U.S. patent number 3,789,231 [Application Number 05/333,517] was granted by the patent office on 1974-01-29 for vapor detector safety system.
Invention is credited to Arthur G. Hayden.
United States Patent |
3,789,231 |
Hayden |
January 29, 1974 |
VAPOR DETECTOR SAFETY SYSTEM
Abstract
A combustible vapor detector system providing both a
proportional visual reading and a simultaneous switching function
in a common instrument includes a meter relay and a vapor sensor
remotely located in a compartment likely to have an accumulation of
combustible vapors which operably coupled to the meter relay to
control its reading at an operator's console and a plurality of
switching sectors associated with the meter relay arranged to
sequentially operate several independent circuits within selected
meter ranges so a "safe" or "caution" condition will be indicated
with auxilliary elements, such as lights or audible elements, apart
from the meter readings, and a "danger" condition will trigger a
disabling circuit to stop or prevent the start-up of any machinery
located in the compartment containing the sensor. The switching
sectors may also be employed to operate a blower to purger the
compartment of any accumulation of combustible vapors and the
"danger" condition can also be employed to shut off all
electrically controlled machinery located in the compartment having
the vapor sensor or elsewhere.
Inventors: |
Hayden; Arthur G. (Walnut
Creek, CA) |
Family
ID: |
23303120 |
Appl.
No.: |
05/333,517 |
Filed: |
February 20, 1973 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
Issue Date |
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198555 |
Nov 15, 1971 |
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Current U.S.
Class: |
307/9.1; 114/211;
340/632 |
Current CPC
Class: |
F02N
15/10 (20130101); B63J 2/06 (20130101); F02P
11/02 (20130101) |
Current International
Class: |
B63J
2/06 (20060101); B63J 2/00 (20060101); F02N
15/00 (20060101); F02N 15/10 (20060101); F02P
11/00 (20060101); F02P 11/02 (20060101); B63j
002/06 () |
Field of
Search: |
;307/9,116 ;200/61.03
;340/237R,237S ;114/211 |
References Cited
[Referenced By]
U.S. Patent Documents
Primary Examiner: Hohauser; Herman
Assistant Examiner: Ginsburg; M.
Attorney, Agent or Firm: Fryer, Tjensvold, Phillips &
Lempio
Parent Case Text
CROSS-REFERENCE TO RELATED APPLICATION
This application is a continuation-in-part of application Ser. No.
198,555 filed Nov. 15, 1971 by Arthur G. Hayden, and now abandoned.
Claims
Having described my invention, I claim:
1. A vapor detector control system comprising:
a source of electrical power;
a meter relay having at least three sequential independent
switching ranges and a visual reading in all of said ranges, said
meter relay operably coupled to said source;
a first circuit having a first indicating means coupled to a first
switching range of said meter relay and being operably connected to
said source by said meter relay when said visual reading is in its
first switching range;
a second circuit having second indicating means coupled to a second
switching range of said meter relay and being operably connected to
said source when said visual reading is in its second switching
range;
a third circuit having a disabling means to render machinery in a
monitored compartment inoperable coupled to a third switching range
of said meter relay when said visual reading is in its third
switching range; and
a vapor sensor electrically coupled to said meter relay and located
in said monitored compartment where explosive organic fumes are
likely to accumulate, said sensor operable to control said visual
reading together with the respective said indicating means and
disabling means in direct relationship to the concentration of said
fumes whereby auxiliary warnings are provided when said meter
reading is in said first and second switching ranges and said
disabling means renders the machinery in said monitored compartment
inoperable when said meter reading is in the said third switching
range.
2. The vapor detector system defined in claim 1 wherein the first
indicating means is an electrical lamp and the second indicating
means is an audible alarm.
3. The vapor detector system defined in claim 1 wherein the second
circuit includes a blower means connected to the monitored
compartment and operable to purge said monitored compartment of
accumulated fumes when the meter of the meter relay reading is in
its second switching range.
4. The vapor detector system defined in claim 1 wherein a
multi-position switch is coupled between the source and the meter
relay whereby the vapor detector system can be operated
independently and in combination with other electrical
circuits.
5. The vapor detector system defined in claim 1 wherein the
disabling means is a normally closed circuit breaker which opens
its contacts when activated by said power source through the meter
relay.
Description
BACKGROUND OF THE INVENTION
In watercraft such as motor boats, and in particular inboard motor
boats, it is possible for fumes to accumulate in the engine
compartment, or other compartments, under a variety of
circumstances. Since these fumes are often combustible, it is
possible that a small spark from mechanical equipment located in
such a compartment can cause an explosion capable of destroying the
watercraft or causing a hazardous fire.
A number of patents have issued which provide various safety
systems for such watercarft that often involve delay circuits so a
blower can purge one or more compartments in the craft before the
engine is started. Typical of such patents are U.S. Pat. No.
