JPH05272492A - Motor integrated type pump - Google Patents

Motor integrated type pump

Info

Publication number
JPH05272492A
JPH05272492A JP6592292A JP6592292A JPH05272492A JP H05272492 A JPH05272492 A JP H05272492A JP 6592292 A JP6592292 A JP 6592292A JP 6592292 A JP6592292 A JP 6592292A JP H05272492 A JPH05272492 A JP H05272492A
Authority
JP
Japan
Prior art keywords
rotor
impeller
casing
stator
face
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.)
Pending
Application number
JP6592292A
Other languages
Japanese (ja)
Inventor
Masahiro Atsumi
正博 渥美
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.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries 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 Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP6592292A priority Critical patent/JPH05272492A/en
Priority to FR939300233A priority patent/FR2686657B1/en
Priority to US08/003,612 priority patent/US5407331A/en
Publication of JPH05272492A publication Critical patent/JPH05272492A/en
Pending legal-status Critical Current

Links

Abstract

PURPOSE:To dispense with shaft seal so as to dissolve friction loss and wear caused by sliding motion between a shaft and the seal and to prevent the leak of liquid by mounting the rotor of an induction motor to the outer periphery of a rotatably supported impeller, and disposing a stator inside a casing, face to face with the rotor. CONSTITUTION:In this pump, the rotor 1 of an induction motor is mounted to the outer periphery of an impeller 5, integrally with the impeller 5, and the impeller 5 integral with the rotor 1 is integrated into a casing 2, together with a bearing 6, a rotary shaft 3, and the like. Inside the casing, a stator 4 is fitted face to face with the rotor 1, and the inside where a fluid passes is completely separated from the outside by the casing 2. When magnetic force is generated by the stator 4, resiliency is generated to the rotor 1, against this magnetic force, so that the rotor 1 is rotated. At the same time, the impeller 5 is also rotated to perform pumping action. Accordingly, there is no need to pass the rotary shaft 3 through to the outside of the casing 2 to drive the impeller 5, so that shaft seal can be dispensed with.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】本発明は、ロケットにおける液体
燃料のブースターなどに適用される電動機一体型ポンプ
に関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a motor-integrated pump applied to a liquid fuel booster in a rocket.

【0002】[0002]

【従来の技術】図2は従来のポンプの説明図である。図
において、従来のポンプは電動モータ或いはタービン等
の動力源に回転軸03を直結されて駆動され作動する。
このポンプ内部から流体が外部或いは電動モータ内へ流
出しないように軸シールを必要とし、パッキン04が装
着されている。符号05は電動モータの回転子、06は
固定子(ステータ)、07はベアリング、08は軸シー
ルのパッキン押えである。
2. Description of the Related Art FIG. 2 is an explanatory view of a conventional pump. In the figure, a conventional pump operates by directly connecting a rotary shaft 03 to a power source such as an electric motor or a turbine.
A shaft seal is required to prevent fluid from flowing out of the pump to the outside or the electric motor, and packing 04 is attached. Reference numeral 05 is a rotor of an electric motor, 06 is a stator (stator), 07 is a bearing, and 08 is a packing holder for a shaft seal.

【0003】[0003]

【発明が解決しようとする課題】上記のように従来のポ
ンプは、ポンプ内部から流体が外部或いは電動モータ内
へ流出しないように軸シールを必要としており、回転軸
03とパッキン04との摺動による動力損失および磨耗
を生ずる。また、ポンプ内部からの流体の漏洩を軸シー
ルにより完全に防止するのは難しい。
As described above, the conventional pump needs a shaft seal so that the fluid does not flow out of the pump to the outside or the electric motor, and the sliding between the rotary shaft 03 and the packing 04. Causes power loss and wear. Further, it is difficult to completely prevent the fluid leakage from the inside of the pump by the shaft seal.

【0004】[0004]

【課題を解決するための手段】本発明に係る電動機一体
型ポンプは上記課題の解決を目的にしており、ケーシン
グ内に回転可能に軸支されたインペラの外周に装着され
た誘導電動機の回転子と、該回転子と対峙して上記ケー
シング内側に配設された上記誘導電動機の固定子とを備
えた構成を特徴とする。
SUMMARY OF THE INVENTION An electric motor-integrated pump according to the present invention is intended to solve the above problems, and is a rotor of an induction motor mounted on the outer periphery of an impeller rotatably supported in a casing. And a stator of the induction motor arranged inside the casing so as to face the rotor.

