Boat ignition safety apparatus and method

Information

  • Patent Grant
  • 6670722
  • Patent Number
    6,670,722
  • Date Filed
    Monday, September 10, 2001
    23 years ago
  • Date Issued
    Tuesday, December 30, 2003
    21 years ago
Abstract
A boat ignition safety apparatus and method that prevents a gasoline engine of a boat from being started until the enclosed engine compartment has received proper ventilation for a predetermined period of time to ensure dangerous gasoline fumes have been removed. The invention uses an air pressure sensor to detect fresh air drawn into an engine compartment by a ventilation fan or blower. When this takes place a positive pressure develops within the engine compartment. This positive pressure is detected by the air pressure sensor and indicates that the ventilation fan or blower is operating properly. The present invention makes boating safer by ensuring adequate ventilation of volatile gasoline fumes, thereby preventing accidental explosions that can occur when a boat's engine is started.
Description




TECHNICAL FIELD




BACKGROUND OF THE INVENTION




Boats are generally powered by gasoline engines, which are typically mounted in enclosed compartments in either a boat's hull, or in an area toward its stern. As a result, when the engine is not in operation, volatile fumes from the fuel emanate from the engine and its surrounding components. These fumes quickly accumulate within the enclosed engine compartment reaching a concentration substantial enough to become a hazard for explosion. Furthermore, because of the mechanical and electrical components involved in a combustion engine, it is very likely that electrical charges or sparks may be emitted throughout the surrounding engine compartment. Because of the engine compartment's volatile environment, conditions are highly conducive for the occurrence of an explosion. To prevent these fumes from exploding when the engine is started, the gas fumes must be exhausted from the engine compartment prior to starting the boat's engine. If the enclosed engine compartment is not properly exhausted, the boat could explode thereby endangering the safety of the boat's passengers and others nearby.




Today, all boats that have inboard motors include a fan in the engine compartment for exhausting fuel fumes. Further, current federal regulations and safety operating guidelines suggest using a powered ventilation system for at least four minutes before a boat is started. However, boaters are not likely to be aware of how long to ventilate the engine compartment to properly prevent the concentration of hazardous fuel fumes. In addition, many boaters may unintentionally forget to turn on the ventilation fan, if they are not reminded to do so in some fashion. Finally, other boaters may intentionally avoid activating the exhaust fan if they have the ability to start the engine independently of the exhaust fan.




Therefore, in light of the foregoing deficiencies in the prior art, the applicant's invention is herein presented.




SUMMARY OF THE INVENTION




The present invention is directed to a boat ignition safety apparatus and method, which prevents the engine of a boat from being started until there has been continuous positive air flow within an engine compartment for a predetermined period of time to ensure adequate ventilation of gasoline fumes. Thus, the present invention ensures that volatile fumes do not collect in an engine compartment, which poses the threat of an explosion.




Today, many areas allow both boating and docking in and around shoreline recreation areas where people swim and engage in beach related activities. Furthermore, because of the popularity of beach and water recreation, these areas are often highly populated. Because of the number of boaters and beach goers sharing common water areas, the distance boaters are from these shoreline recreation areas has decreased, thereby increasing the chances of great harm to people located in these areas if a boat were to explode. However, the present invention provides the boater with the appropriate safety measures to avoid such a result.




It is an object of the present invention to prevent a boat engine from starting until continuous, positive air flow has been detected within the engine compartment for a predetermined period of time in order to ensure proper ventilation of fumes from the engine compartment.




A further object of the present invention is to make boating safer by preventing accidental explosions of boats caused when gasoline engines are started prior to adequate ventilation of enclosed engine compartments.




The advantages that the present invention provides in terms of functionality and utility will be further made apparent when the detailed description is read in conjunction with the applicable drawings and claims.











BRIEF DESCRIPTION OF DRAWINGS





FIG. 1

is a block diagram of the general functionality of the boat ignition safety apparatus.





FIG. 2

is a schematic diagram of the boat ignition safety apparatus of the present invention.





FIG. 3

is a perspective view of a boat equipped with the boat ignition safety apparatus of the present invention with the engine compartment shown partially cut-away.





FIG. 4

is a schematic diagram of an alternate embodiment of the boat ignition safety apparatus.





FIG. 5

is a schematic diagram of the embodiment in

FIG. 4

showing internal and external wiring connections for the present invention.





