calculation unit 60. Therefore, the control amount calculation unit 60 refers to the table and calculates the lag phase addition amount based on the difference ΔV. The table may be set in accordance with the rotation speed Ne of the engine 20. [0025] Next, the control amount calculation unit 60 adds the lag phase addition amount to the voltage phase control amount set in the process of step S11, and calculates the voltage phase control amount (step S14). The control amount calculation unit 60 once ends (ends) this series of processing. [0026] On the other hand, when the control amount calculation unit 60 determines that the target power generation voltage is lower than the current power generation voltage (step S12: No), it calculates the leading phase addition amount (step S15). The advanced phase addition amount is an amount (phase angle) that advances the phases of the applied voltages Vu, Vv, and Vw to the signals of the magnetic pole position sensor. In this embodiment, the amount of power generation can be reduced by advancing the phase of the switch. In addition, in this embodiment, the relationship between the difference ΔV between the target power generation voltage and the current power generation voltage and the leading phase addition amount is set in the table in advance. The control amount calculation unit 60 refers to this table and calculates the advanced phase addition amount based on the difference ΔV. The table may be set in accordance with the rotation speed Ne of the engine 20. [0027] Next, the control amount calculation unit 60 calculates the voltage phase control amount by subtracting the advanced phase addition amount from the voltage phase control amount set in the process of step S11 (step S16). The control amount calculation unit 60 once ends (ends) this series of processing. [0028] The failure detection device 70 includes a memory section 71 and a failure determination section 72. The memory section 71 is a non-volatile memory. The storage unit 71 is composed of a ROM, a rewritable nonvolatile memory, a backup RAM, and the like. The memory section 71 stores a voltage phase (a voltage phase control amount in a normal state) that is controlled based on the operating state of the engine 20 during power conversion of the inverter 50 when the MG 30 is normal. Specifically, as shown in the example of FIG. 3, in the memory section 71, the relationship between the magnitude of the electrical load when the MG30 is normal, the speed of the engine 20, the speed of rotation Ne, and the voltage phase control amount of the inverter 50 is used as mapping data and Remember it. The memorized data is a value measured by, for example, performing a predetermined experiment or the like when the MG30 is normal. The mapping data associates the value of the electrical load with the value of the rotation speed Ne of the engine 20 and the value of the voltage phase control amount of the inverter 50 in correspondence. That is, the information used to indicate the operating state of the engine 20 includes the electrical load of the supplementary machine 80 and the rotation speed Ne of the engine 20. In the memory unit 71, a failure determination threshold value (a reference value for determining a failure) of a deviation amount of the voltage phase control amount and / or a deviation amount of the voltage phase control amount with respect to a speed of change described later is used as data and memorized. Of it. [0029] The exemplary relationship of FIG. 3 is a case where the MG30 performs power generation. For example, as the electrical load becomes larger and the rotation speed Ne of the engine 20 becomes slower, the voltage phase control amount of the inverter 50 becomes a lag phase. The voltage phase control amount (voltage phase) may be stored in at least one of the U-phase, V-phase, and W-phase. [0030] The failure determination unit 72 detects a failure of the MG 30 according to the sequence illustrated in the flowchart of FIG. 4. This series of processes is repeatedly executed by the failure determination unit 72 at a predetermined cycle when the MG 30 generates power. In this embodiment, a case where MG30 performs power generation is described as an example. [0031] The fault determination unit 72 of this embodiment controls the voltage phase control amount in the normal state (the normal time in the memory section 71 when the current voltage phase control amount (actual control amount) corresponds to the running state of the engine 20 at that time. Data) is calculated (step S21). The voltage phase control amount in the normal state can be obtained by reading the voltage phase control amount corresponding to the current operating state of the engine 20 by referring to the map data of FIG. 3 stored in the memory section 71. The current voltage phase control amount is a voltage phase control amount used for the control of the inverter 50 in the current operating state of the engine 20, and it can be obtained by input from the control amount calculation section 60. The failure determination unit 72 subtracts the voltage phase control amount in the normal state from the current voltage phase control amount. Based on this, the failure determination unit 72 calculates the amount of deviation (amount of deviation = current voltage