【0005】[0005]

【作用】即ち、本発明に係る電動機一体型ポンプにおい
ては、ケーシング内に回転可能に軸支されたインペラの
外周に誘導電動機の回転子が装着されるとともに回転子
と対峙してケーシング内側に誘導電動機の固定子が配設
されており、ケーシング内側の固定子によりケーシング
内の回転子が回転してインペラを直接駆動することによ
りポンプ作用を行う。従って、回転軸をケーシング外側
へ貫通させてインペラを駆動する必要がなく、軸シール
をなくすことができる。
That is, in the motor-integrated pump according to the present invention, the rotor of the induction motor is mounted on the outer periphery of the impeller rotatably supported in the casing, and the rotor is guided inside the casing so as to face the rotor. A stator of the electric motor is provided, and a rotor inside the casing rotates by a stator inside the casing to directly drive the impeller, thereby performing a pumping action. Therefore, it is not necessary to drive the impeller by penetrating the rotary shaft to the outside of the casing, and the shaft seal can be eliminated.

【0006】[0006]

【実施例】図1は本発明の一実施例に係る電動機一体型
ポンプの説明図である。図において、本実施例に係る電
動機一体型ポンプはロケットにおける液体燃料のブース
ターに使用されるもので、軸シールを必要としないよう
にするために図に示すように本ポンプのインペラ5外周
に誘導モータの回転子1がインペラ5と一体化して装着
され、ケーシング2内にベアリング6、回転軸3などと
ともにロータとしてこの回転子1と一体型のインペラ5
が組込まれている。また、ケーシング2内部にはこの回
転子1と対峙して回転子1を駆動する固定子(ステー
タ)4が取付けられ、この固定子4の電線7はケーシン
グ2を貫通して外部へ引き出されており、この貫通部を
シールすることにより流体の通る内部がケーシング2に
より外部と完全に隔てられている。なお、回転子1はイ
ンペラ5に代えて図示しないインデューサ外周に一体化
して装着されていてもよい。固定子4により磁力が発生
するとこの磁力に対して回転子1に反撥力を生じ、誘導
モータと同じ原理で回転子1が回転する。回転子1とと
もにインペラ5も回転し、ポンプ作用が行われる。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS FIG. 1 is an explanatory view of an electric motor integrated pump according to an embodiment of the present invention. In the figure, the electric motor integrated pump according to the present embodiment is used as a booster for liquid fuel in a rocket, and is guided to the outer periphery of the impeller 5 of the present pump as shown in the figure so as not to require a shaft seal. The rotor 1 of the motor is mounted integrally with the impeller 5, and the impeller 5 integrated with the rotor 1 as a rotor together with the bearing 6, the rotating shaft 3 and the like in the casing 2.
Is incorporated. Further, inside the casing 2, a stator (stator) 4 facing the rotor 1 and driving the rotor 1 is attached, and an electric wire 7 of the stator 4 penetrates the casing 2 and is drawn out to the outside. By sealing this penetrating portion, the inside through which the fluid flows is completely separated from the outside by the casing 2. The rotor 1 may be integrally mounted on the outer circumference of an inducer (not shown) instead of the impeller 5. When a magnetic force is generated by the stator 4, a repulsive force is generated in the rotor 1 against this magnetic force, and the rotor 1 rotates on the same principle as an induction motor. The impeller 5 also rotates together with the rotor 1 to perform pumping action.