FIG. 6

is a schematic diagram of an alternate embodiment of the boat ignition safety apparatus.





FIG. 7

is a schematic diagram of an alternate embodiment of the boat ignition safety apparatus.





FIG. 8

is a schematic diagram of an alternate embodiment of the boat ignition safety apparatus.





FIG. 9

is a schematic diagram of an alternate embodiment of the boat ignition safety apparatus.





FIG. 10

is an elevational view showing an air pressure sensor used in the boat ignition safety apparatus to detect positive air flow within an engine compartment.





FIG. 11

is an elevational view showing an air pressure sensor coupled to an in-line blower motor in one embodiment of the present invention.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT




In the following detailed description of embodiments of the present invention, reference is made to the accompanying drawings which, in conjunction with this detailed description, illustrate and describe an apparatus for preventing a boater from starting an engine until a ventilation fan has removed volatile fumes from an engine compartment. The invention may also be embodied in many different forms and should not be construed as limited to only the disclosed embodiments. The provided embodiments are included so the disclosure will be thorough, complete and will fully convey the scope of the invention to persons of ordinary skill in the art.





FIG. 1

is a block diagram of the general functionality of the boat ignition safety apparatus


10


. When preparing to start a boat's engine, the first step is for the user to turn on


16


the ventilator. In one preferred embodiment the ventilator comprises an exhaust or ventilation fan


92


(see FIG.


3


). If the user does not turn on


12


the exhaust fan


92


, then the engine will not start


14


. In an alternate embodiment, not only will the engine not start


14


but the exhaust or ventilation fan


92


will be automatically turned on. After the user turns on


16


the exhaust fan


92


(or it is turned on automatically), an air pressure sensor


96


(see

FIG. 3

) monitors


18


the presence of positive air flow in the engine compartment


98


. The air pressure sensor


96


determines whether the exhaust fan


92


is clearing the engine compartment


98


of volatile gasoline fumes.

FIGS. 2

,


4


and


5


show similar air pressure sensors


50


and


126


. Reference numerals


50


,


96


and


126


are used interchangeably to refer to air pressure sensing switches because the present invention uses the switches that are triggered by variations in air pressure. One of ordinary skill in the art would understand that separate air pressure sensors and switches could be used in place of an air pressure sensing switch.




In a preferred embodiment, air pressure sensor


96


is an air pressure sensing switch such as Model RSS-495-11 sold by Cleveland Controls. The air pressure sensing switch is comprised of a housing containing a diaphragm and a snap-acting switch. Barbed sample line connectors on each side of the diaphragm accept flexible tubing. The snap-action switch can be actuated by a positive or negative pressure, or by a pressure differential. The switch includes normally open, normally closed and common connect terminals. The air pressure sensing switch has an adjustable set point range that is set to a predetermined set point for use in the present invention. To adjust the sensitivity of the air pressure sensor


96


, the adjustable set point of the air pressure sensing switch can be altered. In the boat ignition safety apparatus


10


of the present invention, the air pressure sensor, implemented with an air pressure sensing switch, is configured to detect positive pressure within an engine compartment. When fresh air is drawn into an engine compartment by a ventilation fan or blower in order to flush fumes out from the engine compartment, a positive pressure develops within the engine compartment. This positive pressure is detected by the air pressure sensor and indicates that the ventilation fan or blower is operating properly.




Use of an air pressure sensor in the present invention provides a number of advantages over prior art boat ignition safety devices. In particular, prior art boat ignition safety devices were adversely affected by the direction of air flow, the devices orientation and forces applied to the prior art devices due to acceleration and deceleration. Because the present invention includes an air pressure sensing switch it can detect air flow from all directions. Prior art devices use a sail and cam arrangement that will only trigger a separate switch if air flows in one direction to push the sail and cam into the switch.




Another advantage provided by the use of an air pressure sensing switch is that it can be mounted within the boat in almost any orientation, making the boat ignition safety apparatus easily adaptable to different types of boats. Prior art devices, such as that disclosed in U.S. Pat. No. 5,050,520, will only detect air flow if the mechanical sensory device, made up of a sail, cam and switch, are within a horizontally mounted vent tube. If the vent tube where mounted vertically with the intake side of the vent tube upward, the position of the sail changes and triggers the switch. If the intake side of the tube were mounted vertically with the intake side of the tube downward, the position of the sail changes away from the switch and never triggers the switch. The prior art devices requires that the vent tube always be positioned so that air flow works the sail properly. The use of an air pressure sensing switch in the present invention does not depend on a sail, cam and switch arrangement, only the detection of positive air pressure. Therefore the air pressure sensing switch can be mounted in any position, making the device much more convenient to mount and/or retrofit in boats.




