Information
-
Patent Grant
-
6672425
-
Patent Number
6,672,425
-
Date Filed
Wednesday, July 24, 200223 years ago
-
Date Issued
Tuesday, January 6, 200421 years ago
-
Inventors
-
Original Assignees
-
Examiners
Agents
- Bracewell & Patterson LLP
-
CPC
-
US Classifications
Field of Search
US
- 181 252
- 181 264
- 181 265
- 181 278
- 181 281
- 181 259
- 181 267
-
International Classifications
-
Abstract
The current invention is device for lowering the air velocity and inherent noise of high-speed air released from a closed system, comprising a straight pipe module with an outer tube and a concentric inner tube creating an annular space therebetween. The inner tube has interior fins at the inlet, which initiate rotation in an airflow directed therethrough, and interior fins at the outlet, which arrest the airflow rotation. Perforations along the length of the inner tube, from inlet fins to outlet fins, permit the release of a turbulent outer zone of the airflow, permitting the high velocity core of the airflow to expand and slow, reducing the noise of the airflow.
Description
CROSS-REFERENCE TO RELATED APPLICATIONS
Not applicable.
STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT
Not applicable.
BACKGROUND OF THE INVENTION
1. Field of Invention
This invention relates to a noise abatement system for lowering air velocity in a closed system. Specifically, the invention describes a straight pipe module suppressor, with internal vanes, which reduces the velocity of air used in an industrial airblow cleaning operation.
2. Description of the Related Art
High pressure/high velocity air may be used to clean industrial piping. Reference to cleaning in this application is the process of removing loose and/or lightly adhered debris from piping. The piping to be cleaned may be that which is used in the operation of a power generating plant by providing steam to turbines, in a petrochemical plant to provide stock or product to a process or storage unit, or in any other environment using piping that is typically operated under high pressure and/or high temperature.
The piping to be cleaned may be new fabrication, which may nonetheless contain dirt, sand, loose bolts, used welding rods or other non-structural items or debris left from the fabrication process. Alternatively, the piping to be cleaned may already have been in service and in need of cleaning to remove built-up material (usually scaling) on the interior of the piping. Typically, cleaning of piping that has been in service is accomplished by first flushing the line with a chemical flush to loosen the mill scale, which is solubilized into a solution. The line is then rinsed, and the metal neutralized (washed) to remove the solution containing the chemical flush and the soluble scale particles. The remaining loose or lightly adhered insolubles left in the piping are then removed with the high-pressure air.
Debris from either new fabrication or scaling can damage downstream equipment, such as a turbine, processing unit or other equipment/systems. For example, high pressure impingement of debris on turbine blades operating at high speed could result in damage or catastrophic failure of the turbine.
In a typical pipe cleaning operation, the piping to be cleaned is connected at its upstream end to an air pressurization system, typically a pressure vessel and/or piping, and at its downstream end to a temporary bypass line. The temporary bypass line diverts the high pressure cleaning air away from downstream equipment.
In either use of high pressure air for cleaning piping (new or used), the air pressurization system is typically charged to a level sufficient to provide air pressure through the piping 1.2 times the normal operating pressure of the piping. This high pressure air passes through the piping and is discharged along with the debris out of the piping.
If the high pressure cleaning air, typically traveling at or above sonic speed through the piping, is released directly to the environment without velocity suppression, the noise is intolerable. It is not unusual for such a release to generate noise levels between 115 dB and 140 dB, which can cause hearing loss to those nearby and structural damage or nuisance several miles away. Further, high pressure air can penetrate the skin of a person exposed to the exhaust airflow. This air penetration through the skin can cause air embolisms in the blood vessels, which can be fatal. Thus an air velocity suppression/reduction system is needed in such environments.
Air velocity suppressors for high pressure/high velocity air used to clean piping air are found in the prior art. However, these silencers typically use a baffle system to reduce the velocity of the air. These create unwanted backpressure that reduces the velocity of the air upstream in the cleaning process, thus creating the requirement for higher initial air velocity.
Other air velocity/noise suppressors use a muffling device with a closed cap end, and direct all airflow laterally outward through release holes in the sides of the inner and outer pipes of the suppressor. This system is dangerous when used with high velocity/high pressure stream, since sudden blockage of the release holes, as from a large piece of debris, will cause immediate over-pressurization of the suppressor and likely explosion.