phase control amount-normal voltage phase control amount). [0032] Next, the failure determination unit 72 determines whether the deviation amount calculated in the process of step S21 is greater than the failure determination threshold value (step S22). The failure judgment threshold (equivalent to a prescribed amount) is set to a prescribed deviation amount that does not occur during normal MG30. When the failure determination unit 72 determines that the amount of deviation is larger than the failure determination threshold (step S22: YES), it is determined that the MG 30 is abnormal (step S23). That is, the failure determination unit 72 determines that the MG 30 has failed. Specifically, the process of step S23 sets the failure determination flag to a high level (1). In addition, the failure of MG30 can be considered as a disconnection or short circuit of any of the windings 31, 32, and 33 of each phase. The failure determination unit 72 once ends (ends) this series of processing. [0033] On the other hand, in the determination processing of step S22, the failure determination unit 72 determines that the deviation amount is below the failure determination threshold (step S22: No), and determines that there is no abnormality in MG30 (step S24). That is, the failure determination unit 72 determines that the MG 30 is not broken. Specifically, the processing of step S24 is to set the failure determination flag to a low level (0). In this case, the failure determination unit 72 may determine that there is a possibility that the MG30 is abnormal depending on the magnitude of the deviation, or temporarily determine that the MG30 is abnormal. The failure determination unit 72 once ends (ends) this series of processing. [0034] FIG. 5 is a sequence diagram of an example of fault detection in this embodiment. [0035] Prior to time t1, the voltage phase control amount (actual voltage phase control amount) at this time is calculated according to the electrical load of the supplementary machine 80. In this sequence, the actual voltage phase control amount is the same as the voltage phase control amount (normal time data) during normal time. Therefore, the deviation between the actual voltage phase control amount and the normal voltage phase control amount is approximately 0. The fault determination flag is set to a low level (0). [0036] At time t1, for example, suppose that the U-phase winding 31 of MG30 is disconnected. Based on this, the current generation voltage becomes lower than the target generation voltage, and the amount of lag phase addition increases. The lag phase addition amount is added to the initial value of the voltage phase control amount, and the voltage phase control amount increases. As a result, the deviation between the actual voltage phase control amount and the normal voltage phase control amount increases. [0037] After that, at time t2, the deviation between the actual voltage phase control amount and the normal voltage phase control amount is greater than the fault determination threshold. Based on this, it is determined that the MG30 is abnormal. The failure determination flag is set to on. [0038] The embodiment described above has the following advantages. [0039] In the case of an MG30 failure, the phase controlled by the inverter 50 when performing power conversion will deviate from the normal phase. Therefore, the fault detection device 70 of the present embodiment is based on the deviation between the phase at the time of power conversion controlled by the control amount calculation unit 60 and the phase at the time of normal power conversion of the MG 30 that is associated and memorized in the memory 71 Can determine the failure of MG30. Further, the memory section 71 of the fault detection device 70 stores a phase that is controlled in accordance with the operating state of the engine 20 when power conversion is performed when the MG 30 is normal. Therefore, the fault detection device 70 can reflect the running state of the engine 20 to determine the fault of the MG30, and can detect the fault of the MG30 early and correctly. [0040] The failure detection device 70 of this embodiment includes a failure determination unit 72. When the amount of deviation between the phase at the time of power conversion controlled by the control amount calculation section 60 and the phase at the time of normal power conversion of the MG 30 memorized by the memory section 71 is greater than the failure determination threshold, the failure determination section 72 Determined that MG30 is faulty. Accordingly, the failure detection device 70 can easily detect a failure of the MG30. [0041] The power generation voltage generated by the MG30 varies according to the rotation speed Ne of the engine 20. Therefore, the phase for setting each phase of the inverter 50 to ON (conducting) during power conversion also changes in accordance with the rotation speed Ne of the engine 20. Here, the memory section 71 of the fault detection device 70 of this embodiment associates and memorizes the phase controlled during the normal power conversion of the MG 30 with the rotation speed Ne of the engine 20. Accordingly, the failure detection device 70 can accurately reflect the failure of the MG 30 by reflecting the rotation speed Ne of the engine 