A further advantage of the use of an air pressure sensing switch in the present invention is that it is unaffected by forces due to acceleration and deceleration of the boat. Because the prior art devices use a mechanical sensory device, i.e., a sail, cam and switch, they have mass, which a sudden force from acceleration or deceleration could activate due to inertia. For example, if a boat were to slam into a wave or surf down the face of a wave, this motion would cause a change in the position of the sail and thereby detect forces of acceleration rather than air flow. Because the present invention monitors and detects air pressure, the detection method has little mass and forces due to acceleration and deceleration do not affect the results.




Once an adequate flow of air is detected


20


within the engine compartment


98


, verifying that the exhaust or ventilation fan


92


is operating properly, a predetermined time delay begins


22


. During the predetermined time delay, the exhaust fan


92


maintains the flow of fresh air through the engine compartment


98


. During the predetermined time delay, the engine of the boat is disabled and may not be started. Once the predetermined time delay expires, boat ignition safety apparatus


10


again allows the engine of the boat to be started


24


. However, in the event the air pressure sensor


96


(see

FIG. 3

) determines that the air flow is not adequate


26


to remove the gasoline or other fumes from the engine compartment


98


, the user is prevented from starting


28


the engine. Unless the air pressure sensor


50


detects adequate air flow for the duration of the predetermined time delay, the engine will not be allowed to start. For example, if half way through the predetermined time delay the air pressure sensor


50


no longer detects positive air flow in the engine compartment


98


, the predetermined time delay will be reset and start over upon the next detection of positive air flow by air pressure sensor


50


.




Additionally, a user also has the option in an emergency to by-pass the boat ignition safety apparatus


10


by actuating a by-pass safety switch


30


. By activating the by-pass switch


30


, the user can immediately start


32


the engine. This feature of the present invention allows the user to start the engine immediately. This can be advantageous in that it allows the user to avoid a collision with another boat or other source of imminent danger. To provide as much safety as possible to boaters, in an alternate embodiment of the by-pass function the exhaust or ventilation fan


92


is automatically started or remains operating upon actuation of the by-pass switch


30


. This provides for some ventilation in an emergency, which is always preferable to no ventilation. While safety dictates that there be some means for by-passing the boat ignition safety apparatus


10


, having a by-pass safety switch


30


can be an invitation for abuse by impatient boaters.




To help protect boaters from themselves, a further contemplated embodiment of the by-pass safety switch


30


includes a time limitation on its use imposed by the boat ignition safety apparatus


10


. Thus, when the by-pass switch


30


has been engaged the engine would only operate for a predetermined time period sufficient to avoid an emergency. Although not shown, one of ordinary skill in the electronic arts will recognize that the by-pass time limitation function could be implemented using circuitry similar to that used for the delay function shown in FIGS.


2


and


4


-


9


.





FIG. 2

is a schematic diagram of the boat ignition safety apparatus of the present invention. The boat ignition safety apparatus


10


is comprised of an ignition switch


52


that when actuated, applies +12VDC


46


to terminal block


2


(TB


2


)


66


, terminal


7


of latching relay


1


(LR


1


)


58


and to fan off indicator lamp


48


. Instead of an ignition switch, apparatus


10


could include a sensor that detects when a preexisting ignition switch or actuator of a boat is initiated. This sequence of events has the effect of preventing the engine from being started until air flow has been proven to be adequate at air pressure sensor (APSS)


50


. To initiate the boat ignition safety apparatus


10


and start the boat, the user must actuate blower fan switch


44


, which engages the blower motor (BM


1


)


42


. In an alternate embodiment, apparatus


10


detects the actuation of ignition switch


52


and automatically engages blower motor


42


. The blower motor


42


provides positive air flow and a positive air pressure within the engine compartment, which is detected by air pressure sensing switch


50


causing the contacts of the air pressure sensing switch


50


to close and the fan indicator lamp


48


to turn off. When the contacts of air pressure sensing switch


50


close, +12VDC


46


is applied to both terminal block


1


(TB


1


)


