U.S. patent number 3,712,032 [Application Number 05/091,118] was granted by the patent office on 1973-01-23 for high speed centrifugal air-oil separator.
Invention is credited to Alvaro Obligado.
United States Patent |
3,712,032 |
Obligado |
January 23, 1973 |
**Please see images for:
( Certificate of Correction ) ** |
HIGH SPEED CENTRIFUGAL AIR-OIL SEPARATOR
Abstract
An air-oil separator is constructed as an integral part of a
gear box and it includes a rotating cylindrical housing in which
are mounted an axially positioned radial deflector and a plurality
of radial vanes for centrifuging the oil-air mixture. The heavier
oil displaces the lighter air creating a pool of oil on the inner
surface of the cylinder. The pool of oil is permitted to flow
through radially disposed holes in the housing but is maintained at
a sufficient depth to provide a seal against the escape of air
which is vented axially overboard.
Inventors: |
Obligado; Alvaro (Portchester,
NY) |
Family
ID: |
22226183 |
Appl.
No.: |
05/091,118 |
Filed: |
November 19, 1970 |
Current U.S.
Class: |
55/409 |
Current CPC
Class: |
B01D
45/14 (20130101); F01M 2013/0422 (20130101) |
Current International
Class: |
B01D
45/12 (20060101); B01D 45/14 (20060101); F01M
13/04 (20060101); F01M 13/00 (20060101); B01d
045/12 () |
Field of
Search: |
;55/409 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Miles; Tim R.
Claims
I claim:
1. An air-oil separator comprising:
a hollow rotating cylinder;
an axial opening in one end of said cylinder, said opening
providing an inlet admitting a mixture of air and oil thereto;
an axial opening in the opposite end of said cylinder, said opening
providing an air outlet from said cylinder;
a plurality of passages in the periphery of said cylinder, said
passages providing radial oil outlets through said cylinder, said
passages being sized to maintain a pool of oil on the inner
cylindrical surface of said cylinder to provide a seal for
preventing the flow of air through said passages;
an axially positioned radial deflector fixed to said cylinder, said
deflector intercepting said air-oil mixture and radially deflecting
said mixture to the inner surface of said cylinder;
and a plurality of axially and radially extending vanes fixed to
the inner cylindrical surface of said cylinder, said vanes
imparting a centrifugal force to said mixture.
2. The invention as defined in claim 1 wherein said radial
deflector has a curved surface of revolution having a 90.degree.
arc with its apex positioned on the axis of said cylinder and
facing said inlet.
3. An air-oil separator comprising in combination:
a rotating gear affixed to a hollow cylindrical rotating shaft,
said shaft being partially closed at both ends;
an axial inlet in one end of said shaft for admitting an air-oil
mixture;
an axial outlet in the other end of said shaft for exhausting air
therefrom;
a plurality of oil outlet passages radially extending through the
cylindrical surface of said shaft, said passages being sized to
maintain a pool of oil on the inner cylindrical surface of said
cylinder to provide a seal for preventing the flow of air through
said passages;
a radial deflector fixed within said shaft adjacent said inlet,
said deflector intercepting and deflecting said air-oil mixture
radially toward the inner cylindrical surface of said shaft;
and a plurality of axially and radially extending vanes affixed to
the inner cylindrical surface of said shaft for imparting a
centrifugal force to said air-oil mixture, whereby said air and oil
are separated and said oil exits through said plurality of oil
outlet passages, and whereby said air is exhausted through said air
outlet.
4. The invention as defined in claim 3 wherein said vanes extend
radially from said inner surface to the surface of said
deflector.
5. The invention as defined in claim 4 wherein said vanes extend
axially the entire distance between said inlet and said outlet.
6. The invention as defined in claim 5 wherein said radial
deflector has a curved surface of revolution having a 90 degree arc
with its apex positioned on the axis of said shaft and facing said
inlet.