Air suppressor systems used in low velocity applications, such as mufflers used on internal combustion machines or small scale pneumatic silencers on leaf blowers and the like, are unacceptable in high pressure/high velocity air cleaning systems. These low velocity devices, even if scaled up, are unable to adequately reduce the volume and velocity of high-pressure air being exhausted from the system due to their structural and design limitations.
BRIEF SUMMARY OF THE INVENTION
Accordingly, the objectives of this invention are to provide, inter alia, a new and improved air suppression system that:
Does not create undue back pressure;
Does not pose a risk of sudden blockage;
Reduces high air velocity, including those about sonic speed;
Uses standard fabrication components; and
Is cost effective.
These objectives are addressed by the structure and use of the inventive device. A straight through pipe has air directing internal vanes attached to the interior wall of an inside tube. The walls of the inside tube are perforated to permit airflow separated from the main air stream to escape to a space between the inside tube and the outside tube. These vanes cause the high velocity air to rotate about its directional axis. Laminar resistance of the rotation causes a tail of air to form, moving away from the center or core of the exhaust stream and against the interior wall of the inside tube. The high velocity air being released into the inside tube has an exhaust
15
shape shown in
FIGS. 6 and 6A
, comprising a outer layer
19
and a core
17
. Outer layer
19
is formed as laminar resistance allows side air to move away from the center of exhaust
15
, while the faster air of core
17
speeds through the center of the inner tube
30
. By directing exhaust
15
to rotate about its linear axis, outer layer
19
is “chewed away” as its air is directed into velocity dampening areas between the inside tube
30
and the outside tube
20
of the invention. As outer layer
19
is removed, it is replaced by air from core
16
, thus decreasing the overall velocity of exhaust
15
.
Other objects of the invention will become apparent from time to time throughout the specification hereinafter disclosed.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1
depicts a single inventive noise abatement module.
FIG. 2
depicts an inlet view of the single noise abatement module of FIG.
1
.
FIG. 3
depicts an outlet view of the single noise abatement module of FIG.
1
.
FIG. 4
depicts a side view of either a single inlet vane or outlet vane.
FIG. 5
depicts a top view of an inlet vane showing its oblique offset from the axial centerline of the direction of inlet airflow.
FIG. 5A
depicts a top view of an inlet vane with no offset.
FIG. 6
a view of the regions of high velocity air as it travels through the inner tube of
FIG. 1
, cut at line
6
—
6
.
FIG. 6A
is a view of the regions of high velocity air as it travels through the inner tube of
FIG. 1
, cut at line
6
A—
6
A.
FIG. 7
depicts the use of multiple noise abatement modules.
DETAILED DESCRIPTION OF THE INVENTION
The present invention comprises the module shown as noise abatement module
10
, depicted in
FIGS. 1
,
2
and
3
. Noise abatement module
10
comprises an inside tube
30
that is connected at each end to stubs
24
, which are attached to flanges
40
. Each flange
40
has a flange face
42
and typically flange bolt holes
44
for mating with and bolting to piping and/or other noise abatement modules
10
. Circumferential about inside tube
30
is outside tube
20
, defining annular inside space
33
. Outside tube
20
has outside tube ends
22
that define the inlet and outlet boundaries of inside space
33
between inside tube
30
and outside tube
20
.
An insulating material
34
may be position in space
33
between inside tube
30
and outside tube
20
. When used in noise abatement module
10
, insulating material
34
may be supported in place by expanded material
36
. Expanded material
36
is rigid enough to hold insulating material
34
in place in space
33
, yet is flexible to be shaped around insulating material
34
and inside tube
30
, as well as permeable to air. In the exemplary embodiment, the insulating material is a blanket of insulation, typically fiberglass or kaowool. Also in the exemplary embodiment as expanded material
36
is a sheet of wire mesh
34
, wrapped around the insulation blanket
34
to hold the insulating material
34
in place between the inner wall of outside tube
20
and the outer wall of inside tube
30
.
The diameters of inside tube
30
and outside tube
20
are any that can accommodate the high velocity airflow to be suppressed. In typical applications of noise abatement module
10
being used to abate noise from industrial pipe and vessel air cleaning, inside tube
30
typically has an inner diameter of 30″ to 38″ (76.2 cm to 96.5 cm), and outside tube
20
typically has an inner diameter of 40″ to 54″ (101.6 cm to 147.2 cm).
