JPH10274048A - Variable capacity turbocharger - Google Patents

Variable capacity turbocharger

Info

Publication number
JPH10274048A
JPH10274048A JP9077315A JP7731597A JPH10274048A JP H10274048 A JPH10274048 A JP H10274048A JP 9077315 A JP9077315 A JP 9077315A JP 7731597 A JP7731597 A JP 7731597A JP H10274048 A JPH10274048 A JP H10274048A
Authority
JP
Japan
Prior art keywords
turbine
engine
variable nozzle
movable
vane
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
JP9077315A
Other languages
Japanese (ja)
Inventor
Hiroshi Uchida
博 内田
Akinobu Bessho
昭信 別所
Akihide Okuyama
晃英 奥山
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.)
Toyota Motor Corp
Toyota Central R&D Labs Inc
Original Assignee
Toyota Motor Corp
Toyota Central R&D Labs Inc
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 Toyota Motor Corp, Toyota Central R&D Labs Inc filed Critical Toyota Motor Corp
Priority to JP9077315A priority Critical patent/JPH10274048A/en
Publication of JPH10274048A publication Critical patent/JPH10274048A/en
Pending legal-status Critical Current

Links

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Supercharger (AREA)
  • Control Of Turbines (AREA)

Abstract

(57)【要約】 【課題】 可変ノズルから噴出したエンジン排気がター
ビン翼車に入るまでの距離が長くなってその間の損失が
多くなることを防止する。 【解決手段】 エンジンの排気で回転されるタービンに
可変ノズルを設けた可変容量形ターボチャージャにおい
て、タービンは、タービン翼車2の外回りに、可変ノズ
ルを構成する複数枚の可動ベーン7を配置し、各可動ベ
ーン7をその下流端側に配置した軸8の回りに回転可能
に設けた。
(57) [Summary] [PROBLEMS] To prevent a long distance until engine exhaust blown from a variable nozzle enters a turbine wheel, thereby preventing loss during that time from increasing. SOLUTION: In a variable displacement turbocharger in which a variable nozzle is provided in a turbine rotated by exhaust of an engine, the turbine has a plurality of movable vanes 7 constituting a variable nozzle arranged around an outer periphery of a turbine impeller 2. Each movable vane 7 is rotatably provided around a shaft 8 disposed on the downstream end side.

Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【発明の属する技術分野】本発明は、エンジンの排気で
回転されるタービンに可変ノズルを設けた可変容量形タ
ーボチャージャに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a variable displacement turbocharger in which a variable nozzle is provided in a turbine rotated by the exhaust of an engine.

【0002】[0002]

【従来の技術】可変容量形ターボチャージャのタービン
は、ハウジング内にタービン翼車を回転可能に設け、図
6に示すように、タービン翼車12の外回りに可動ベー
ン17を等間隔位置に配置して回転可能に設け、隣接す
る可動ベーン17で可変ノズルを構成している。
2. Description of the Related Art A turbine of a variable displacement turbocharger has a turbine wheel rotatably provided in a housing, and movable vanes 17 are arranged at equal intervals around the turbine wheel 12 as shown in FIG. The movable vanes 17 adjacent to each other constitute a variable nozzle.

【0003】エンジンの排気流量に応じてタービンの可
変ノズルの開口面積を増減し、ターボチャージャの過給
効率を高め、エンジンの出力特性を向上させる。
[0003] The opening area of the variable nozzle of the turbine is increased or decreased in accordance with the exhaust flow rate of the engine, the supercharging efficiency of the turbocharger is increased, and the output characteristics of the engine are improved.

【0004】エンジンの排気流量が少ないときには、図
6に実線で示すように、各可動ベーン17をタービン翼
車12のほぼ周方向に配置し、各可動ベーン17の下流
端をそれぞれその可動ベーン17の下流側に隣接する可
動ベーン17の上流端に近接して、可変ノズルの開口を
狭め、エンジンの排気流量が少なくても、タービンの駆
動動力従って圧縮機の駆動動力を高める。
When the exhaust flow rate of the engine is small, the movable vanes 17 are arranged substantially in the circumferential direction of the turbine wheel 12 and the downstream ends of the movable vanes 17 are respectively connected to the movable vanes 17 as shown by solid lines in FIG. In the vicinity of the upstream end of the movable vane 17 adjacent to the downstream side, the opening of the variable nozzle is narrowed, and the driving power of the turbine and hence the driving power of the compressor are increased even if the exhaust flow rate of the engine is small.

