Information
-
Patent Grant
-
6401590
-
Patent Number
6,401,590
-
Date Filed
Monday, July 24, 200024 years ago
-
Date Issued
Tuesday, June 11, 200222 years ago
-
Inventors
-
Original Assignees
-
Examiners
- Carone; Michael J.
- Chambers; Troy L.
Agents
-
CPC
-
US Classifications
Field of Search
US
- 089 111
- 169 36
- 440 88
- 440 89
- 701 36
- 070 168
- 070 256
- 180 309
-
International Classifications
-
Abstract
A flow blocking device is lowered by cable from a helicopter for insertion into the exhaust gas stack of a fuel burning combustion engine propelling a marine vessel under full engine speed. The wall of the exhaust stack are engaged upon entry of the flow blocking device to insure its retention within the exhaust stack and to initiate in sequence ejection of cooling water into the outflow of the exhaust gas followed by pressurized gas expansion of a flexible hose portion of the flow blocking device into sealing contact with the walls of the exhaust stack to stop exhaust gas outflow and cause back pressure build up to a high engine shut down level.
Description
The present invention relates generally to shut down of propulsion engines of marine vessels during seaway travel.
BACKGROUND OF THE INVENTION
Devices for plugging of tubular pipes to block flow of fluids therethrough, are generally well known. It is also well known in the art, that build up of exhaust back pressure to certain high levels in fuel burning combustion engines, will cause engine shut down. It is an important object of the present invention to produce such engine shut down without engine damage under high temperature and full engine speed conditions by exhaust gas flow blockage to cause sufficient back-up pressure build-up.
SUMMARY OF THE INVENTION
In accordance with the present invention, engine shut down by build up of exhaust back-up pressure is effected by insertion of a flow blocking device into an engine exhaust stack during outflow of the exhaust gas therefrom under full engine speed. Pursuant to certain embodiments of the invention, such flow blocking device is inserted by cable lowering from a helicopter into the exhaust stack associated with the fuel burning propulsion engine of a marine vessel undergoing seaway travel at full engine speed. Entry of the flow blocking device into the exhaust stack stops outflow of the exhaust gas to cause back pressure build-up therein. The requisite duration for such flow blocking action is insured according to one embodiment by mechanical means after entry of the flow blocking device, to prevent its ejection from the stack by the back pressure build-up therein. Also, according to other embodiments a sequence of events is initiated after the flow blocking device reaches a lowermost position within the exhaust stack to perform the flow blocking function. Such events may include water cooling of the exhaust gas to low temperature conditions within the exhaust stack under which a flexible portion of the flow blocking device is inflated or expanded into contact with the stack for pressurized sealing there to block exhaust outflow until engine shut down occurs.
BRIEF DESCRIPTION OF DRAWING
A more complete appreciation of the invention and many of its attendant advantages will be readily appreciated as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawing wherein:
FIG. 1
is a block diagram depicting the environment of the present invention;
FIG. 2
is a side elevation view of an exhaust flow blocking device in accordance with one embodiment, being lowered into an engine exhaust stack;
FIG. 3
is a partial section view taken substantially through a plane indicated by section line
3
—
3
in
FIG. 2
;
FIG. 4
is a partial section view of the exhaust flow blocking device shown in
FIGS. 2 and 3
, in a fully lowered position within the engine exhaust stack; and
FIG. 5
is a partial section view taken substantially through a plane indicated by section line
5
—
5
in FIG.
4
.
DETAILED DESCRIPTION OF PREFERRED EMBODIMENT
Referring now to the drawing in detail,
FIG. 1
diagrams a system
10
for shut down of a full burning combustion engine
12
utilized for propulsion of a marine vessel or ship. Engine shut down is effected without damage by blockage of the engine exhaust
14
, causing build up of engine back pressure to a high shut down level. Such blockage of engine exhaust is performed with respect to the propulsion engine
12
of a marine vessel while underway at sea, by blockage of its exhaust
14
having an exhaust stack
16
associated therewith as shown in FIG.