Inside tube
30
has inside tube perforations
32
, which are typically ⅛″ to ⅜″ (3.2 mm to 15.9 mm) in diameter. In the exemplary embodiment, inside tube perforations
32
are intermediate inlet vanes
50
and outlet vanes
51
.
Inlet vanes
50
are attached to the interior wall of inside tube
30
at the air inlet side
27
. In the exemplary embodiment inlet vanes
50
are six in number and circumferentially equally spaced, as shown in FIG.
2
. As shown in
FIG. 4
, each inlet vane
50
has a vane base
52
and a vane first end
53
and a vane second end
54
. Vane second end
54
is a trailing end as viewed by the airflow past inlet vane
50
. Airflow travels first past first vane end
53
, past the length of inlet vane
50
, and then past vane second end
54
. Vane base
52
is attached to the interior wall of inside tube
30
, typically with a weld. In an exemplary embodiment where inside tube
30
has a 36″ (91.4 cm) inner diameter, vane base
52
is 8″-16″ (20.3 cm to 40.6 cm), vane first end
54
is 1″-3″ (2.5 cm to 7.6 cm) high, and vane second end
53
is less than ½″ (12.7 mm). As shown in
FIG. 5
, an inside tube centerline
31
is referenced at each inlet vane
50
, which passes through vane first end
53
and runs parallel with the length of inner tube
30
along the inner wall. Each inlet vane
50
is oriented oblique to an inside tube centerline
31
. In the exemplary embodiment an offset angle
35
is 0.5° to 2.0°. Such an angle results in inlet vane offset A being approximately 0.25″ (6.3 mm) where vane base
52
is 12″ (30.5 cm). Each inlet vane
50
is thus offset obliquely to its own inside tube centerline
31
while remaining normal to the interior wall of inside tube
30
, as depicted in FIG.
2
. While inlet vane
50
is shown in
FIG. 5
as a straight vane, alternatively inlet vane
50
can have an arcuate shape (not shown) that results in the same amount of inlet vane offset A as described above for a straight vane.
Outlet vanes
51
are attached to the interior wall of inside tube
30
at the air outlet side
28
. In the exemplary embodiment outlet vanes
51
are four in number and circumferentially equally spaced as shown in FIG.
3
. An exemplary outlet vane
51
is also depicted in
FIG. 4
as having the same shape and dimensions as inlet vane
50
when inlet vane
50
is a straight vane. Referring to
FIGS. 3
,
5
and
5
A, the key difference between outlet vanes
51
and inlet vanes
50
is that outlet vanes
51
each align along an inside tube centerline
31
with no offset A. Each outlet vane
51
is thus aligned with its own inside tube centerline
31
while remaining normal to the interior wall of inside tube
30
.
Referring to
FIG. 7
, noise abatement module
10
may be used singularly or in conjunction with other noise abatement modules
10
or other systems. For example, noise abatement modules
10
may be aligned in series. Alternatively and additionally, noise abatement modules
10
may include Y-connector
26
to afford parallel alignment as well where the outlet end stub
24
of noise abatement module
10
is joined to the inlet end stub
24
of noise abatement module
10
′.
OPERATION
Referring to
FIGS. 1
,
2
,
3
,
6
, and
6
A, noise abatement module
10
is attached to piping or equipment (not shown) from which high pressure air is being exhausted. This is typically accomplished by bolting flange
40
at inlet side
27
to an equipment outlet flange (not shown), thus providing sealed fluid communication between the exhaust air and the interior of noise abatement module
10
. High velocity air enters inside tube
30
through the center opening in flange
40
at inlet side
27
, and is rotated about its linear axis by inlet vanes
50
. This causes outer layer
19
of exhaust
15
to rotate about this linear axis, forcing air into space
33
through inside tube perforations
32
, where it is slowed, and high velocity air from core
17
is allowed to expand and move into outer layer
19
. Thus exhaust
15
is “chewed” until it has less and less high velocity air.
When the exhaust air nears air outlet side
28
, it encounters outlet vanes
51
, which stop the rotation of the exhaust air, baffling even more of the exhaust gas outer layer
19
, and further “chewing” away outer layer
19
. Piping between outlet vanes
51
and the exit flange
40
, typically 24″-48″ (61.0 cm to 121.9 cm) long and including stub
24
and/or a portion of inside tube
30
, acts as a buffer zone to allow the exhaust air to stabilize back to its original linear flow direction.