【0005】エンジンの排気流量が多いときには、図6
に鎖線で示すように、各可動ベーン17をタービン翼車
12のほぼ径方向に配置し、各可動ベーン17の下流端
をそれぞれその可動ベーン17の下流側に隣接する可動
ベーン17から遠ざけて、可変ノズルの開口を広げ、エ
ンジンの排気流量が多くても、タービンの入口圧力従っ
てエンジンの排気圧力の上昇を抑える。
When the exhaust flow rate of the engine is large, FIG.
As shown by a chain line, each movable vane 17 is arranged substantially in the radial direction of the turbine wheel 12, and the downstream end of each movable vane 17 is moved away from the movable vane 17 adjacent to the downstream side of the movable vane 17, respectively. The opening of the variable nozzle is widened to suppress a rise in the turbine inlet pressure and hence the engine exhaust pressure even when the engine exhaust flow rate is large.

【0006】[0006]

【発明が解決しようとする課題】ところが、上記のよう
な可変容量形ターボチャージャのタービンにおいては、
図6に示すように、回転可能な可動ベーン17は、その
軸18を上流端と下流端の中間位置に配置しているの
で、可変ノズルの開口が狭くなったときに、可変ノズル
の開口がタービン翼車12の入口から上流側に遠ざか
り、可変ノズルから噴出したエンジン排気がタービン翼
車12に入るまでの距離が長くなって、その間の損失が
多くなる。従って、タービンの効率が低下して、ターボ
チャージャの過給効率が低下する。
However, in the variable displacement turbocharger turbine as described above,
As shown in FIG. 6, the rotatable movable vane 17 has its shaft 18 disposed at an intermediate position between the upstream end and the downstream end. Therefore, when the opening of the variable nozzle becomes narrow, the opening of the variable nozzle is The distance from the inlet of the turbine impeller 12 to the upstream side and the engine exhaust ejected from the variable nozzle to enter the turbine impeller 12 becomes longer, and the loss during that time increases. Therefore, the efficiency of the turbine is reduced, and the supercharging efficiency of the turbocharger is reduced.

【0007】また、可動ベーンは、エンジン排気の熱で
変形するハウジングの両側壁部の間に挟まれており、そ
の熱変形によって回転不能になるのを防止するため、ハ
ウジングの各側壁部との間に広い隙間を設けている。従
って、その広い隙間から漏れるエンジン排気の量が多
く、タービンの効率が低下して、ターボチャージャの過
給効率が低下する。
The movable vanes are sandwiched between both side walls of the housing which are deformed by the heat of the engine exhaust. There is a wide gap between them. Therefore, the amount of engine exhaust leaking from the wide gap is large, the efficiency of the turbine is reduced, and the supercharging efficiency of the turbocharger is reduced.

【0008】[0008]

【課題を解決するための手段】本発明は、エンジンの排
気で回転されるタービンに可変ノズルを設けた可変容量
形ターボチャージャにおいて、タービンは、タービン翼
車の外回りに、可変ノズルを構成する複数枚の可動ベー
ンを配置し、各可動ベーンをその下流端側に配置した軸
の回りに回転可能に設けた。
SUMMARY OF THE INVENTION The present invention relates to a variable displacement turbocharger in which a variable nozzle is provided in a turbine rotated by the exhaust of an engine. A plurality of movable vanes were arranged, and each movable vane was provided rotatably around an axis arranged at the downstream end thereof.

【0009】更に具体的には、タービンは、ハウジング
内に回転可能に設けたタービン翼車の外回りに、可変ノ
ズルを構成する固定ベーンと可動ベーンを交互に配置
し、各固定ベーンをハウジングの両側壁部の間に固定
し、各可動ベーンをハウジングの両側壁部の間に挟んで
その可動ベーンの下流端側に配置した軸の回りに回転可
能に設けた。
More specifically, in the turbine, fixed vanes and movable vanes constituting a variable nozzle are alternately arranged around a turbine wheel rotatably provided in a housing, and each fixed vane is placed on both sides of the housing. The movable vanes were fixed between the wall portions, and each movable vane was rotatably provided around an axis disposed on the downstream end side of the movable vane between both side wall portions of the housing.

