Mitsubishi Heavy Industries Limited

Mitsubishi Heavy Industries Engine & Turbocharger, Ltd.

Mitsubishi Hitachi Power Systems, Ltd.

Mitsubishi Power, Ltd.

Daigo Watanabe

Motoki Ebisu

Keigo Sakamoto

Takumi Tokiyoshi

Takashi Arai

Takao Yokoyama

Isao Tomita

Eigo Katou

Shingo Shudo

Hiroshi Suzuki

Masahiro Yamada

Hideki Yamaguchi

Toyotaka Yoshida

Yosuke Dammoto

Yasuaki Jinnai

Takeshi Matsuo

Taiji Torigoe

Ryoji Okabe

Takashi Yoshimoto

Toru Kikuchi

Hirotaka Higashimori

Masayuki Shimizu

Katsuyuki Osako

Makoto Ozaki

Yuta Furukawa

Yuya Konno

Kazuhisa Tsutsumi

Uwe Stein

Masahiro Kashiwagi

Yuta Ishii

Nariaki Seike

Masaaki Fujita

Michio Kyoya

Youji Akiyama

Yuichi Kanemaki

Shigeyoshi Sakuma

Satomi Nagae

Fumitoshi Sakata

Hiroyuki Ohyama

Shintaro Matsumoto

Yasuharu Chuman

Shinji Kawabata

Wataru Murono

Takuya Fukahori

Ichiro Ohtsu

Chikako Kato

Yasutaka Urashita

Aki Inoue

Fergus Mcintyre

John Stevenson

A precombustion chamber gas engine includes a main-chamber forming portion forming a main combustion chamber, and a precombustion-chamber forming portion forming a precombustion chamber communicating with the main combustion chamber via a plurality of nozzle holes. The precombustion-chamber forming portion includes a cylindrical portion extending along an extension direction of a precombustion chamber central axis of the precombustion-chamber forming portion, and a tip portion closing a main-combustion-chamber-side end of the cylindrical portion and having the nozzle holes. The tip portion includes a thin region having a thickness T satisfying T&#x3c;L where L is a length of each nozzle hole.

Precombustion chamber gas engine

A turbine housing includes an outer housing portion which includes an inner wall internally forming a spiral space, a first heat shield core which separates the spiral space into a scroll flow passage where an exhaust gas flows and a heat shield space positioned on a side of the inner wall, the first heat shield core being disposed so as to face the inner wall in the spiral space, a variable nozzle unit for adjusting a flow of the exhaust gas from the scroll flow passage toward an impeller, the variable nozzle unit being disposed on a side opposite to the outer housing portion across the first heat shield core in an axial direction, and at least one annular seal portion disposed between the first heat shield core and the outer housing portion in the axial direction.

Turbine housing and turbocharger including the same

An impeller for a rotary machine includes a base material of the impeller made of Al or an Al alloy. A surface layer for the impeller is formed by an electroless plating layer with a Ni&#x2014;P based alloy and an under layer disposed between the base material and the surface layer, the under layer having a smaller Vickers hardness than the surface layer.

Impeller for rotary machine, compressor, supercharger, and method for producing impeller for rotary machine

A turbocharger includes a gripping unit gripping a turbine-housing side flange portion and a bearing-housing side flange portion to couple a turbine housing and a bearing housing. In a state where the turbine housing and the bearing housing are coupled by the gripping unit, an elastic force in a direction to separate the turbine-housing side flange portion and the bearing-housing side flange portion from each other is applied to each of the turbine housing and the bearing housing.

Turbocharger

A turbocharger includes: a turbine wheel; a turbine housing; a bearing housing; a shroud having a facing surface which faces a tip of a blade of the turbine wheel and being configured to surround the turbine wheel, the shroud comprising a separate member from the turbine housing and being disposed inside the turbine housing via a gap with respect to the turbine housing; a mount supported to at least one of the turbine housing or the bearing housing, at a position closer to the bearing housing than a scroll flow path in an axial direction of the turbine wheel; and at least one connection part connecting the mount and the shroud.