64


and terminal A


76


of latching relay


58


. Furthermore, terminals


4


and


7


of latching relay


58


close applying +12VDC


46


to time delay relay


1


(TDR


1


)


60


, common node


70


, normally open terminal


82


and terminal


8


of latching relay


58


, which activates coil


78


. Activating coil


78


has the effect of closing terminals


6


and


9


of latching relay


58


, which activates coil


80


of time delay relay


60


and initiates the preset four (4) minute time delay of the apparatus


10


. The relay logic, or combination of latching relays and time delay relays, is primarily responsible for controlling the functions of the boat ignition safety apparatus


10


. In order to complete the preset four (4) minute timing cycle, air pressure sensing switch


50


must detect positive air flow in the form of positive air pressure for the full timing cycle otherwise the sequence is repeated until positive air flow is detected for the entire timing cycle.




Once the preset four (4) minute timing cycle is completed, time delay relay


60


opens normally closed terminal


72


and closes normally open contact


82


. Next, +12VDC


46


is applied to terminal


74


of ignition switch


52


and illuminates run indicator lamp


56


thereby allowing the boat's engine to be started. Once the engine has been started and is running, the blower fan switch


44


can be turned off allowing the engine to continue normal operation until the ignition switch


52


is turned off. Once the ignition switch


52


is turned off the above sequence must be repeated in order to restart the boat's engine. As a further safety measure, a bypass switch


54


has been provided to give the user the ability to circumvent the boat ignition safety apparatus


10


in the event of an emergency. This allows the user of the boat ignition safety apparatus


10


to immediately start the boat's engine to avoid potential danger—such as a head on collision. Additionally, in the preferred embodiment, when the bypass switch


54


is activated the blower motor


42


is automatically started.





FIG. 3

is a perspective view of a boat


112


equipped with the boat ignition safety apparatus


10


of the present invention with the engine compartment shown partially cut-away. Ordinarily, as a boat


112


is moving through the water, an adequate flow of fresh air is provided through the air inlet duct


110


. However, when a boat is not being operated, volatile gasoline fumes can accumulate over a period of time within the engine's compartment


98


, providing an environment that is conducive for an explosion. The present invention includes a ventilation fan


92


for evacuating contaminated air from the boat's engine compartment


98


. Alternatively, ventilation fan


92


may be located in a remote location while being connected to exhaust ducting


108


in order to provide a ventilating flow of fresh air through the engine compartment


98


.




Current federal regulations and safety guidelines suggest using a powered engine compartment ventilation system for at least four minutes before a boat is initially operated. Consequently, one object of the present invention is to assist in the reduction of boat explosions that result from the ignition of volatile fuel vapors that accumulate in the boat's engine compartment


98


. To achieve this result, the present invention utilizes a number of sensing devices and timing relays. Specifically, apparatus


10


comprises an air pressure sensing switch


96


and timing relays contained in control module


94


to prevent engine ignition until air flow in the boat's engine compartment


98


has been established for a specified period of time.




The sequence of operation of the boat ignition safety apparatus


10


is initiated when the boat's user attempts to actuate the ignition switch


102


. When this occurs, the control module


94


interrupts the ignition circuit and prevents the boat's user from being able to start the engine. The user must then turn on the ventilation fan


92


, which provides positive air flow throughout the engine compartment


98


. In an alternate embodiment, control module


94


automatically turns on ventilation fan


92


upon detection of an attempt to actuate the ignition switch


102


. The ventilation fan


92


dissipates any fuel fumes that may have accumulated in the boat's engine compartment


98


as a result of the boat not having been operated. An air pressure sensing switch


96


monitors the flow of air via an air flow sensing tube


106


to ensure that clean, fresh air is being channeled through the engine compartment


98


by the ventilation fan


92


. Once the air pressure sensing switch


96


determines that fresh air is entering the engine compartment, the electrical contacts of the air pressure sensing switch


96


are activated. The activation of the electrical contacts of air pressure sensing switch


96


initiates a timing circuit located within the control module


94


. This timing circuit restricts the user from being able to start the boat's engine, as well as ensures that the ventilation fan


92


runs for a predefined period of time—four (4) minutes in one preferred embodiment. After a period of four (4) minutes has elapsed, the control module


94


completes the ignition circuit and illuminates the run indicator lamp


100


allowing the boat to resume normal operation. Once the engine has been started, the ventilation fan


92


can be turned off until the ignition switch


102


is again switched off.




