US4464902A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Plural turbochargers having a common exhaust housing
Assignee: MAN AG
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Filing: 1982-03-02
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Granted: 1984-08-14
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Expires: 2002-03-02
Abstract
Abstract The twin exhaust-gas-powered turbines (9, 10) driving intake air compressors (1, 2) for an internal-combustion engine are connected together and mounted on central support brackets (47, 48) by a common turbine discharge housing (20) that deflects the discharge of each turbine separately towards an outlet funnel (24) with the help of a guiding structure that contains a median wall (33). Diffuser horns (31, 32) and hollow central plugs provide, in a short axial distance, for establishing a static pressure for causing the gas to flow with uniform pressure distribution out through the discharge funnel (24). The latter portion of the outflow path is enlarged by side pieces (26, 27) fitting over holes in the central piece (20) of the discharge casing through which the diffuser horns (31, 32) protrude with ample spacing from other components. The static pressure just mentioned creates a back pressure that improves the efficiency of the turbo-superchargers in their extraction of dynamic energy from the exhaust gas stream. The air compressors are provided with a "floating" suspension from brackets (49, 50) that is tolerant of thermal expansion.
Inventors
- 👤 Hans Mendle
- 👤 Rudolf Bandel
- 👤 Hanns-Gunther Bozung
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 17:07
CPC Classifications
F; F01; F01D; F01D25/00; F01D25/30; F02; F02C; F02C6/00; F02C6/04; F02C6/10; F02C6/12; F05; F05D; F05D2220/00; F05D2220/40; F05D2240/00; F05D2240/10; F05D2240/14
Claims Analysis
Total Claims: 14
Claim 1
Independent Claim
286 words
A twin turbo-supercharger unit forming a component of an internal-combustion engine having two supercharger units of substantially identical construction, each including a radial-flow compressor and a radial-flow turbine mounted coaxially and driven to provide opposite directions of flow by power provided from the exhaust gas output of said engine, into a common turbine discharge housing disposed between the two exhaust-driven turbo-superchargers and serving also for connecting the two superchargers together, said twin turbo-supercharger further having an improvement which comprises: supporting elements (47,48) rigidly fastening said turbine discharge housing to a mounting component body (46) provided laterally on said engine; support brackets (49,50) extending laterally from said engine for supporting said respective turbo-superchargers (1,2) of the twin unit at a distance from said engine in a floating manner from portions (51,52) of said engine providing mounting surfaces on a side of said engine; said turbine discharge housing (19) consisting of a plurality of parts, including a box-shaped housing mid-portion (20) having side apertures centered on the axis of the superchargers and a funnel-shaped discharge portion (24) and two housing side parts (26,27) fastened to said housing mid-portion (20) around the edges of the respective side apertures thereof and also fastened to the respective casings (13,14) of said turbines; a guiding structure within said turbine discharge housing (19) comprising guiding wall means (33,34,35,40,41,42,43) including a median wall (33) for separately leading the respective gas streams issuing from said radial turbines towards said median wall, and diffuser horns (31,32) at the respective outputs (29,30) of said radial turbines (9,10) which flare outward in the direction of flow for cooperating with said guiding structure to produce a static pressure for improving the recovery of exhaust gas energy by said turbo-superchargers.
Claim 2
Dependent Claim
286 words
A twin turbo-supercharger unit forming a component of an internal-combustion engine having two supercharger units of substantially identical construction, each including a radial-flow compressor and a radial-flow turbine mounted coaxially and driven to provide opposite directions of flow by power provided from the exhaust gas output of said engine, into a common turbine discharge housing disposed between the two exhaust-driven turbo-superchargers and serving also for connecting the two superchargers together, said twin turbo-supercharger further having an improvement which comprises: supporting elements (47,48) rigidly fastening said turbine discharge housing to a mounting component body (46) provided laterally on said engine; support brackets (49,50) extending laterally from said engine for supporting said respective turbo-superchargers (1,2) of the twin unit at a distance from said engine in a floating manner from portions (51,52) of said engine providing mounting surfaces on a side of said engine; said turbine discharge housing (19) consisting of a plurality of parts, including a box-shaped housing mid-portion (20) having side apertures centered on the axis of the superchargers and a funnel-shaped discharge portion (24) and two housing side parts (26,27) fastened to said housing mid-portion (20) around the edges of the respective side apertures thereof and also fastened to the respective casings (13,14) of said turbines; a guiding structure within said turbine discharge housing (19) comprising guiding wall means (33,34,35,40,41,42,43) including a median wall (33) for separately leading the respective gas streams issuing from said radial turbines towards said median wall, and diffuser horns (31,32) at the respective outputs (29,30) of said radial turbines (9,10) which flare outward in the direction of flow for cooperating with said guiding structure to produce a static pressure for improving the recovery of exhaust gas energy by said turbo-superchargers.