20. [0042] The target power generation voltage when the MG30 generates power varies according to the electrical load of the supplementary machine 80. Therefore, the phase at which each phase of the inverter 50 is set to be turned on during power conversion also changes in accordance with the electrical load of the supplementary machine 80. Here, the memory section 71 of the fault detection device 70 of this embodiment associates and memorizes the phase controlled during the normal power conversion of the MG 30 with the electrical load of the supplementary machine 80. According to this, the fault detection device 70 can reflect the electrical load of the supplementary machine 80 and correctly determine the fault of the MG 30. [0043] The first embodiment can be modified as follows. [0044] In a modified example of the first embodiment, when the speed of change in the amount of deviation between the phase controlled at the time of power conversion and the phase at the normal time of MG30 is greater than the failure determination threshold (when the speed of change is not normal, the In the case where the speed is high), the failure determination unit 72 may determine that the MG30 is malfunctioning. [0045] FIG. 6 is a flowchart showing a processing procedure of failure detection in a modification of the first embodiment. The failure determination unit 72 calculates the change speed of the deviation amount calculated by the same method as the processing of step S21 in FIG. 4 (step S31). The rate of change of the deviation amount can be calculated, for example, by subtracting the deviation amount calculated previously from the deviation amount calculated this time. Next, the failure determination unit 72 determines whether the rate of change of the deviation amount calculated in the process of step S31 is greater than the failure determination threshold value (step S32). The threshold value of failure judgment related to the change speed of the deviation amount (equivalent to the specified change speed) is set to the specified change speed that would not occur during normal MG30. When the failure determination unit 72 determines that the change speed of the deviation amount is greater than the failure determination threshold (step S32: YES), the process of step S33 is performed. On the other hand, the failure determination unit 72 determines that the speed of change in the amount of deviation is below the failure determination threshold (step S32: NO) and executes the processing of step S34. The processing in steps S33 and S34 is the same as the processing in steps S23 and S24 in FIG. 4, respectively. [0046] FIG. 7 is a timing chart showing an example of failure detection in a modification of the first embodiment. The operation up to time t1 is the same as that shown in FIG. 5. At time t3 before time t2, it is assumed that the rate of change of the deviation amount becomes greater than the failure determination threshold. Based on this, it was determined that MG30 was abnormal. The failure determination flag is set to on. According to the above configuration, in this modification, when the amount of deviation between the phase controlled at the time of power conversion and the phase at the normal time of the MG30 increases rapidly, the failure of the MG30 can be detected early. [0047] <Second Embodiment> Hereinafter, the second embodiment will be described focusing on the differences from the first embodiment. The same components as those in the first embodiment are assigned the same reference numerals as those in the first embodiment, and descriptions thereof are omitted. [0048] FIG. 8 shows a schematic block diagram of a system 110 according to this embodiment. [0049] The MG130 includes a first group of windings 31A, 32A, and 33A and a second group of windings 31B, 32B, and 33B. The windings of windings 31A, 32A, 33A (three-phase windings of the first group) are more than the windings of windings 31B, 32B, 33B (three-phase windings of the second group). The MG 130 can switch the group of three-phase windings (windings of each phase corresponding to U-phase, V-phase, and W) connected to the inverter 50 to the first group and the second group. Specifically, the MG 130 includes switching units 37, 38, and 39. The switching section 37 switches between the winding 31A and the winding 31B. The switching unit 38 switches between the winding 32A and the winding 32B. The switching unit 39 switches between the winding 33A and the winding 33B. The operations of the switching sections 37, 38, and 39 are controlled by a winding switching control section (hereinafter referred to as a “switching control section”) 65. [0050] The switching control unit 65 is similar to the control amount calculation unit 60 and the failure detection device 70, and is configured of, for example, an MGECU, an engine ECU, a hybrid ECU, and the like. MGECU controls MG130. The engine ECU controls the engine 20. Hybrid ECU is a higher-level ECU that controls MGECU and engine ECU. When the rotation speed Ne of the engine 20 is slower than a predetermined rotation speed, the switching control unit 65 operates the switching units 37, 38, and 39 to switch the three-phase windings connected to the inverter 50 to the windings 31A, 32A, and 33A. Specifically, when the rotation speed Ne of the engine 20 is slower than the predetermined rotation speed, the switching sections 37, 38, and 39 are switched from windings 31B, 32B, and 33B (second group) to windings 31A, 32A, and 33A (second team 1). When the rotation speed Ne of the engine 20 is faster than a predetermined rotation speed, the switching control unit 65 operates the switching units 37, 38, and 39 to switch the three-phase windings connected to the inverter 50 to the windings 31B, 32B, and 33B. Specifically, when the rotation speed Ne of the engine 20 is faster than a predetermined rotation speed, the switching sections 37, 38, and 39 are switched from windings 31A, 32A, and 33A (the first group) to windings 31B, 32B, and 33B (the first group), respectively. 