2
.
With continued reference to
FIG. 2
, the engine shut down system
10
of the present invention involves lowering of an exhaust flow blocking device
18
, dimensioned to fit into the exhaust stack
16
, while the marine vessel is underway. The device
18
is accordingly suspended from a helicopter
20
for such purpose by a cable
22
connected at its lower end to a pair of slide-up attachment brackets
24
secured to the upper end of a cylindrical gas pressure canister
26
associated with the device
18
. The canister
26
is held assembled in axial relationship to a nose cone
28
by a tubular flexible hose
30
clamped adjacent its upper and lower axial ends to the canister
26
and the nose cone
28
by pairs of bands
32
as shown in FIG.
2
. Also associated with the device
18
is a cross-bar
34
slidably mounted on the attachment brackets
24
. On the upper end of the canister
26
several radially projecting pawls
36
are mounted. Secured to the underside of the cross-bar
34
is the upper end of an actuator cable
38
, the lower end of which is attached to a valve trigger element
40
projecting from the lower tip end of the nose cone
28
. The valve trigger element
40
when actuated through cable
38
as hereinafter explained, is operative to cause ejection of pressurized cooling liquid such as water from openings
42
in the nose cone
28
, in close spaced surrounding relation to the tip end location of the valve trigger element
40
. Thus, engine exhaust blockage is initiated by entry of the device
18
into the stack
16
at its upper rim formed by a top edge
44
, from which exhaust gas
46
emerges during engine operation at full speed.
As shown in
FIG. 3
, the canister
26
filled with pressurized gas, such as nitrogen, has a normally closed gas valve
48
connected to its lower end from which pressurized gas may be ejected upon opening of the valve
48
into an expansion chamber enclosed by the hose
30
for expansion thereof from the contracted condition shown. The expansion chamber is formed within the hose
30
axially between the locations at which the hose is clamped by the bands
32
to the canister
26
and the nose cone
28
. Such hose
30
is accordingly made of a suitable nonlinear orthotropic composite material composed of rubber and fibers, with the fibers layed-up so that the hose expands in diameter when internal gas pressure is applied thereto between 40 and 80 psi for example, upon opening of the valve
48
. Associated with such valve
48
is a pressure responsive actuator
50
connected by tube
52
to the upper end of a pressurized cooling liquid tank
54
formed within the nose cone
28
. The lower end of the tank
54
is connected to a normally closed valve
56
opened by actuation of the valve trigger element
40
through cable
38
. Opening of the valve
56
accordingly supplies pressurized liquid such as water from tank
54
to galleries
58
from which the water is ejected from the nose cone openings
42
.
The valve
56
is opened by the trigger element
40
after the device
18
descends into exhaust stack
16
causing the cross-bar
34
to abut the upper stack edge
44
as shown in FIG.
4
. The cross-bar
34
is thereby displaced upwardly relative to the device
18
as it continues to be lowered into the stack
16
until it reaches the position shown in
FIG. 4
, automatically exerting a pulling force through cable
38
on the valve trigger element
40
to initiate exhaust blockage of the stack
16
. The pressurized water from tank
54
is thereby ejected from the nose cone
28
through openings
42
into the exhaust gas
46
for mixing therewith so as to be vaporized and cool the exhaust stream as well as the wall surfaces within the stack
16
. Such cooling effect is related to the properties of the material of hose
30
so as to maintain most or all of its room temperature strength.
As the device
18
is being lowered into the stack
16
, the pawls
36
make contact with the top edge
44
of the stack at its upper rim and are pushed radially inwardly against spring bias exerted for example by springs
60
shown in FIG.
5
. Such spring bias maintains the pawls
36
in contact with the stack walls. Should the canister
26
be urged in an upward direction, the sharpened tips of the pawls
36
dig into the stack wall so as to prevent upward displacement of the device
18
. Such upward urge could be imposed on the canister
26
by subsequently developed pressures therebelow within the stack
16
.