When used in either or both series and parallel as shown in
FIG. 7
, each transition through a noise abatement module
10
results in further decrease in the velocity of the air and its attendant noise. The air is finally exhausted to the atmosphere or additional air directing equipment, such as an upward plenum.
The foregoing disclosure and description of the invention is illustrative and explanatory thereof. Various changes in the details of the illustrated construction may be made within the scope of the appended claims without departing from the spirit of the invention. The present invention should only be limited by the following claims and their legal equivalents.
Claims
- 1. A noise abatement module comprising:an inside tube having an interior, an inlet side, an outlet side and a centerline; an outside tube; said outside tube circumferentially about said inside tube; a space defined by the inside of said outside tube and the outside of said inside tube; a plurality of inside tube perforations on said inside tube; said perforations providing fluid communication between said interior of said inside tube and said space; a plurality of inlet vanes inside said inside tube and proximate said inlet side of said inside tube; said inlet each having a first vane end and a second vane end; said second vane end of each inlet vane each being obliquely offset from the centerline of said inside tube; and a plurality of outlet vanes inside said inside tube and proximate said outlet side of said inside tube.
- 2. The noise abatement module as in claim 1, further comprising:said inner tube having an inner wall; and said plurality of inlet vanes and said plurality of outlet vanes attached to said inner wall of said inside tube.
- 3. The noise abatement module as in claim 1, further comprising:an insulation blanket oriented in said space.
- 4. The noise abatement module as in claim 1, further comprising:expanded material supporting said insulation blanket.
- 5. The noise abatement module as in claim 1, wherein each said plurality of outlet vanes aligned along the centerline of said inside tube.
- 6. The noise abatement module as in claim 1, wherein said plurality of inlet vanes numbers six.
- 7. The noise abatement module as in claim 1, wherein said plurality of inlet vanes numbers four.
- 8. The noise abatement module as in claim 1, wherein:said outlet side of said inside tube connecting to said inlet side of said inside tube of a subsequent said noise abatement module.
- 9. The noise abatement module as in claim 1, wherein:a Y-connector having an inlet end and at least two outlet ends; said outlet side of said inside tube connecting to said inlet end of said Y-connector; and said each at least two outlet ends on said Y-connector connecting to said inlet side of said inside tube of a subsequent said noise abatement module.
- 10. The noise abatement module as in claim 1, comprising:and inside tube having an interior, an inner wall, an inlet side and a centerline; an outside tube; said outside tube circumferentially about said inside tube; a space defined by the side of said outside tube and the outside of said inside tube; a plurality of inside tube perforations on said inside tube; said perforations providing fluid communication between said interior of said inside tube and said space; an insulation blanket oriented in said space; an expanded material supporting said insulation blanket; a plurality of inlet vanes attached to said inner wall of inside tube and proximate said inlet side of said inside tube; said inlet vanes each having a first vane and a second vane end; said second vane end of each inlet vane each being obliquely offset from the centerline of said inside tube; a plurality of outlet vanes attached to said inner wall of inside tube and proximate said outlet side of said inside tube; and each of said plurality of outlet vanes aligned along the centerline of said inside tube.
- 11. The noise abatement module as in claim 10, wherein multiple modules are connecting in series.
- 12. The noise abatement module as in claim 10, wherein multiple modules are connecting in parallel.
- 13. A method of abating noise from a high velocity air, said method comprising:directing said high velocity air through a noise abatement module, said noise abatement module comprising an inside and an outside tube; rotating said high velocity air about an airflow axis, said rotation effected by a plurality of inlet vanes attached to an interior wall of said inside tube, said inlet vanes having a trailing end oriented obliquely offset from centerline of said inside tube; directing, through a plurality of inside perforations in said inside tube, said rotated air into a space between said inside tube and sad outside tube; reducing an air velocity of said high velocity air in said space and an interior of said inside tube; and redirecting said high velocity air exiting said noise abatement module into a liner direction along said airflow axis with a plurality of outlet vanes attached to said inner wall of said inside tube, said outlet vanes being proximate an outlet side of said inside tube and aligned along the centerline of said inside tube.
US Referenced Citations (9)