2 teams). [0051] The memory section 71 performs voltage phases (normally controlled voltage phase control amounts) of the three-phase windings in accordance with the operating state of the engine 20 during power conversion of the MG130 through the inverter 50 during normal conversion. memory. Specifically, as shown in the example of FIG. 10, the memory section 71 is the electrical load in the state of the windings 31A, 32A, and 33A (three-phase windings in the first group) connected to the inverter 50 in the normal state of the MG130. The relationship between the size and the rotation speed Ne of the engine 20 and the voltage phase control amount of the inverter 50 are used as mapping data and memorized. As shown in the example of FIG. 11, the memory section 71 stores the magnitudes of the electrical loads in the state of the windings 31B, 32B, and 33B (second-phase three-phase windings) connected to the inverter MG130 in the normal state 50. The relationship between the speed of the rotation speed Ne of the engine 20 and the voltage phase control amount of the inverter 50 is used as mapping data and memorized. The memorized data is a value measured in the same manner as in the first embodiment when the MG130 is normal, for example, by performing a predetermined experiment. The mapping data associates the value of the electrical load with the value of the rotation speed Ne of the engine 20 and the value of the voltage phase control amount of the inverter 50 in association with each other. That is, the information indicating the operating state of the engine includes the electrical load of the supplementary machine 80 and the rotation speed Ne of the engine 20. [0052] In this embodiment, the failure determination unit 72 determines the voltage phase control amount at the normal time that is referred to when the failure detection processing illustrated in FIGS. 4 and 6 is executed as follows. The failure determination section 72 corresponds to a group of three-phase windings connected to the inverter 50, and determines reference data from among the data of the voltage phase control amount at the normal time stored in the storage section 71. FIG. 9 is a flowchart for determining a processing sequence of reference data in a normal state. This series of processing is repeatedly executed by the failure determination unit 72 at a predetermined cycle. [0053] The failure determination unit 72 of this embodiment determines whether or not the group of three-phase windings connected to the inverter 50 is before switching (step S41). Specifically, the failure determination unit 72 determines whether the group of three-phase windings is switched from the windings 31A, 32A, and 33A (the first group) to the windings 31B, 32B, and 33B (the second group) through the switching control unit 65. When the failure determination unit 72 determines that the group of three-phase windings is before switching (step S41: YES), the reference data of the group of three-phase windings is determined as the voltage phase control amount at the time of normal before switching (step S42). That is, if the determination of step S41 is affirmative, the failure determination unit 72 will memorize the state of the windings 31A, 32A, and 33A (the three-phase windings of the first group) connected to the inverter 50 when the MG130 is normal. The data (refer to FIG. 10) of the relationship between the magnitude of the electrical load in the engine, the speed Ne of the engine 20 and the voltage phase control amount of the inverter 50 (see FIG. 10) is determined as the reference data. After that, the failure determination unit 72 once ends (ends) this series of processing. [0054] On the other hand, in the determination processing of step S41, if the failure determination unit 72 determines that the group of three-phase windings is not before switching (step S41: No), the reference data of the group of three-phase windings is determined as The voltage phase control amount in the normal state after switching (step S43). That is, when the determination in step S41 is negative, the failure determination unit 72 will memorize the state of the windings 31B, 32B, and 33B (second-phase three-phase windings) connected to the inverter 50 when the MG130 is normal. The data (see FIG. 11) of the relationship between the magnitude of the electrical load and the rotation speed Ne of the engine 20 and the voltage phase control amount of the inverter 50 are determined as reference data. After that, the failure determination unit 72 once ends (ends) this series of