As the cooling water leaves tank
54
for ejection into the emerging engine exhaust, the tank pressure drops. When such tank pressure drops below a preset value, it is sensed by valve actuator
50
to open gas valve
48
through which the pressurized gas from canister
26
fills the expansion chamber void inside of the hose
30
and then causes its expansion into sealing contact with the walls of the stack
16
as shown in FIG.
4
. Exit of exhaust gas from the stack is then blocked by such sealing action of the hose
30
caused by the canister gas producing back pressure build up to a level causing shut down of the engine. The pawls
36
assist and/or insure retention of the device
18
within the stack
16
under the high level back pressure.
Obviously, other modifications and variations of the present invention may be possible in light of the foregoing teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.
Claims
- 1. In combination with a fuel burning combustion engine having an exhaust stack from which outflow of exhaust gas occurs under full engine speed, a system for shut down of engine operation comprising: a flow blocking device; and cable means lowered from a helicopter for inserting said flow blocking device into the exhaust stack to stop said outflow of the exhaust gas therefrom under full engine speed; said flow blocking device including sealing means expanded into contact with the stack upon entry thereinto for blocking said outflow of the exhaust gas to effect build up of back pressure to an engine shut down level.
- 2. The combination as defined in claim 1, wherein said exhaust stack has an upper rim and said flow blocking device further includes: mechanical means engageable with said upper rim of the exhaust stack for preventing ejection of the flow blocking device therefrom by said build up of the back pressure.
- 3. The flow blocking device as defined in claim 2, further including: a nose cone having a source of pressurized cooling liquid therein; and valve means connected to said source for discharge of the pressurized cooling liquid from the nose cone into the exhaust gas within the stack in response to displacement of the flow blocking device to a lowermost position within the exhaust stack establishing cooled temperature conditions therein preceding operation of the sealing means.
- 4. The flow blocking device as defined in claim 3, wherein said sealing means includes a canister of pressurized gas; a flexible hose interconnecting the canister and the nose cone to form an expansion chamber therebetween; and pressure control means responsive to depressurization of said source of the pressurized cooling liquid for ejecting the pressurized gas from the canister into the expansion chamber to seal the exhaust stack after the cooled temperature conditions are established.
- 5. In combination with a fuel burning combustion engine having an exhaust stack from which outflow of exhaust gas occurs under full engine speed, a system for shut down of engine operation comprising: a flow blocking device; and means for inserting said flow blocking device into the exhaust stack to stop said outflow of the exhaust gas therefrom under full engine speed; said flow blocking device including: sealing means expanded into contact with the stack upon entry thereinto for blocking said outflow of the exhaust gas to effect build up of back pressure to an engine shut down level; a nose cone having a source of pressurized cooling liquid therein; and valve means connected to said source for discharge of the pressurized cooling liquid from the nose cone into the exhaust gas within the stack in response to displacement of the flow blocking device to a position within the exhaust stack establishing cooled temperature conditions therein preceding operation of the sealing means.
- 6. The flow blocking device as defined in claim 5, wherein said sealing means includes a canister of pressurized gas; a flexible hose interconnecting the canister and the nose cone to form an expansion chamber therebetween; and pressure control means responsive to depressurization of said source of the pressurized cooling liquid for ejecting the pressurized gas from the canister into the expansion chamber to seal the exhaust stack after the cooled temperature conditions are established.
- 7. In combination with a fuel burning combustion engine having an exhaust stack from which outflow of exhaust gas occurs under full engine speed, a system for shut down of engine operation comprising: a flow blocking device; and means for inserting said flow blocking device into the exhaust stack to stop said outflow of the exhaust gas therefrom under full engine speed; said flow blocking device including: sealing means expanded into contact with the stack upon entry thereinto for blocking said outflow of the exhaust gas to effect build up of back pressure to an engine shut down level; said sealing means including a canister of pressurized gas; a flexible hose interconnecting the canister and the nose cone to form an expansion chamber therebetween; and pressure control means for ejecting the pressurized gas from the canister into the expansion chamber to seal the exhaust stack.
US Referenced Citations (11)