Claim 3
Dependent Claim
112 words
A twin turbo-supercharger unit as defined in claim 1, in which said guiding structure (28) includes a median wall (33) subdividing the interior of said housing mid portion (20) into two discharge spaces (38, 39) extending out to the neighborhood of said funnel-shaped discharge opening (24), and also a pair of funnel-shaped guide tubes (34, 35) on opposite sides of said median wall (33) having their widest diameter portions against said median wall and projecting so as to extend into the space enclosed by said diffuser horns (31, 32) with their ends having a diameter corresponding to the internal diameter of the respective outlets (29, 30) of said radial turbines (9, 10).
Claim 4
Dependent Claim
46 words
A twin turbo-supercharger unit as defined in claim 2, in which said median wall (33) has bent wall portions (42,43) so shaped that in both discharge flow spaces (38, 39) a flow cross section is provided that becomes larger in the vortex direction of the flow.
Claim 5
Dependent Claim
54 words
A twin turbo-supercharger unit as defined in claim 2, in which the profile of said diffuser horns (31, 32) and of said guide tubes (34, 35), in a plane passing through the turbo-supercharger axis, is hyperbolic and maintains approximately the same spacing of diffuser horn to guide tube in the region of their overlap.
Claim 6
Dependent Claim
75 words
A twin turbo-supercharger unit as defined in claim 2, in which each said diffuser horn (31, 32) has a fastening flange (36, 37) by which it is screwed onto a casing (13, 14) of the corresponding radial turbine (9, 10) and in which each said diffuser horn is of an axial length that is substantially equal to two thirds of the spacing between said casing (13, 14) of said turbine and said median wall (33).
Claim 7
Dependent Claim
26 words
A twin turbo-supercharger unit as defined in claim 2, in which said guiding structure (28) is integrally constituted in the form of a ferrous metal casting.
Claim 8
Dependent Claim
22 words
A twin turbo-supercharger unit as defined in claim 2, in which said guiding structure (28) is an assembly of parts welded together.
Claim 9
Dependent Claim
70 words
A twin turbo-supercharger as defined in claim 1, in which said housing side parts (26, 27) are constituted as pot-shaped pieces having their bottoms and side walls partly cut out so as to fit respective casing (13, 14) of said radial turbines (9, 10) to which they are connected and are also respectively equipped with peripheral fastening flanges (44, 45) for securing them by screws to said housing mid-portion (20).
Claim 10
Dependent Claim
30 words
A twin turbo-supercharger as defined in claim 8, in which said housing side parts (26, 27) are of sheet steel and are welded onto the respective turbine casings (13, 14).
Claim 11
Dependent Claim
21 words
A twin turbo-supercharger unit as defined in claim 8, in which said housing side parts (26, 27) are of identical shape.
Claim 12
Dependent Claim
37 words
A twin turbo-supercharger unit as defined in claim 1, in which said housing side parts (26, 27) are respectively made integral with a casing (13, 14) of the adjacent radial turbine (9, 10) in a common casting.
Claim 13
Dependent Claim
43 words
A twin turbo-supercharger unit as defined in claim 1, in which said common turbine discharge housing (19) is mounted at a predetermined spacing from said mounting component body (46) of said engine by means of interposed angle brackets (47, 48) reinforced by ribs.
Claim 14
Dependent Claim
58 words
A twin turbo-supercharger unit as defined in claim 1, in which said support brackets supports (49, 50) are attached to the transition and connection region of the spiral casing (7, 8) of the respective compressors and the bearing casings (15, 16) of the respective exhaust-powered turbo-superchargers (1, 2), whereby a mounting tolerant of heat expansion effects is provided.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-08-14 | 1988-02-13 | 1988-08-14 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-08-14 | 1992-02-13 | 1992-08-14 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-08-14 | 1996-02-13 | 1996-08-14 | $7700.00 | Window Closed / Lapsed |