processing. [0055] According to this embodiment, the MG130 includes a first group of windings 31A, 32A, and 33A and a second group of windings 31B, 32B, and 33B. The MG130 can switch the group of the three-phase windings connected to the inverter 50 through the switching sections 37, 38, and 39. The memory section 71 of the fault detection device 70 memorizes the phases that are controlled by the inverter 20 according to the operating state of the engine 20 when the inverter 50 performs power conversion according to each group of the three-phase windings when the MG 130 is normal. The fault determination section 72 of the fault detection device 70 corresponds to the group of three-phase windings connected to the inverter 50, and determines the fault detection processing time from the data of the voltage phase control amount at the normal time stored in the memory section 71. Reference data used. The failure determination unit 72 determines the failure of the MG130 based on the amount of deviation between the phase at the time of power conversion controlled by the control amount calculation unit 60 and the phase at the time of normal power conversion memorized by the storage unit 71 of the MG130. According to this, the failure detection device 70 can detect the failure of each of the three-phase windings included in the MG 130 early and correctly. [0056] In addition, the first and second embodiments can be implemented as modified as follows. [0057] In the modified examples of the first and second embodiments, the rotation speed Ne of the engine 20 may be calculated based on the detection value of the crank angle sensor that detects the crank angle of the engine 20. In addition, as information showing the operating state of the engine 20, instead of the rotation speed Ne of the engine 20, a value obtained by calculating the rotation speed Ne or a rotation speed of a cam shaft (not shown) provided in the engine 20 may be used instead. . [0058] In a modification of the first embodiment, the failure determination unit 72 adds the counter from the point when the determination in step S22 in FIG. 4 or step S32 in FIG. 6 is affirmative. The failure determination unit 72 determines that the MG 30 is abnormal under the condition that the counter value is greater than a predetermined counter value. That is, the failure determination unit 72 may determine that the MG 30 is abnormal based on the condition that the determination in step S22 in FIG. 4 or step S32 in FIG. 6 is positive within a predetermined time. In the second embodiment, the data of the voltage phase control amount at the normal time referred to when the fault detection processing illustrated in FIGS. 4 and 6 is executed is switched according to the group of the three-phase windings connected to the inverter 50. Here, in the modification of the second embodiment, the failure determination unit 72 may set a counter for each group of the three-phase windings. According to this configuration, even when the set of the three-phase windings connected to the inverter 50 is switched during the counting of the counter, the counter value can be held in the counter before the switching. The failure determination unit 72 may detect a disconnection or the like of each of the three-phase windings based on the counter value of the counter of each of the three-phase windings. [0059] In the first and second embodiments, an example of detecting a failure of the MG30 or MG130 when the MG30 or MG130 is performing power generation will be described. On the other hand, in this modification, if the power supplied by the DC power source 40 is used to boost the driving force of the engine 20 by MG30 or MG130, the failure of MG30 or MG130 may be detected. That is, when the MG30 or MG130 is driven (powered), the failure of the MG30 or MG130 may be detected. In this case, instead of the lead / lag phase control shown in FIG. 2, the control amount calculation unit 60 executes lead / lag phase control of the voltage phase control amount based on the target drive torque instead. Specifically, when the MG30 is driven, the control amount calculation unit 60 repeatedly sets each phase of the inverter 50 according to the rotation angle (electrical angle) of the rotor to be turned on during 180 ° and turned off during 180 °. Off. This type of control is called a rectangular wave voltage control. In addition, instead of the rectangular wave voltage control, the control amount calculation unit 60 may use a sine wave drive control, an overmodulation drive control, or a conduction period that is repeatedly turned on and off between 180 ° of the rotation angle (electrical angle) of the rotor. (on-period) 120 degree energization control of 120 °. When the target driving torque is larger than the current MG30 driving torque, the control amount calculation unit 60 sets the voltage phase control amount to a leading phase. When the target drive torque is smaller than the current MG30 drive torque, the control amount calculation unit 60 sets the voltage phase control amount to a lag phase. In this modification, the relationship obtained by replacing the power supply voltage with the electrical load of FIG. 3 and replacing the advanced phase amount with a lag phase amount is measured in advance, and the measurement results