To further enhance both boater and bystander safety, the present invention contains, an emergency bypass switch


104


. Emergency bypass switch


104


allows a user to immediately start the engine of the boat, thus avoiding the time required to complete the sequences of the boat ignition safety apparatus


10


. Furthermore, when the emergency bypass switch


104


is activated the ventilation fan


92


is automatically started. This feature provides as much immediate ventilation to the engine compartment


98


as possible in the time allowed by any impending emergency, as some ventilation in an emergency is better than none.





FIG. 4

is a schematic diagram of an alternate embodiment of the boat ignition safety apparatus


10


. When the ignition switch


124


is initially activated, the +12VDC power source (battery)


122


is applied to the common contact C


146


of air pressures sensing switch (APSS)


126


. The ignition switch


124


and the boat's existing starting circuit


144


are then interrupted until the user activates the engine compartment ventilation fan


92


(see FIG.


3


). In an alternate embodiment, apparatus


10


automatically engages the ventilation fan


92


when the ignition switch


124


is initially activated. When the ventilation fan is activated, +12VDC


122


is applied to air pressure sensing switch


126


causing common contact C


146


and normally open contact NO


147


of air pressure sensing switch


126


to close. The closing of common contact C


146


and normally open contact NO


147


results in +12VDC


122


being applied to coil


130


of control relay (CR


1


)


128


. As a result, control relay


128


closes normally open NO contact


148


and applies +12VDC


122


to time delay relay (TDR


2


)


136


and common contact C


150


of time delay relay (TDR


1


)


132


. Time delay relays


132


and


136


initiate the timing cycle, which in a preferred embodiment is approximately four (4) minutes. When the timing cycle is completed, time delay relay


132


closes common contact C


150


and normally open contact NO


152


. Time delay relay


136


closes common contact C


154


and normally open contact NO


156


which applies +12VDC


122


to run light


140


, ignition return path


158


and starting circuit


144


, thereby allowing the engine to resume normal operation. Finally, the run light


140


is contained within the control module


94


(see

FIG. 3

) and the auxiliary light


142


terminals are provided for external connection to the control module


94


.





FIG. 5

is a schematic diagram of an alternate embodiment of the boat ignition safety apparatus


10


, as shown in

FIG. 4

, depicting internal and external wiring connections. When the ignition switch


124


is activated, the +12VDC power source


122


is applied to common contact C


146


of air pressure sensing switch (APSS)


126


. The ignition switch


124


and the starting circuit


144


are then interrupted until the user activates the engine compartment ventilation fan


92


(see FIG.


3


). Once the user initiates the engine compartment ventilation fan


92


, the +12VDC power source


122


is applied to air pressure sensing switch


126


, which causes common contact C


146


and normally open contact


147


in air pressure sensing switch


126


to close resulting in the +12VDC power source


122


being applied to coil


130


in control module (CR


1


)


128


. As a result, the control module


128


closes normally open contacts NO


148


and applies the +12VDC power source


122


to time delay relay (TDR


2


)


136


and common contact C


150


of time delay relay (TDR


1


)


132


. Time delay relays


132


and


136


initiate the timing cycle, which in one preferred embodiment is approximately four (4) minutes. When the timing cycle is completed, time delay relay


132


closes common contact C


150


and normally open contact NO


152


. Time delay relay


136


closes common contact C


154


and normally open contact NO


156


, which applies the +12VDC power source


122


to run light


140


and starting circuit


144


. This in turn allows the boat's engine to resume normal operation. Finally, the run light


140


is contained within the control module


94


(see

FIG. 3

) and the auxiliary light


142


terminals are provided for external connection to the control module


94


.





FIG. 6

refers to an alternate embodiment of the boat ignition safety apparatus. The alternate embodiment is comprised of a timing module


186


, which controls the functions of the boat ignition safety apparatus. Although not show, timing module


186


can be comprised of electromechanical relay logic, solid state and digital switches, or microprocessor or microcontroller circuitry. The use of digitally programmable control devices allows for advanced monitoring of air flow, reprogrammable time delays, and more versatile control of the engine. A person of ordinary skill in electronics would know that there are many ways to implement the control functions of the present invention and would be able to do so based upon the descriptions set forth herein. Therefore, FIG.


