Heat shield for an exhaust gas turbocharger and arrangement of a heat shield between two housing parts of an exhaust gas turbocharger
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F04D-029/58
F01D-025/14
F02C-006/12
F02C-007/24
F01D-025/16
F01D-025/24
F01D-025/28
출원번호
US-0175631
(2014-02-07)
등록번호
US-9683456
(2017-06-20)
우선권정보
DE-10 2011 114 060 (2011-09-22)
발명자
/ 주소
Burmester, Hermann
Delitz, Joachim
출원인 / 주소
IHI CHARGING SYSTEMS INTERNATIONAL GMBH
대리인 / 주소
Bach, Klaus J.
인용정보
피인용 횟수 :
1인용 특허 :
3
초록▼
In a heat shield for an exhaust gas turbocharger, by means of which at least a first area of the exhaust gas turbocharger is to be shielded against a second area in a heat insulating manner wherein the heat shield comprises at least one fastening structure by which the heat shield is attached to one
In a heat shield for an exhaust gas turbocharger, by means of which at least a first area of the exhaust gas turbocharger is to be shielded against a second area in a heat insulating manner wherein the heat shield comprises at least one fastening structure by which the heat shield is attached to one of the housing parts of the exhaust gas turbocharger, the fastening structure is in the form of locking elements for interlocking the heat shield with the respective housing part. The invention also resides in an arrangement of a heat shield between two housing parts of an exhaust gas turbocharger in such a way that it is firmly attached to one housing part without contacting the other housing part.
대표청구항▼
1. A heat shield for an exhaust gas turbocharger having a bearing housing part (12) attached to a turbine housing part (18) of an exhaust gas turbocharger (10), the heat shield (22) being arranged between the bearing housing part (12) and the turbine housing part (16) so as to limit heat transfer be
1. A heat shield for an exhaust gas turbocharger having a bearing housing part (12) attached to a turbine housing part (18) of an exhaust gas turbocharger (10), the heat shield (22) being arranged between the bearing housing part (12) and the turbine housing part (16) so as to limit heat transfer between the turbine housing part (18) and the bearing housing part (12) and comprising a base body (27) provided at its circumference with locking elements (24, 34, 45), for resiliently connecting the heat shield (22) to one of the housing parts (12, 18) of the exhaust gas turbocharger (10), the locking elements (24, 34, 45) interlocking the heat shield (22) with the housing part (12, 18) to which the heat shield is attached, the locking elements (24, 34, 45) comprising recesses, in which a corresponding wall portion of the housing part (12, 18) is accommodated for interlocking the heat shield (22) with the respective housing part (12, 18) at least one of the recesses and the locking elements (45) being in the form of an at least essentially spherically shaped segment. 2. The heat shield according to claim 1, wherein the locking elements (24, 34, 45) are integrally formed with the base body (27) of the heat shield (22). 3. The heat shield according to claim 1, wherein each locking element (24, 34, 45) comprises at least one protrusion (45) for be accommodation in a corresponding mounting feature (46) of the housing part (12, 18) to which the heat shield (22) is to be connected for interlocking the heat shield (22) with the respective housing part (12, 18). 4. An arrangement of a heat shield between a bearing housing part (12) and a turbine housing part (18) of an exhaust gas turbocharger for a combustion engine, wherein the heat shield (22) is mounted by fastening elements (24, 34, 45), to one of the housing parts (12, 18) so as to be arranged between the housing parts (12, 18) thereby limiting heat transfer between the turbine housing part (18) and the bearing housing part (12), the fastening elements (24, 34, 45) being in the form of resilient locking elements (24, 34, 45) which are provided at the circumference of the heat shield (22) and by which the heat shield (22) is elastically locked to one of the housing parts (12, 18) the heat shield being locked to the bearing housing part (12) without being in contact with the turbine housing part (12) and the bearing housing part (12) comprising an additional locking structure (24, 34, 45) in the form of a recess (30, 36, 46) in which the locking element (24, 34, 45) of the heat shield (22) is accommodated and securely locked in position.
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이 특허에 인용된 특허 (3)
Delitz, Joachim, Connection assembly for joining a turbine housing and a bearing housing and exhaust gas turbocharger.
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