Description
Background of the Invention
The present invention is designed for use in connection with the
gear box of a gas turbine engine or other rotating machinery. In
such applications it is well known that the pressurizing air for
such systems must be vented, that is to say, the air entrapped in
the lubricating oil must be separated from the oil and discharged
overboard without the significant loss of oil from the gear box.
While many systems of this type are known to the prior art, the
present invention accomplishes the air-oil separation in a
self-contained compact gear arrangement which operates with
essentially 100 percent efficiency, i.e., the air removed without
significant loss of oil.
THE DRAWINGS
FIG. 1 is an end view of an illustrative embodiment of this
invention; and
FIG. 2 is a cross section taken through the line 2--2 of FIG.
1.
Brief Summary of the Invention
The disclosed air-oil separator is intended for use in a gear box
and is incorporated as an integral part of one of the gear shafts.
It allows venting of large quantities of air directly overboard
without significant loss of oil. The design concept of the
separator is based on the centrifugal pump. Its advantages are its
positive separation mechanism, its compact size and its ability to
operate under a gear box environment with large quantities of air
and oil. The invention utilizes an axially positioned radial
deflector in combination with a plurality of radially disposed
vanes which serve to impart a centrifugal force to the oil and air.
The oil is discharged from the separator through radially disposed
passages. The air exits axially downstream from the incoming
air-oil mixture.
Description of the Illustrated Embodiment
The disclosed air-oil separator is incorporated as an integral part
of a hollow cylindrical shaft 10 of a conventional gear 12. The
gear 12 is incorporated in a gear box (not shown).
The hollow shaft 10 provides a cylindrical housing into which the
centrifuge elements are press fitted. The centrifuge elements
include an axially positioned radial deflector 14 supported by a
plurality of radially disposed vanes 16. The vanes 16 are in turn
supported by a centrally apertured disk 18 and are made integral
with the disk 18. The centrally located aperture in the disk 18
provides an inlet port 20 in axial alignment with the radial
deflector 14.
A slightly positive gear box pressure forces the mixture of air and
oil into the shaft 10 through the axial inlet port 20. The radial
deflector 14 is provided with a curved surface of revolution having
a 90 degree arc with its apex facing the inlet port 20. Thus, the
air-oil mixture intercepted by the deflector 14 is radially
deflected outwardly towards the radial vanes 16 which then
centrifuge the mixture and impels it radially against the inner
surface of the hollow shaft 10. The heavier oil displaces the
lighter air creating a pool of oil 22 on the inner surface of the
cylinder. The pool of oil 22 is maintained at a depth from zero to
an allowable maximum which is determined by the dimensions of the
inlet port 20 and an exit port 24 as compared with the inner
diameter of the hollow shaft 10 and the diameter of the deflector
14, and by the size of the orifices 26 through which the oil is
permitted to escape in a controlled manner back into the gear box.
The orifices 26 are sized on the basis of expected oil flow rates
and developed centrifugal oil pressure. With the apertures 26
sealed to the flow of air, the separated air is forced to exit
through the exit port 24 and is exhausted through a second shaft 28
to the atmosphere.
The efficiency of the separator increases with rotational velocity
and decreases with increasing air flow. The pressure drop across
the unit is mainly a function of the air flow rate and separator
efficiency and size. Rotational velocity has only a slight effect
on pressure drop.
It is noted that the vanes 16 axially extend the entire length of
the separator housing. However, the vane is radially longer at the
inlet side of the housing than it is at the outlet side. This has
some effect on reducing the impedance to the radial inward flow of
air, but a symmetrically shaped vane would also provide
satisfactory operation of the separator.
It is also noted that the separating efficiency will not suffer
should the oil pool 22 be of zero level since the developed
centrifugal air pressure will, in general, be far too low to force
an appreciable quantity of air through the orifices 26.
The advantages of this separator are its compact size and its
ability to operate under most any turbulent gear box environment
with large quantities of air and oil and without significant loss
of energy and efficiency. It allows the venting of large quantities
of air overboard without any loss of oil.
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