6


and several other figures disclose the functions of the present invention in the form of a timing module, which is an electrical or electronic black box for performing the recited functions.




When timing module


186


is actuated it receives +12VDC power


182


via switch


188


, and battery


180


, which causes internal switches


192


and


194


to open, and internal switch


196


to close, disabling the boat's ignition and starter circuits. Internal switch


196


starts the boat's ventilation fan or blower motor BM


1




204


. The blower motor


204


provides air flow in the engine compartment and creates positive air pressure within the engine compartment. When the air pressure sensing switch (APSS)


184


detects the positive air pressure it opens its contacts. The air pressure sensing switch


184


also removes the ground potential from internal connection


206


and starts the timing cycle. The timing cycle will continue for approximately four (4) minutes or some other predetermined time period.




If the boat's operator fails to turn on the manual blower switch SW


2




190


before the timing cycle completes, the blower motor


204


stops, which in turn allows the positive air pressure within the engine compartment to dissipate. The air pressure sensing switch


184


detects the change in air pressure and opens its contacts preventing the boat's engine from starting. The timing cycle must be reset by turning off SW


1




188


or by turning on the manual blower switch SW


2




190


.




When the timing cycle is reset and the blower motor


204


is turned on by the boat's operator, the timing cycle will continue to run for four (4) minutes plus or minus three (3) seconds. When the timing cycle completes and ready lamp


208


is illuminated, the boat's ignition and starter circuits are enabled and the engine may be started. Once the boat's engine is running the blower motor


204


may be turned off and the boat's engine will resume normal operation. Once the boat's engine resumes normal operation, the blower motor


204


may be turned on/off as needed.




Additionally, the boat's operator also has the option in an emergency to by-pass the timing module


186


by activating an emergency by-pass switch (not shown) allowing the boat's engine to be started immediately. This can be advantageous in that it allows the boat operator to avoid a collision or other source of danger.





FIG. 7

is a schematic diagram of an alternate embodiment of the boat ignition safety apparatus of the present invention. The boat ignition safety apparatus is comprised of a timing module


224


, that when actuated, receives +12VDC power


220


supplied via the boat's ignition switch


236


which causes internal switches


230


and


232


to open, and internal switch


234


to close, disabling the boat's ignition and starter circuits


238


. Internal switch


234


starts the boat's blower motor BM


1




242


. The blower motor


242


creates positive air pressure within the engine compartment, which is detected by the air pressure sensing switch (APSS)


222


. As a result the air pressure sensing switch


222


opens its contacts and removes the ground potential from internal connection


244


, thereby starting the four (4) minute timing cycle.




If the boat's operator fails to turn on the manual blower switch


228


before the timing cycle completes, the boat's blower motor


242


stops, which causes the air pressure sensing switch


222


to open its contacts thereby preventing the boat's engine from starting. In addition, the timing cycle must be reset by turning off the boat's ignition switch


236


, or by turning on the manual blower switch


228


.




When the timing cycle is reset and the blower motor


242


is turned on by the boat's operator, the timing cycle will continue to run for approximately four (4) minutes. When the timing cycle completes and ready lamp


246


is illuminated the boat's ignition and starter circuits


238


are enabled and the engine may be started. Once the boat's engine is running the blower motor


242


may be turned off and the boat's engine will resume normal operation. Once the boat's engine resumes normal operation the blower motor


242


may be turned on/off as needed.




Additionally, the boat's operator again has the option in an emergency to by-pass the timing module


224


by activating an emergency by-pass switch (not shown) allowing the boat's engine to be started immediately.




FIG.


8


. is a schematic diagram of an electronic circuit implementing an alternate embodiment of the boat ignition safety apparatus. Power is applied to the circuit through the boat's ignition switch with 12 VDC applied across pins


11


and


12


of the circuit. A 5 VDC regulator (A


3


)


250


produces a regulated +5 volts to the timing and control circuitry. With power applied, a precision timer (A


2


)


252


begins to produce clock pulses and binary counter (A


1


)


254


is reset due to a high logic level at pin


11


. This high logic level is created by the power on reset delay circuit, which is comprised of transistor (Q


3


)


256


and the resistive-capacitive network (C


2


-R


2


)


258


-


260


. If pins


7


and


8


are maintained at ground potential, the reset condition for the disclosed electronic circuit will continue.