【0007】このように、本電動機一体型ポンプはイン
ペラ5の外周に回転子1を取付けて一体化したことによ
りケーシング2内でインペラ5が直接回転子1により駆
動されて回転するようになっており、電動モータとポン
プとを一体化して軸シールを不要にするとともに回転軸
3が短くなることにより、回転軸3、ケーシング2、ベ
アリング6などに対する厳しい同心度、寸法公差が解消
され、また軸シール用の特殊な調整治具などを必要とし
ない。また、回転子4はケーシング2内部に回転子1と
隙間を小さくして対峙しており、従来の電動モータ同様
に高トルク、高出力型になっている。また、インペラ6
の外周に回転子1を直接取付けて一体化したことにより
従来のプンプにおける軸シール、軸シール押などが不要
となって摺動個所が全くないので、ヒドラジン類、水素
等の可燃性および危険性流体や、スペースステーション
等の真空中で使用される流体などの漏洩を皆無にするこ
とができる。また、特に極低温、可燃性流体等の場合に
軸シールに必要なパージが不要になる。また、インペラ
5と回転子1とを一体化することにより回転軸3を短く
することができ、偏心による振動を抑えることができ
る。また、真空中で使用する場合でも電動モータの冷却
が不要である。また、ポンプ重量の軽減、小型化が可能
で、従来の50〜70%程度の重量となる。また、機械
的損失を軽減することができ、また寿命を大きく延ばす
ことが可能である。また、液体水素、液体窒素など極低
温の液体に使用することにより超伝導コイルの冷却が可
能で、これにより伝導効率を大きく向上させることがで
きる。また、ケーシング2によりポンプ内外が流体的に
完全に分離されることにより可燃性の流体に対して漏洩
対策を行うことができる。また、流体の漏洩が絶対に許
されない真空空間用ポンプとして使用することができ
る。従って、本ポンプはロケットにおける液体燃料のブ
ースターに使用される外、液体水素、液体酸素、液体窒
素、液体ヘリウム等の極低温流体、非磁性流体、可燃性
流体などの輸送用としても使用することができる。
As described above, in the electric motor integrated pump, the rotor 1 is attached to the outer periphery of the impeller 5 so as to be integrated, so that the impeller 5 is directly driven by the rotor 1 in the casing 2 to rotate. Since the electric motor and the pump are integrated to eliminate the need for a shaft seal and the rotating shaft 3 is shortened, strict concentricity and dimensional tolerance with respect to the rotating shaft 3, the casing 2, the bearing 6, etc. are eliminated, and No special adjustment jig for sealing is required. Further, the rotor 4 faces the rotor 1 inside the casing 2 with a small gap, and is of high torque and high output type like the conventional electric motor. Also, impeller 6
Since the rotor 1 is directly attached and integrated on the outer circumference of the pump, there is no need for a shaft seal or a shaft seal push in the conventional pump, and there are no sliding points, so flammability and danger of hydrazines, hydrogen, etc. Leakage of fluid, fluid used in a vacuum such as a space station, etc. can be eliminated. In addition, the purge required for the shaft seal is not necessary especially in the case of extremely low temperature and flammable fluid. Further, by integrating the impeller 5 and the rotor 1, the rotating shaft 3 can be shortened and vibration due to eccentricity can be suppressed. Further, even when used in vacuum, cooling of the electric motor is unnecessary. In addition, the weight of the pump can be reduced and the size can be reduced, which is about 50 to 70% of the conventional weight. In addition, mechanical loss can be reduced, and life can be greatly extended. In addition, the superconducting coil can be cooled by using it for liquid cryogenic liquid such as liquid hydrogen and liquid nitrogen, which can greatly improve the conduction efficiency. Further, since the inside and outside of the pump are completely separated from each other by the casing 2, the combustible fluid can be prevented from leaking. Further, it can be used as a vacuum space pump in which fluid leakage is never allowed. Therefore, this pump should not only be used as a liquid fuel booster in rockets, but also for transporting cryogenic fluids such as liquid hydrogen, liquid oxygen, liquid nitrogen, and liquid helium, non-magnetic fluids, and flammable fluids. You can

【0008】[0008]

【発明の効果】本発明に係る電動機一体型ポンプは前記
のように構成されており、軸シールをなくすことができ
るので回転軸と軸シールとの摺動による動力損失および
磨耗を生ぜず、またポンプ内部からの流体の漏洩が完全
に防止される。
The electric motor-integrated pump according to the present invention is constructed as described above, and since the shaft seal can be eliminated, power loss and wear due to sliding between the rotary shaft and the shaft seal do not occur, and Fluid leakage from inside the pump is completely prevented.

【図面の簡単な説明】[Brief description of drawings]

【図1】図1は本発明の一実施例に係る電動機一体型ポ
ンプの断面図である。
FIG. 1 is a sectional view of an electric motor integrated pump according to an embodiment of the present invention.

