US2014348643A1PendingUtilityA1
Semi-permeable media sealing an actuating shaft
Est. expirySep 27, 2031(~5.2 yrs left)· nominal 20-yr term from priority
Inventors:Timothy House
F04D 17/00F01N 3/021F02B 37/186F05D 2220/40Y02T10/12F02C 7/28
44
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Claims
Abstract
To impede soot leakage around a shaft which extends through a bore connecting volumes of differing pressures, e.g., a turbocharger turbine housing and the ambient air, a soot seal is provided to capture particulate matter while allowing the passage of gas.
Claims
exact text as granted — not AI-modifiedNow that the invention has been described, I claim:
1 . A turbocharger with a turbine housing, a device within the turbine housing actuated by an actuating mechanism located outside the turbine housing, a shaft which is rotatably mounted in a bore extending through the turbine housing or the bearing housing for transmitting an actuating movement from the actuating mechanism to the device, wherein a sealing material is provided to seal the bore, and wherein the sealing material is gas permeable and adapted to trap soot particles.
2 . The turbocharger as in claim 1 , wherein the sealing material is adapted to trap soot particles greater than 1.0 μm diameter
3 . The turbocharger as in claim 1 , wherein the sealing material is adapted to trap soot particles greater than 0.05 μm.
4 . The turbocharger as in claim 1 , wherein the sealing material is a porous material of which the primary component is selected from the group consisting of fiberglass, carbon, PTFE, bronze, stainless steel, nickel based alloys, titanium, copper, and aluminum.
5 . The turbocharger as in claim 1 , wherein the bore is widened along a segment in which the sealing material is accommodated.
6 . The turbocharger as in claim 1 , wherein the shaft is narrowed along a segment in which the sealing material is accommodated.
7 . The turbocharger as in claim 1 , wherein the sealing material is provided at the device end of the bore.
8 . The turbocharger as in claim 1 , wherein the sealing material is provided at the actuator end of the bore.
9 . The turbocharger as in claim 1 , wherein the sealing material is provided outside the turbine housing or bearing housing, in a space between the bore and the actuating mechanism.
10 . The turbocharger as in claim 1 , wherein the shaft is mounted in a bore in the turbine housing or bearing housing.
11 . The turbocharger as in claim 1 , wherein the shaft is mounted in a bore in a bushing extending through the turbine housing or bearing housing.
12 . The turbocharger as in claim 1 , further comprising a circumferential groove provided in at least one of said shaft and said bore, wherein at least one generally annular solid non-permeable seal member is provided in the circumferential groove.
13 . The turbocharger as in claim 12 , wherein the seal member is a seal ring.
14 . The turbocharger as in claim 13 , wherein the sealing material is provided between two seal rings.
15 . The turbocharger as in claim 13 , wherein the sealing material is provided either outboard of the seal ring or inboard of the seal rings.Join the waitlist — get patent alerts
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