3,315,584 issued to Van Ranst; U.S. Pat. No. 3,675,034 issued to
Abplanalp; and U.S. Pat. No. 3,489,912 issued to Hoffman. A related
circuit employing a switch associated with a fuel tank cap is
illustrated in U.S. Pat. No. 3,652,868 issued to Hunt.
While all the above safety systems will offer some degree of
protection in watercraft when properly installed, they often tend
to be limited in their effectiveness and/or complicated and
complex. Further, the fixed delay type circuits will often
unnecessarily prevent starting or restarting the engine when no
accumulation of fumes of an explosive character has occurred in the
monitored compartments of a watercraft containing mechanical
equipment that might ignite these fumes. Obviously, in emergency
situations, such as rough weather or imminent collision, a delay in
the starting cycle could lead to hazardous situations of a
different character.
It is therefore an object of the current invention to provide a
simple, yet highly reliable, vapor detector safety system that is
inexpensive, compatible with and easy to install on conventionally
configured watercraft or the like.
It is another object of the instant invention to provide a vapor
detector system that provides several separate indications of the
conditions sensed by the system which can be conveniently
designated as safe, cautionary and dangerous.
Still another object of the instant invention is the provision of a
vapor detector circuit which does not introduce needless delay in
the starting cycles of engines located in compartments where
possible dangerous accumulation of combustible fumes might occur
when such accumulations are not present.
Another object of the instant invention is the provision of a vapor
detector circuit which provides a test mode whereby the actual
conditions can be pre-monitored without activating other electrical
circuits within the watercraft which could cause explosions should
an accumulation of fumes be present and a malfunctionion such as
electrical circuits also be pre-existing.
SUMMARY OF THE INVENTION
The above objects and others can be accomplished with a combustible
vapor detector system which includes a meter relay located at an
operator's console which includes three sequentially arranged
independent switching sectors with separate circuits associated
with each of the switching sectors so these circuits are
independently operated with progressively increasing meter
indications providing sequential operation of these circuits and a
vapor sensor located in a monitored compartment and operable to
sense the presence of organic fumes with the sensor connected to
operate the meter relay when the sensor and meter relay are
energized with a source of electric power. Switching means are
included in the circuits so the meter relay can be operated
independently to sense existing conditions or in combination with
electrically powered machinery control circuits, so that the
machinery control circuits need not be energized until a
preliminary reading has been taken by the operator. Each of the
circuits designated as a safe circuit, a caution circuit and a
danger circuit includes means associated therewith to provide a
separate particular indication or a disabling action when the
particular circuit is energized through the meter relay.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is a combination diagrammatic and general schematic
illustration of the vapor detection system of this invention;
and
FIG. 2 is a circuit wiring schematic of the system shown in FIG.
1.
DESCRIPTION OF THE EMBODIMENT
Referring to FIG. 1, the vapor detector circuit 10 is shown
diagrammatically as it would be installed on a watercraft or the
like (not shown). In this figure, broken lines represent generally
the wiring connections between the several remotely located
components of this system and the meter relay 11 which is
preferably located on the control panel of the watercraft or the
like on which the system is installed. As can be appreciated when
the system has been installed on a water craft or the like, the
battery, the vapor sensor 19, the blower 21, the starting motor and
relay 23 and the circuit breaker 25 will all be located remotely of
the operator's console or control panel which is not shown. FIG. 2
shows the actual wiring schematic of the various components of the
detector system in greater detail than FIG. 1.
More particularly, from the drawings it can be appreciated that key
switch 24, which includes an "on" and a spring resisted "start"
position, is employed to activate the vapor detector system by
closing an integrally contained switch 24b that couples the battery
to a three-position switch 12 in the system when the key switch is
in the "on" or "start" position. This three-position switch can be
rotated from the "off" position to a test position 12 b. In this
test position, the vapor detector circuit is energized, but the
main electrical bus bar of the watercraft, shown in FIG. 2, is not
coupled to the battery when the system is in the test mode.
In the test mode, power is supplied to pointer 31 of the meter
relay 11 and is also coupled, through meter coil 38 and vapor
sensor 19 to ground. With respect to the vapor sensor, it can be
appreciated that multiple sensors can be employed. These sensors
are commercially available and is referred to in the aforementioned
U.S. Pat No. 3,489,912. Since the vapor sensor is remotely located
in a compartment which is to be monitored for combustible organic
fumes, such as the engine compartment of a watercraft, and is
arranged to proportionately decrease its resistance as the level of
combustible vapors in the compartment increase, the pointer 31 will
indicate a reading which is directly proportional to the level of
combustible fumes which have accumulated in the monitored
compartment at all times.