【0010】[0010]

【発明の効果】本発明のタービンにおいては、可動ベー
ンは、その下流端側に配置した軸の回りに回転するの
で、可変ノズルの開口が狭くなっても、広くなっても、
可変ノズルの開口位置が大きく変動せず、可変ノズルか
ら噴出したエンジン排気がタービン翼車に入るまでの距
離が長くならず、その間の損失が多くならない。
In the turbine of the present invention, the movable vane rotates around an axis disposed on the downstream end side, so that the variable nozzle opening becomes narrower or wider.
The opening position of the variable nozzle does not fluctuate greatly, and the distance until the engine exhaust ejected from the variable nozzle enters the turbine wheel does not increase, and the loss during that time does not increase.

【0011】また、固定ベーンと可動ベーンを交互に配
置し、各固定ベーンをハウジングの両側壁部の間に固定
した場合は、可動ベーンを挟んたハウジングの両側壁部
の間の距離が固定ベーンで保持される。従って、ハウジ
ングの各側壁部と可動ベーンの間の隙間を狭くしても、
ハウジングの熱変形によって可動ベーンが回転不能にな
るのを防止することができる。ハウジングの各側壁部と
可動ベーンの間の隙間を狭くして、その隙間から漏れる
エンジン排気の量を減らすことができる。
When the fixed vanes and the movable vanes are alternately arranged and each fixed vane is fixed between both side walls of the housing, the distance between the both side walls of the housing sandwiching the movable vane is fixed vane. Is held. Therefore, even if the gap between each side wall of the housing and the movable vane is narrowed,
It is possible to prevent the movable vane from becoming unrotatable due to thermal deformation of the housing. The gap between each side wall of the housing and the movable vane can be narrowed to reduce the amount of engine exhaust leaking from the gap.

【0012】結局、本発明の可変容量形ターボチャージ
ャにおいては、タービンの効率が高く、過給効率が高
い。
After all, in the variable displacement turbocharger of the present invention, the efficiency of the turbine is high and the supercharging efficiency is high.

【0013】[0013]

【発明の実施の形態】可変容量形ターボチャージャは、
自動車用エンジンのシリンダに接続した吸気通路の途中
に圧縮機を介在し、シリンダに接続した排気通路の途中
にタービンを介在し、圧縮機とタービンを同軸に連結し
ている。
BEST MODE FOR CARRYING OUT THE INVENTION A variable displacement turbocharger
A compressor is interposed in an intake passage connected to a cylinder of an automobile engine, a turbine is interposed in an exhaust passage connected to the cylinder, and the compressor and the turbine are coaxially connected.

【0014】エンジンの排気通路を流れる排気でタービ
ンが回転されて圧縮機が回転され、エンジンの吸気通路
を流れる空気が圧縮機で圧縮され、高圧になった空気が
エンジンのシリンダに供給される。
The exhaust gas flowing through the exhaust passage of the engine rotates the turbine to rotate the compressor. The air flowing through the intake passage of the engine is compressed by the compressor, and the high-pressure air is supplied to the cylinder of the engine.

【0015】タービンは、図1に示すように、ハウジン
グ1の中央部にタービン翼車2を入れ、タービン翼車2
の軸3をハウジング1の後部に軸受し、ハウジング1の
外周部に渦巻室4を設け、渦巻室4の大径部に、図示し
ない排気入口管を接続し、ハウジング1の前部に排気出
口管5を設けている。
As shown in FIG. 1, a turbine wheel 2 is placed in the center of a housing 1 and the turbine wheel 2
Shaft 3 is mounted on the rear part of the housing 1, a spiral chamber 4 is provided on the outer peripheral part of the housing 1, and a large-diameter part of the spiral chamber 4 is connected to an exhaust inlet pipe (not shown). A tube 5 is provided.

【0016】タービン翼車2と渦巻室4の間には、図1
と図2に示すように、同数枚の固定ベーン6と可動ベー
ン7を、それぞれ、タービン翼車2の径方向と周方向の
中間方向に沿わせて等間隔位置に配列し、固定ベーン6
と可動ベーン7を交互に配置し、各固定ベーン6をハウ
ジング1の前後の側壁部の間に固定し、各可動ベーン7
をハウジング1の前後の側壁部の間に挟み、各可動ベー
ン7とハウジング1の各側壁部の間の隙間を狭く設定
し、各可動ベーン7の下流端側の側面に突出した軸8を
ハウジング1の前側壁部に貫通して、各可動ベーン7を
その下流端側に配置した軸8の回りに回転可能に設け、
各可動ベーン7の軸8をその下流側に隣接する固定ベー
ン6に近い位置に配置し、隣接する固定ベーン6と可動
ベーン7で可変ノズルを構成している。
[0016] Between the turbine wheel 2 and the swirl chamber 4, there is shown in FIG.
As shown in FIG. 2 and FIG. 2, the same number of fixed vanes 6 and movable vanes 7 are arranged at equal intervals along the intermediate direction between the radial direction and the circumferential direction of the turbine wheel 2, respectively.
And the movable vanes 7 are alternately arranged, and each fixed vane 6 is fixed between the front and rear side walls of the housing 1.
Between the movable vanes 7 and the side walls of the housing 1 is narrowed, and the shaft 8 protruding from the downstream end side surface of each movable vane 7 is set in the housing. 1, each movable vane 7 is provided rotatably around a shaft 8 disposed at the downstream end side thereof,
The shaft 8 of each movable vane 7 is arranged at a position close to the adjacent fixed vane 6 on the downstream side, and the adjacent fixed vane 6 and movable vane 7 constitute a variable nozzle.