are memorized. The control amount calculation unit 60 may perform the failure detection processing of at least one of FIG. 4 and FIG. 6 using the measurement result. [0060] The torque T of the motor can be calculated from the calculation formula of T = p ・ Φ ・ iq. p is the number of magnetic pole pairs, Φ is the induced voltage constant, and iq is the q-axis current. p and Φ are fixed values. Therefore, the torque T can be simply calculated using iq. iq can be obtained by referring to mapping data set in advance based on a voltage phase control amount, a power supply voltage, and a motor rotation speed. [0061] The lead / lag phase control of the voltage phase control amount in this modification will be specifically described using the flowchart of FIG. 12. The control amount calculation unit 60 of this modification sets an initial value for the voltage phase control amount (step S51). The initial value is an amount of voltage phase control (normal value at idle) of the engine 20 at idle when the MG30 or MG130 is normal. [0062] Next, the control amount calculation unit 60 determines whether the target torque is greater than the current torque (step S52). When the control amount calculation unit 60 determines that the target torque is greater than the current torque (step S52: YES), it calculates the advanced phase addition amount (step S53). The advanced phase addition amount is an amount that advances the phase of the applied voltages Vu, Vv, and Vw to the phase of the signal of the magnetic pole position sensor. In this modification, the relationship between the difference ΔT (ΔT = target torque-current torque) between the target torque and the current torque and the leading phase addition amount is set in advance in a table. That is, in this embodiment, the mapping data in which the correspondence relationship between the difference ΔT and the advanced phase addition amount is set is stored in advance in a memory device provided in the control amount calculation unit 60. Therefore, the control amount calculation unit 60 refers to the table and calculates the advanced phase addition amount based on the difference ΔT. The table may be set in accordance with the rotation speed Ne of the engine 20. [0063] Next, the control amount calculation unit 60 adds the leading phase addition amount to the voltage phase control amount set in the process of step S51, and calculates the voltage phase control amount (step S54). The control amount calculation unit 60 once ends (ends) this series of processing. [0064] On the other hand, when the control amount calculation unit 60 determines that the target torque is lower than the current torque (step S52: No), it calculates the lag phase addition amount (step S55). The lag phase addition amount is an amount that lags the phases of the applied voltages Vu, Vv, and Vw to the phases of the magnetic pole position sensor signals. In this modification, the relationship between the difference ΔT between the target torque and the current torque and the lag phase addition amount is stored in advance in a table. The control amount calculation unit 60 refers to this table and calculates the lag phase addition amount based on the difference ΔT. The table may be set in accordance with the rotation speed Ne of the engine 20. [0065] Next, the control amount calculation unit 60 calculates the voltage phase control amount by subtracting the lag phase addition amount from the voltage phase control amount set in the process of step S51 (step S56). The control amount calculation unit 60 once ends (ends) this series of processing. [0066] As described above, in this modification, a case where the MG30 or MG130 performs driving (power operation) is assumed. In this case, the power supply voltage is low, and the faster the rotation speed Ne of the engine 20 is, the more the voltage phase control amount of the inverter 50 is advanced. [0067] As in the case where the MG30 or MG130 performs power generation, in this modification, the fault determination unit 72 of the fault detection device 70 detects a fault of the MG30 or MG130 according to the processing sequence illustrated in the flowchart of FIG. [0068] For example, suppose that the U-phase winding 31 of MG30 is disconnected. As a result, the current torque becomes smaller than the target torque, and the lead phase addition amount increases. Here, the leading phase addition amount is added to the initial value of the voltage phase control amount, and the voltage phase control amount increases. As a result, the amount of deviation between the actual voltage phase control amount and the normal voltage phase control amount appears to increase. After that, the deviation between the actual voltage phase control amount and the normal voltage phase control amount becomes larger than the failure determination threshold. Based on this, it was determined that MG30 was abnormal. The fault determination flag is set to a high level (1). [0069] When a three-phase rotating electric machine detects a failure of the three-phase rotating electric machine while generating power, an MG or an alternator may be used as the three-phase rotating electric machine. In addition, when a failure of the three-phase rotary electric machine is detected when the three-phase rotary electric machine is