-
公开(公告)号：WO2018208873A1
公开(公告)日：2018-11-15
申请号：PCT/US2018/031719
申请日：2018-05-09
Applicant: BORGWARNER INC.
Inventor： HARRIS, Thomas Craig , PRUITT, Daniel , LEDGER, David , EDMONDS, Paul
CPC classification number: F04D29/4206 , F02B33/40 , F02B37/16 , F02B39/02 , F02B39/10 , F02M35/10157 , F02M35/10262 , F04D25/04 , F04D27/0207 , F04D29/053 , F04D29/284 , F04D29/4213 , F04D29/662 , F04D29/667 , F05D2220/40 , F05D2260/96
Abstract: A turbocharger (20) includes ported shroud compressor housing (28) disposed about a compressor wheel (36), having an air inlet passage (33) extending axially along and circumferentially about a longitudinal axis (A), volute base portion (50) operably adjacent to compressor wheel (36), contour (52) that encircles and complementarily matches compressor wheel (36), inducer (54) including ring (60) and plurality of extending members (62), inlet section (56) extending from volute base portion (50), and recirculation cavity (70) formed in volute base portion (50) and inlet section (56) with a recirculation slot (80) and inlet re-entry slot (82) for reentry of airflow into inlet section (56). The ring (60) has an inner wall surface (66) defining a first section (84) extending axially along the longitudinal axis (A) and proximate to the compressor wheel (36), second section (86) extending from first section (84) radially away from longitudinal axis (A), and third section (88) extending from second section (86) along longitudinal axis (A) and distal to the compressor wheel (36). The inlet section (56) has a first diameter (D1) and third section (88) has a second diameter (D2) greater than first diameter (D1).
-
公开(公告)号：WO2018208874A1
公开(公告)日：2018-11-15
申请号：PCT/US2018/031721
申请日：2018-05-09
Applicant: BORGWARNER INC.
Inventor： HARRIS, Thomas Craig , PRUITT, Daniel , LEDGER, David , EDMONDS, Paul
Abstract: A turbocharger (20) includes ported shroud compressor housing (28) disposed about compressor wheel (36) having air inlet passage (33) extending axially along and circumferentially about a longitudinal axis (A), volute base portion (50) operably adjacent to compressor wheel (36), contour that encircles and complementarily matches compressor wheel (36), inducer (54) including ring (60) and plurality of extending members (62), inlet section (56) extending from volute base portion (50), and recirculation cavity (70) formed in volute base portion (50) and inlet section (56) with recirculation slot (80) and inlet re-entry slot (82) for reentry of airflow into inlet section (56). The ring (60) has inner wall surface (66) defining first section (84) extending axially along longitudinal axis (A) proximate to compressor wheel (36), second section (86) extending from first section (84) radially away from longitudinal axis (A), and third section (88) extending from second section (86) radially away from and along longitudinal axis (A) and distal to compressor wheel (36). The inlet section (56) has first diameter (Dl) and third section (88) has second diameter (D2) being either one of equal to or less than first diameter (Dl).
-
公开(公告)号：EP3406848A2
公开(公告)日：2018-11-28
申请号：EP18165874.1
申请日：2018-04-05
Applicant: Borgwarner Inc.
Inventor： EDMONDS, Paul , HARRIS, Thomas
CPC classification number: F04D29/662 , F01D5/027 , F01D5/043 , F04D25/04 , F04D29/266 , F04D29/284 , F05D2220/40
Abstract: A turbocharger (20) includes a turbine wheel portion (36) to receive exhaust gas from an internal combustion engine, a turbocharger shaft (40) coupled to and rotatable by the turbine wheel portion, the turbocharger shaft extending along a longitudinal axis, and a compressor wheel portion (38) coupled to and rotatable by the turbocharger shaft. The compressor wheel portion includes a symmetrical leading edge region (54) facing airflow and an imbalance correction region (56) disposed longitudinally inboard from the symmetrical leading edge region and extending radially inward to correct an imbalance of the turbocharger shaft and to reduce aero-acoustic noises.
-
公开(公告)号：EP3406848A3
公开(公告)日：2018-12-05
申请号：EP18165874.1
申请日：2018-04-05
Applicant: Borgwarner Inc.
Inventor： EDMONDS, Paul , HARRIS, Thomas
CPC classification number: F04D29/662 , F01D5/027 , F01D5/043 , F04D25/04 , F04D29/266 , F04D29/284 , F05D2220/40
Abstract: A turbocharger (20) includes a turbine wheel portion (36) to receive exhaust gas from an internal combustion engine, a turbocharger shaft (40) coupled to and rotatable by the turbine wheel portion, the turbocharger shaft extending along a longitudinal axis, and a compressor wheel portion (38) coupled to and rotatable by the turbocharger shaft. The compressor wheel portion includes a symmetrical leading edge region (54) facing airflow and an imbalance correction region (56) disposed longitudinally inboard from the symmetrical leading edge region and extending radially inward to correct an imbalance of the turbocharger shaft and to reduce aero-acoustic noises.
-
-
-
Search Results
4
records
(took 0.023 seconds)