【0017】可動ベーン7とハウジング1の各側壁部の
間の隙間を狭く設定しているが、ハウジング1の両側壁
部の間の距離が固定ベーン6で保持されているので、ハ
ウジング1が熱変形しても、可動ベーン7が回転不能に
なるのが防止される。
Although the gap between the movable vane 7 and each side wall of the housing 1 is set to be small, the distance between the both side walls of the housing 1 is held by the fixed vane 6, so that the housing 1 is heated. Even if deformed, the movable vane 7 is prevented from becoming unrotatable.

【0018】ハウジング1の外に突出した各可動ベーン
7の軸8の前端は、図1に示すように、全可動ベーン7
を連動して傾斜させる機構9に連結し、連動傾斜機構9
に、図示しない駆動装置を連結し、駆動装置をエンジン
の排気流量従ってエンジンの回転速度に応じて制御する
制御装置を設けている。
The front end of the shaft 8 of each movable vane 7 projecting out of the housing 1, as shown in FIG.
Is linked to a mechanism 9 for interlocking and tilting, and an interlocking tilting mechanism 9
And a control device for controlling the drive device in accordance with the exhaust flow rate of the engine and hence the rotational speed of the engine.

【0019】エンジンの排気流量が少ないときには、図
3に示すように、各可動ベーン7をタービン翼車2のほ
ぼ周方向に配置し、各可動ベーン7の上流端をそれぞれ
その可動ベーン7の上流側に隣接する固定ベーン6の下
流端に当てて、各可動ベーン7とその上流側に隣接する
固定ベーン6の間を閉鎖し、各可動ベーン7の下流端を
それぞれその可動ベーン7の下流側に隣接する固定ベー
ン6に近接して、可変ノズルの開口を狭め、エンジンの
排気流量が少なくても、タービンの駆動動力を高める。
When the exhaust flow rate of the engine is small, as shown in FIG. 3, each movable vane 7 is arranged substantially in the circumferential direction of the turbine wheel 2, and the upstream end of each movable vane 7 is located upstream of the movable vane 7 respectively. The movable vane 7 is closed to the downstream end of the movable vane 7 by contacting the downstream end of the fixed vane 6 adjacent to the movable vane 6 to close the gap between each movable vane 7 and the fixed vane 6 adjacent to the upstream thereof. The opening of the variable nozzle is narrowed in the vicinity of the fixed vane 6 adjacent to the nozzle, and the driving power of the turbine is increased even if the exhaust flow rate of the engine is small.

【0020】エンジンの排気流量が多いときには、図4
に示すように、各可動ベーン7をタービン翼車2のほぼ
径方向に配置し、各可動ベーン7をそれぞれその可動ベ
ーン7の下流側に隣接する固定ベーン6の上流端に当て
て、各可動ベーン7とその下流側に隣接する固定ベーン
6の間を閉鎖し、各可動ベーン7の上流端をそれぞれそ
の可動ベーン7の上流側に隣接する固定ベーン6から遠
ざけて、可変ノズルの開口を広げ、エンジンの排気流量
が多くても、タービンの入口圧力の上昇を抑える。
When the exhaust flow rate of the engine is large, FIG.
As shown in FIG. 5, each movable vane 7 is disposed substantially in the radial direction of the turbine wheel 2, and each movable vane 7 is brought into contact with the upstream end of the fixed vane 6 adjacent to the downstream side of the movable vane 7 so that each movable vane 7 is moved. The gap between the vane 7 and the fixed vane 6 adjacent to the downstream side thereof is closed, and the upstream end of each movable vane 7 is moved away from the fixed vane 6 adjacent to the upstream side of the movable vane 7 to widen the opening of the variable nozzle. Even when the exhaust flow rate of the engine is large, the rise in the turbine inlet pressure is suppressed.