Bolt holesare formed in a joint partof a turbine housing, with flanged boltsscrewed in the bolt holes. A flange partof a bearing housingis sandwiched between bearing surfacesof the flanged boltsand an inner end faceof the joint part. A sealing ringis interposed in an annular space s. Before the flanged boltsare fastened, there is formed a height difference G equivalent to a compression allowance h for the sealing ring, between an outer end faceof the joint partand a bolt receiving surfaceof the flange part. The flanged boltsare screwed into the bolt holesuntil the bearing surfacesmake tight contact with the outer end faceso as to resiliently deform the sealing ring

Sealing structure for turbocharger housing

A compressor includes: an impeller including a hub and a plurality of blades disposed on an outer surface of the hub; and a housing which houses the impeller. The housing includes: a shroud section facing the outer surface of the hub to form a fluid flow path between the shroud section and the outer surface, and surrounding the impeller; and a casing section formed integrally with the shroud section and supporting the shroud section. The shroud section includes a first resin-based material having a static tensile strength of at least 65 MPa and no more than 200 MPa and a breaking strain of no more than 0.3 mm/mm at a temperature of 100&#xb0; C. The casing section includes a second resin-based material having a static tensile strength of at least 40 MPa and a breaking strain of at least 0.1 mm/mm at a temperature of 100&#xb0; C.

Compressor

Provided is a turbine housing that comprises: a scroll unit; a flat annular cover () that is disposed in a state where one end face abuts a flanged portion () of the scroll unit and that is welded to the flanged portion (); an annular seal portion () that extends from a basal end () welded to the inner circumferential side of the other end face of the annular cover () to the distal end () disposed further to the exterior than the basal end () in the radial direction and that comprises a member that can be elastically deformed; and a plurality of threaded bushings () that are each welded in a plurality of locations on the outer circumferential side of the other end face of the annular cover () and that have fastening holes () for fastening bolts () inserted along the direction of the axis of rotation. A sealing region that extends around the entire circumference of the axis of rotation is formed by elastically deforming the annular seal portion () by the distal end () being in contact with the outer circumferential face () of a bearing housing () by way of the bearing housing () being pressed toward the annular cover () via a seat face of a washer ().

Turbine housing

An object is to provide a sheet-metal turbine housing reinforced by a readily-manufacturable structure, the sheet-metal turbine housing also having a small thickness and improved containment performance. A sheet-metal turbine housing includes: a scroll part forming an exhaust gas channel of a scroll shape in a turbocharger for driving a turbine with exhaust gas of an engine, the scroll part comprising sheet metal; and at least one rib portion of a protrusion shape formed on an outer wall surface of the scroll part at a radially outer side of an inlet edge of a turbine blade along a circumferential direction of the scroll part, the at least one rib portion protruding either outward or inward, or both, and including a bend and bend-back structure formed on the sheet metal forming the scroll part.

Sheet-metal turbine housing

A method of extending a life expectancy of a high-temperature piping, includes removing a heat insulation material which covers the piping having a high creep rupture risk, and lowering an outer surface temperature of piping, wherein a width of an exposed portion obtained is twice or more a distance from a peeled-off end portion of the exposed portion to a portion where a compressive stress is asymptotical to 0 after a change in stress between a tensile stress and the compressive stress occurring in the piping due to the removal of the heat insulation material is made from the tensile stress to the compressive stress, and the distance is calculated based on the following formulae, &#x3b2;x=5, here, &#x3bd; is a Poisson's ratio, a is an average radius of the piping, and h is a plate thickness of the piping.

Method of extending life expectancy of high-temperature piping and life expectancy extension structure of high-temperature piping

In a scroll structure for a radial turbine configured such that a turbine rotoris rotationally driven by causing exhaust gas to flow from a spiral scroll portionformed in a turbine housingtoward a rotor bladeof the scroll portionin a radial direction, and act on the rotor blade, then flow out in an axial direction, a heat radiation space portion is formed in a shroud portionbetween the turbine housingand a turbine chamber provided with the rotor blade

Scroll portion structure for radial turbine or diagonal flow turbine

The turbine housingis formed by sheet metal scroll membersandbutted opposite each other and welded together. A center core partarranged in a central part of the scroll partis integrally formed in one piece from a steel pipe member such as to include a housing portionsurrounding a turbine wheel, a bearing receiving portionaxially supporting the turbine wheel, and a plurality of circumferentially spaced supportsbridging a gap between the housing portionand the bearing receiving portion

Sheet metal turbine housing

In the neighborhood area X of the tongue partforming the winding end part of the scroll part, the wall part membersare provided on both the sides of the welding part (the facing part) 'a' of the first scroll partand the second scroll part, wherein: the wall part membersencloses the welding part (the facing part) 'a' and forms the gas-tight space; and, the outer circumference wall which enclose the facing part and forms a gas-tight space configure a double-wall structure.

Turbine housing made of sheet metal

Growing community of inventors

Tokyo, Japan

Daigo Watanabe