【図2】図2は従来のポンプの断面図である。FIG. 2 is a cross-sectional view of a conventional pump.

【符号の説明】[Explanation of symbols]

1 回転子 2 ケーシング 3 回転軸 4 固定子 5 インペラ 6 ベアリング 7 電線 8 シール 1 rotor 2 casing 3 rotating shaft 4 stator 5 impeller 6 bearing 7 electric wire 8 seal

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 ケーシング内に回転可能に軸支されたイ
ンペラの外周に装着された誘導電動機の回転子と、該回
転子と対峙して上記ケーシング内側に配設された上記誘
導電動機の固定子とを備えたことを特徴とする電動機一
体型ポンプ。
1. A rotor of an induction motor mounted on an outer periphery of an impeller rotatably supported in a casing, and a stator of the induction motor arranged inside the casing so as to face the rotor. An electric motor integrated pump characterized by comprising:
JP6592292A 1992-01-14 1992-03-24 Motor integrated type pump Pending JPH05272492A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP6592292A JPH05272492A (en) 1992-03-24 1992-03-24 Motor integrated type pump
FR939300233A FR2686657B1 (en) 1992-01-14 1993-01-13 MOTORIZED PUMP, PARTICULARLY FOR FUEL.
US08/003,612 US5407331A (en) 1992-01-14 1993-01-13 Motor-driven pump

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6592292A JPH05272492A (en) 1992-03-24 1992-03-24 Motor integrated type pump

Publications (1)

Publication Number Publication Date
JPH05272492A true JPH05272492A (en) 1993-10-19

Family

ID=13300951

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6592292A Pending JPH05272492A (en) 1992-01-14 1992-03-24 Motor integrated type pump

Country Status (1)

Country Link
JP (1) JPH05272492A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008522582A (en) * 2004-12-03 2008-06-26 エマーソン エレクトリック カンパニー Cryogenic pump system, rotor, and method of pumping cryogenic fluid
KR102166165B1 (en) * 2019-09-19 2020-10-15 주식회사 비츠로넥스텍 Propellant supply equipment of liquid rocket engine driven by superconducting electric motor

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2008522582A (en) * 2004-12-03 2008-06-26 エマーソン エレクトリック カンパニー Cryogenic pump system, rotor, and method of pumping cryogenic fluid
JP4834675B2 (en) * 2004-12-03 2011-12-14 エマーソン エレクトリック カンパニー Rotor, electrical equipment including rotor, and cryogenic pump system
KR102166165B1 (en) * 2019-09-19 2020-10-15 주식회사 비츠로넥스텍 Propellant supply equipment of liquid rocket engine driven by superconducting electric motor

Similar Documents

Publication Publication Date Title
US5407331A (en) Motor-driven pump
US4644202A (en) Sealed and balanced motor and fluid pump system
US8297948B2 (en) Arrangement for delivering fluids
US4013384A (en) Magnetically driven centrifugal pump and means providing cooling fluid flow
JPH08326687A (en) Molecular vacuum pump with cooling gas mechanism and operating method thereof
EP3952074A1 (en) Canned motor and pump driven by same, and rocket engine system and liquid fuel rocket employing same
JP4059416B2 (en) Integrated motor pump
JP5631350B2 (en) Compressor
CN214998262U (en) High-temperature shielding molten salt pump supported by magnetic suspension bearing
JP3918432B2 (en) Two-stage centrifugal compressor driven directly by an electric motor
JPH06185483A (en) Dry mechanical booster pump
JP2544825B2 (en) Magnet pump
JPH05272492A (en) Motor integrated type pump
JPH05187380A (en) Pump integrated with electric motor
CN216343036U (en) Magnetic suspension hydrogen circulating pump
CN113556016B (en) Motor and centrifugal compressor integrated device
JPH0579491A (en) Motor-operated pump
JP3742777B2 (en) Magnetic levitation type magnet pump
JP2010019164A (en) Pump device
JP2009156242A (en) Flat micropump
JP3485351B2 (en) Axial fluid electric machine
JPH06165478A (en) Superconducting rotating machine
KR102634155B1 (en) Rotating device
JP3432716B2 (en) Pressure generator and motor
JPH1137079A (en) Axial flow pump

Legal Events

Date Code Title Description
A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20010911