driven (powered), the three-phase rotary electric machine may be an MG or a motor. [0070] Above, the embodiments of the technology of the present disclosure have been described, but the technology of the present disclosure is not limited to the above embodiments. The technology of the present disclosure is applicable to various embodiments without departing from the gist of the present disclosure. [0071] For example, as another embodiment [1], when the amount of deviation between the current voltage phase control amount and the normal voltage phase control amount is larger than the failure determination threshold (predetermined amount), the failure determination section 72 Make a temporary judgment on the fault judgment of MG30 and keep it for a while. Next, when the change rate of the deviation between the phase controlled at the time of power conversion and the phase when the MG30 is normal becomes greater than the failure determination threshold (predetermined speed), the failure determination unit 72 may determine that the MG30 is a true failure. . [0072] The memory section 71 stores the voltage phase controlled by the inverter 50 according to the operating state of the engine 20 during normal power conversion of the MG 30 and the speed of change of the voltage phase. [0073] In another embodiment [1], the above-mentioned fault determination threshold is determined according to the voltage phase and the change rate of the voltage phase stored in the memory section 71. The above determination is performed in accordance with the processing sequence of the flowcharts illustrated in FIGS. 4 and 6. [0074] Also, as another embodiment [2], the failure determination unit 72 may reverse the execution order of the temporary determination and the true determination of the other embodiment [1]. That is, when the variation rate of the deviation amount is larger than the failure determination threshold, the failure determination section 72 sets the failure determination of the MG30 as a temporary determination and reserves it for a time. When the amount of deviation between the current voltage phase control amount and the normal voltage phase control amount is greater than the failure determination threshold, the failure determination section 72 may determine that the failure of the MG30 is a true failure. [0075] In another embodiment [2], when the variation speed of the deviation amount becomes large and is momentarily larger than the failure determination threshold, the failure determination unit 72 does not immediately determine that MG30 is abnormal. When the amount of deviation between the current voltage phase control amount and the normal voltage phase control amount becomes larger than the failure determination threshold, the failure determination section 72 determines that the failure of the MG30 is a true failure. Therefore, in the other embodiment [2], it is possible to perform more accurate fault determination. [0076] According to this, in the other embodiment [2], it is possible to suppress the transmission of unintentional abnormalities to passengers, and it is possible to correctly detect the failure of the rotating electrical machine.
[0077][0077]
10、110‧‧‧系統10, 110‧‧‧ system
20‧‧‧引擎20‧‧‧ Engine
30、130‧‧‧MG30, 130‧‧‧MG
40‧‧‧直流電源40‧‧‧DC Power
50‧‧‧逆變器50‧‧‧ Inverter
60‧‧‧電壓相位控制量運算部(相位控制部)60‧‧‧Voltage phase control amount calculation section (phase control section)
70‧‧‧故障檢測裝置70‧‧‧Fault detection device
71‧‧‧記憶部71‧‧‧Memory Department
72‧‧‧故障判定部72‧‧‧Fault determination department
[0011] [圖1]表示第1實施形態之系統之概略的方塊圖。 [圖2]超前/滯後相位控制之處理順序的流程圖。 [圖3]表示正常時之引擎旋轉速度與電氣負載與電壓相位控制量之關係的映射數據(map data)。 [圖4]表示第1實施形態之故障檢測之處理順序的流程圖。 [圖5]表示故障檢測之一例的時序圖。 [圖6]表示故障檢測之變形例之處理順序的流程圖。 [圖7]表示故障檢測之其他例的時序圖。 [圖8]表示第2實施形態之系統之概略的方塊圖。 [圖9]表示正常時之參照數據決定之處理順序的流程圖。 [圖10]表示第1組之三相繞組連接時正常時之引擎旋轉速度與電氣負載與電壓相位控制量之關係的映射。 [圖11]表示第2組之三相繞組連接時正常時之引擎旋轉速度與電氣負載與電壓相位控制量之關係的映射。 [圖12]超前/滯後相位控制之變形例之處理順序的流程圖。[0011] [FIG. 1] A block diagram schematically showing a system of the first embodiment.图 [Figure 2] Flow chart of processing sequence of lead / lag phase control. [Fig. 3] Map data showing the relationship between the engine rotation speed and the electrical load and the voltage phase control amount in the normal state. [Fig. 4] A flowchart showing a processing procedure of failure detection in the first embodiment.图 [Fig. 5] A timing chart showing an example of fault detection. [Fig. 6] A flowchart showing a processing procedure of a modified example of failure detection. [Fig. 7] A timing chart showing another example of failure detection. [Fig. 8] A schematic block diagram showing a system of the second embodiment.图 [Fig. 9] A flowchart showing a processing procedure of reference data determination in a normal state.图 [Fig. 10] A map showing the relationship between the engine rotation speed, the electrical load, and the voltage phase control amount when the three-phase windings in the first group are connected normally.图 [Fig. 11] shows the mapping of the relationship between the engine rotation speed and the electrical load and the voltage phase control amount when the three-phase windings in the second group are connected normally. [Fig. 12] A flowchart of a processing sequence of a modification of the lead / lag phase control.
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