As the pointer 31 of the meter relay 11 gives a proportional
reading of the accumulated fumes which could lead to explosions or
fire, its scale can be divided into three separate independent
switching sectors which sequentially with increasing meter readings
are designated as the safe sector 16, the caution sector 17 and the
danger sector 18. For purposes of illustration, this meter relay is
shown in a most simplistic embodiment where the pointer 31
sequentially engages the sectors in a brushing contacting
relationship in order to connect battery power with each of the
sectors when the pointer is in contact with a sector. However,
since the power utilized in the several independent circuits
associated with the sectors is small, this arrangement is adequate.
It is to be appreciated that should a more sophisticated embodiment
be desired, other types of meter relays, such as that shown in U.S.
Pat. No. 2,967,278 issued to Sullivan et al, could be employed.
Further, the meter relay can be completely sealed with a glass
panel 15 so the contacts within the relay will not corrode.
As can be seen from the drawings and the simple meter relay
embodiment illustrated, each separate sector has a separate
electrical circuit associated therewith. Safe sector 16 is
connected through a filament of the green light bulb 13 to ground
and when pointer 31 brushingly engages this sector, which is the
safe range and when the pointer is in this range, the green light
will be lit.
In a similar manner, when caution sector 17 is brushingly engaged
by pointer 31, the caution range, power is supplied via a lead 32
to horn 14 and via lead 22 to blower 21.
The horn provides an audible alarm any time the pointer is in the
caution range and at the same time energizes blower 21 which is
connected to the monitored compartment in a manner so that it can
purge the compartment of accumulated fumes. As a result of the
above described circuits and arrangements, the operator is provided
with at least two independent indications of both the safe and
caution conditions of the monitored compartment as well as
automatic operation of the blower 21 in the caution range.
Because the circuit associated with danger sector 18 is essentially
a disabling circuit, its discussion will be deferred until the
operating circuits that it disables have been described. However,
it should be noted that when a dangerous condition is indicated,
i.e. when pointer 31 is brushingly contacting sector 18, the
operator can depress a spring closed manual switch shown in FIG. 2
to connect lead 22 to the battery to operate the blower so an
attempt can be made to purge the monitored compartment of any
accumulation of explosive fumes then being monitored by the
sensors. If the operation of the blower removes the accumulation of
fumes in the monitored compartment, the meter reading will swing
back through the caution range to the safe range, at which time
pointer 31 will be in contact with sector 16. When the manual
switch is released, lead is reconnected as shown in FIG. 2.
When the operator of the watercraft has completed his test check,
the three-position switch 12 can be changed to the "on" position
12c that will energize the other electrical circuits in the
watercraft via leads 40 and 41, the latter being connected to the
main electrical bus of the watercraft through circuit breaker 25.
Alternatively, the operator may choose to skip the test mode of the
vapor detector position and go directly to the "on" position
without danger, since the system will function properly in either
mode.
With the three-position switch 12 in the "on" position 12c, key
switch 24 may be rotated further counterclockwise in the "on"
position against its spring to momentarily close internal switch
24c that will temporarily energize the starting relay via lead 27
in the starting motor and relay 23, causing the battery to be
coupled directly to the starting motor by heavy-duty lead, provided
the circuit breaker is closed. After the engine has been started
and the key switch released, the spring within the key switch will
open switch 24c, de-energizing the starting relay. Further, it
should be appreciated that when the key switch is rotated to the
start position, internal contact 24b remains closed.
Also, when the circuit breaker is closed and the vapor detector
circuit switch 12 is in the "on" position 12c, the main electrical
bus of the watercraft will be energized by a lead 41 connected to
the circuit breaker which is directly coupled to the main
electrical bus through the circuit breaker as illustrated in FIG.
2.
However, if any accumulation of combustible fumes are present or
subsequently accumulate in the monitored compartment at a level
which is dangerous, the needle pointer will contact sector 18 of
the meter relay 11 and connect battery power to the circuit breaker
25 via lead 28. Conventionally, the circuit breaker will be a
multiple contact, normally closed relay, and when battery power is
connected to the ungrounded side of its coil 43, the armature (not
shown) will open the contacts, breaking the connection of circuits
connected through the relay. When this occurs, if the engine is not
running, it will be impossible to start the engine, as the starting
relay cannot be actuated due to the open contacts between switch
24c and lead 27. Further, if the engine is running, it will stop,
since the distributor will be conventionally powered by the main
electrical bus which is disconnected from lead 41 when pointer 31
is in the danger range by the circuit breaker relay.
Thus, as a result of the above arrangement and operation, the
instant vapor detector system provides a simple, reliable,
fail-safe vapor detector circuit which is suitable for the
environmental operating conditions of watercraft at a reasonable
cost. Further, the system is easy to maintain and simple to operate
as well, as providing an automatic control against mis-operation of
watercraft by inexperienced personnel.
* * * * *