While the circuit is reset, pin


3


will remain at a low logic level, which prevents relays K


1


(


262


) and K


2


(


264


) from energizing. In turn, this inhibits ignition and prevents starter motor power. Turning on the boat's ventilation fan and/or blower motor creates positive air pressure within an engine compartment, which air pressure sensing switch (external to circuit shown in

FIG. 8

) detects and forces pins


7


and


8


to a positive potential. If pins


7


and


8


are at a positive potential greater than 2 volts, delay capacitor (C


2


)


258


charges until it reaches approximately 0.7 VDC, and transistor (Q


3


)


256


conducts, which applies a low logic level on the reset input (pin


11


) to counter (A


1


)


254


, allowing counter operation to begin timing.




Counting continues until the instant 16,384 counts are registered and pin


3


of counter (A


1


)


254


goes high. With pin


3


high, transistors (Q


1


)


268


and (Q


2


)


266


will conduct, relays (K


1


)


262


and (K


2


)


264


will activate, thereby enabling the ignition and starter motor power when selected. Contact K


1


C (not shown) provides a latch so that additional clock pulses do not effect the enabled status of the circuit. Relay contacts (K


2


)


270


, (K


1


A)


272


and (K


1


D)


274


close during the enabled status. The nominal time from end of reset to enabled status is approximately 4.1 minutes. Reset may be initiated at any time by grounding pins


7


and


8


for approximately 0.5 seconds or more. Timing will begin when the grounding of pins


7


and


8


is removed.





FIG. 9

is a schematic diagram of an alternate embodiment of the boat ignition safety apparatus for use in boats having multiple engines. When ignition switches


306


,


308


, or the ignition switches for both engines are activated, +12VDC power


300


is supplied to the timing module


302


, which causes internal switches


310


and


312


to open, and internal switch


316


to close, disabling the ignition and starter circuits


318


in the engine compartment


320


. The internal switch


316


remains closed until the boat's operator turns on the boat's manual blower switch SW


3




322


, which starts the boat's ventilation fan or blower motor BM


1




324


. The blower motor


324


creates positive air pressure within the engine compartment sensed by the air pressure sensing switch (APSS)


304


. This causes air pressure sensing switch


304


to open its contacts and remove the ground potential from the internal connection


316


, which starts the timing cycle. The timing cycle will continue for approximately four (4) minutes or some other predetermined time period. If the boat operator turns off the manual blower switch SW


3




322


or the air pressure is interrupted before the timing cycle completes, the air pressures sensing switch


304


will detect the change in air pressure and close its contacts. This in turn will stop the timing cycle and reset the timer to zero. This will continue until the air pressure sensing switch


304


detects that the air pressure has been restored. Until the positive air pressure is restored, the ignition and starter circuit


318


will remain disabled.




When the timing cycle is reset by restoring positive air pressure within the engine compartment, the air pressure sensing switch


304


closes its contacts and restarting the timing cycle for four (4) minutes. When the timing cycle completes, the ignition and starter circuit


318


is enabled, the engines may be started. Once the engines are running, the boat's blower motor


324


may be turned off. This causes the contacts on switch


314


to open thereby removing the ground potential at the internal connection


316


and allowing the engines to resume normal operation. Additionally, the boat's operator again has the option in an emergency to by-pass the timing module


302


by activating an emergency by-pass switch (not shown) allowing the engines to be started immediately.





FIG. 10

is an elevational view illustrating the functionality of the air pressure sensing switch (APSS)


350


. The air pressure sensing switch


350


may be located at any given location within the hull of a boat (see

FIG. 3

,


112


) as long as the air pressure sensing tube


338


is located near the bottom of the engine compartment and above the normal bilge water line. When squirrel cage blower motor


352


is running, air enters through the air inlet


354


and exits through the air outlet


356


, which creates a negative air pressure, within the air pressure sensing tube


338


thus activating the contacts in the air pressure sensing switch (APSS)


350


. In this embodiment, instead of detecting positive air pressure within the engine compartment, the air pressure sensing switch


350


is preconfigured to sense the negative air pressure created at the blower motor


352


.