【0021】図3と図4から明らかなように、可変ノズ
ルの開口が狭くなっても、広くなっても、可変ノズルの
開口位置が大きく変動せず、可変ノズルから噴出したエ
ンジン排気がタービン翼車2に入るまでの距離が長くな
らず、その間の損失が多くならない。
As is clear from FIG. 3 and FIG. 4, the opening position of the variable nozzle does not fluctuate greatly even if the opening of the variable nozzle becomes narrow or wide, and the engine exhaust blown from the variable nozzle is discharged from the turbine blade. The distance to the car 2 does not become long, and the loss during that time does not increase.

【0022】また、ハウジング1の各側壁部と可動ベー
ン7の間の隙間を狭く設定しているので、その隙間から
漏れるエンジン排気の量が少ない。
Further, since the gap between each side wall of the housing 1 and the movable vane 7 is set to be small, the amount of engine exhaust leaking from the gap is small.

【0023】その結果、タービンの効率が高い。図5に
示すように、本発明の可変容量形ターボチャージャにお
いては、図6に示した従来例に比較して、過給効率が高
い。特に、エンジンの排気流量が少ないときに、過給効
率が高い。
As a result, the efficiency of the turbine is high. As shown in FIG. 5, in the variable displacement turbocharger of the present invention, the supercharging efficiency is higher than in the conventional example shown in FIG. In particular, when the exhaust flow rate of the engine is small, the supercharging efficiency is high.

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

【図1】本発明の実施形態の可変容量形ターボチャージ
ャのタービンの縦断側面図。
FIG. 1 is a vertical sectional side view of a turbine of a variable displacement turbocharger according to an embodiment of the present invention.

【図2】同タービンの部分縦断正面図。FIG. 2 is a partial vertical sectional front view of the turbine.

【図3】同タービンの可変ノズルの開口が狭くなった状
態を示す部分縦断正面図。
FIG. 3 is a partial vertical sectional front view showing a state where an opening of a variable nozzle of the turbine is narrowed.

【図4】同タービンの可変ノズルの開口が広くなった状
態を示す部分縦断正面図。
FIG. 4 is a partial vertical sectional front view showing a state where an opening of a variable nozzle of the turbine is widened.

【図5】同可変容量形ターボチャージャの過給効率と排
気流量の関係を示す線図。
FIG. 5 is a diagram showing the relationship between the supercharging efficiency and the exhaust gas flow rate of the variable displacement turbocharger.

【図6】従来の可変容量形ターボチャージャのタービン
の部分縦断正面図。
FIG. 6 is a partial longitudinal front view of a turbine of a conventional variable displacement turbocharger.

【符号の説明】[Explanation of symbols]

1 ハウジング 2 タービン翼車 6 固定ベーン 7 可動ベーン 8 可動ベーンの軸 DESCRIPTION OF SYMBOLS 1 Housing 2 Turbine wheel 6 Fixed vane 7 Movable vane 8 Movable vane shaft

フロントページの続き (72)発明者 別所 昭信 愛知県愛知郡長久手町大字長湫字横道41番 地の1 株式会社豊田中央研究所内 (72)発明者 奥山 晃英 愛知県豊田市トヨタ町1番地 トヨタ自動 車株式会社内Continuing from the front page (72) Inventor Akinobu Bessho 41 No. 41, Yokomichi, Nagakute-cho, Aichi-gun, Aichi Prefecture Inside Toyota Central Research Laboratory Co., Ltd. Inside the corporation

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 エンジンの排気で回転されるタービンに
可変ノズルを設けた可変容量形ターボチャージャにおい
て、 タービンは、タービン翼車の外回りに、可変ノズルを構
成する複数枚の可動ベーンを配置し、各可動ベーンをそ
の下流端側に配置した軸の回りに回転可能に設けたこと
を特徴とする可変容量形ターボチャージャ。
1. A variable displacement turbocharger in which a variable nozzle is provided on a turbine rotated by exhaust gas of an engine, wherein the turbine has a plurality of movable vanes constituting a variable nozzle disposed around an outer periphery of a turbine wheel. A variable displacement turbocharger, wherein each movable vane is rotatably provided around an axis disposed at a downstream end thereof.
JP9077315A 1997-03-28 1997-03-28 Variable capacity turbocharger Pending JPH10274048A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP9077315A JPH10274048A (en) 1997-03-28 1997-03-28 Variable capacity turbocharger

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP9077315A JPH10274048A (en) 1997-03-28 1997-03-28 Variable capacity turbocharger

Publications (1)

Publication Number Publication Date
JPH10274048A true JPH10274048A (en) 1998-10-13

Family

ID=13630502

Family Applications (1)

Application Number Title Priority Date Filing Date
JP9077315A Pending JPH10274048A (en) 1997-03-28 1997-03-28 Variable capacity turbocharger

Country Status (1)

Country Link
JP (1) JPH10274048A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009074542A (en) * 2007-08-28 2009-04-09 Toyota Central R&D Labs Inc Variable capacity turbocharger
DE102009020592A1 (en) * 2009-05-09 2010-11-11 Bosch Mahle Turbo Systems Gmbh & Co. Kg Charging device i.e. exhaust gas turbocharger, for motor vehicle, has flow channel lying between rotatably supported guide vanes, where one guide vane is flow-permeable and forms another flow channel
CN102900479A (en) * 2012-10-30 2013-01-30 北京理工大学 Variable nozzle turbocharger regulating mechanism integrated on turbine shell
WO2013116136A1 (en) * 2012-02-02 2013-08-08 Borgwarner Inc. Mixed-flow turbocharger with variable turbine geometry
JP2014516133A (en) * 2011-06-01 2014-07-07 ターボメカ Variable pitch nozzles for radial turbines, especially auxiliary power source turbines
JP2015505004A (en) * 2012-01-18 2015-02-16 アイ・エイチ・アイ チャージング システムズ インターナショナル ゲーエムベーハー Exhaust gas turbocharger turbine guide mechanism and turbine
US20160040590A1 (en) * 2014-08-11 2016-02-11 Ford Global Technologies, Llc Supercharged internal combustion engine with mixed-flow turbine
CN108825362A (en) * 2018-08-21 2018-11-16 天津北方天力增压技术有限公司 A kind of monoblock type twayblade group variable-geometry section nozzles ring
CN109236460A (en) * 2017-07-10 2019-01-18 通用汽车环球科技运作有限责任公司 Variable geometry turbine shell inlet channel for exhaust-driven turbocharger

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2009074542A (en) * 2007-08-28 2009-04-09 Toyota Central R&D Labs Inc Variable capacity turbocharger
DE102009020592A1 (en) * 2009-05-09 2010-11-11 Bosch Mahle Turbo Systems Gmbh & Co. Kg Charging device i.e. exhaust gas turbocharger, for motor vehicle, has flow channel lying between rotatably supported guide vanes, where one guide vane is flow-permeable and forms another flow channel
JP2014516133A (en) * 2011-06-01 2014-07-07 ターボメカ Variable pitch nozzles for radial turbines, especially auxiliary power source turbines
JP2015505004A (en) * 2012-01-18 2015-02-16 アイ・エイチ・アイ チャージング システムズ インターナショナル ゲーエムベーハー Exhaust gas turbocharger turbine guide mechanism and turbine
WO2013116136A1 (en) * 2012-02-02 2013-08-08 Borgwarner Inc. Mixed-flow turbocharger with variable turbine geometry
CN104053882A (en) * 2012-02-02 2014-09-17 博格华纳公司 Mixed-flow turbocharger with variable turbine geometry
US10408228B2 (en) 2012-02-02 2019-09-10 Borgwarner Inc. Mixed-flow turbocharger with variable turbine geometry
CN102900479A (en) * 2012-10-30 2013-01-30 北京理工大学 Variable nozzle turbocharger regulating mechanism integrated on turbine shell
US20160040590A1 (en) * 2014-08-11 2016-02-11 Ford Global Technologies, Llc Supercharged internal combustion engine with mixed-flow turbine
US10260406B2 (en) * 2014-08-11 2019-04-16 Ford Global Technologies, Llc Supercharged internal combustion engine with mixed-flow turbine
CN109236460A (en) * 2017-07-10 2019-01-18 通用汽车环球科技运作有限责任公司 Variable geometry turbine shell inlet channel for exhaust-driven turbocharger
CN108825362A (en) * 2018-08-21 2018-11-16 天津北方天力增压技术有限公司 A kind of monoblock type twayblade group variable-geometry section nozzles ring
CN108825362B (en) * 2018-08-21 2023-10-27 天津北方天力增压技术有限公司 Integral double-vane set nozzle ring with variable geometric section

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