FIG. 11

is an elevational view illustrating the functionality of the air pressure sensing switch (APSS)


350


when used with an in-line blower motor


352


. The air pressure sensing switch


350


may be located at any given location within the hull of a boat (see

FIG. 3

,


112


) as long as the air pressure sensing tube


354


is located near the bottom of the engine compartment and above the normal bilge water line. When the in-line blower motor


352


is running, air enters through the air inlet


356


and exits through the air outlet


358


, which creates negative air pressure within the air pressure sensing tube


354


thereby causing the air pressure sensing switch


350


to activate its contacts. This embodiment also takes advantage of negative air pressure rather than the earlier embodiments which monitor positive air pressure within the engine compartment.




Other variations are also contemplated within the scope of the present invention. For example, in lieu of relay logic in the form of electro-mechanical and time delay relays as illustrated, solid state and digital switches could be used. Additionally, the present invention may also be designed around microprocessor or microcontroller circuitry. The use of digitally programmable control devices would allow for advanced monitoring of air pressure and air flow, reprogrammable time delays, and more versatile control of the engine. The use of microprocessor technology, in conjunction with standard memory, communication and input/output devices, will also allow the boat ignition safety apparatus to monitor and store statistics related to its operation such as air pressure, air flow, use of the by-pass switch, failures, and other conditions. One of ordinary skill in the art of electronics will understand that a wide variety of data acquisition functions can be implemented using microprocessor technology, including but not limited to data storage, printing of monitored data, and wire/wireless transfer of information.




One or more embodiments of the present invention could also be used in conjunction with other types of machines in which fumes accumulate in enclosed or partially enclosed compartments. For example, the present invention could be used in conjunction with automobiles, aircraft, electrical panels that house gaseous emitting battery supplies, and other uses. The present invention can be adapted for use in any situation in which fumes need to be evacuating from an enclosed environment before further operations within that enclosed environment are undertaken.




Thus, while the form of the apparatus and method herein described constitutes the preferred embodiment of this invention, it is to be understood that the invention is not limited to these precise forms of the disclosed apparatus and methods, and that changes may be made therein without departing from the scope of the invention.



Claims
  • 1. A boat ignition safety apparatus for use with at least one engine housed within an engine compartment comprising:an ignition switch for starting said engine; a controller that detects actuation of said ignition switch; a ventilator for removing fumes from within said engine compartment, wherein said ventilator is operated by said controller; and a monitor for sensing air flow within said engine compartment based upon the air pressure within said engine compartment; wherein said monitor provides the value of said air pressure to said controller; and wherein said controller prevents said engine from starting until said controller determines that sufficient air flow was continually present within said engine compartment for a predetermined period of time.
  • 2. An apparatus as recited in claim 1, wherein said monitor for sensing air flow within said engine compartment is comprised of an air pressure sensing switch.
  • 3. An apparatus as recited in claim 1, wherein said controller automatically activates said ventilator upon actuation of said ignition switch.
  • 4. An apparatus as recited in claim 1, further comprising a by-pass switch that allows said engine to be started immediately.
  • 5. An apparatus as recited in claim 4, wherein actuation of said by-pass switch activates said ventilator.
  • 6. An apparatus as recited in claim 4, wherein said controller allows said engine to be started immediately upon actuation of said by-pass switch and operated for only a predetermined period of time.
  • 7. An apparatus as recited in claim 1, wherein said controller is comprised of circuitry selected from the group consisting of relay logic circuitry, analog circuitry, digital logic circuitry, microprocessor circuitry and microcontroller circuitry.
  • 8. An apparatus as recited in claim 1, wherein said ventilator is comprised of an exhaust fan coupled to said engine compartment.
  • 9. An apparatus as recited in claim 1, wherein said ventilator is comprised of a blower motor coupled to said engine compartment.
  • 10. An apparatus for use with at least one engine housed in a engine compartment, comprising:a controller that detects an attempt to start said at least one engine; a ventilator for removing fumes from within said engine compartment; and a monitor for sensing air flow within said engine compartment created by said ventilator; wherein said monitor senses air flow by determining the air pressure within said engine compartment; wherein said monitor provides information about the air pressure to said controller; and wherein said controller prevents said at least one engine from starting until said controller determines that sufficient air flow was continually present within said engine compartment for a predetermined period of time.
  • 11. An apparatus as recited in claim 10, wherein said monitor for sensing air flow within said engine compartment is comprised of an air pressure sensing switch.
  • 12. An apparatus as recited in claim 10, wherein said controller automatically activates said ventilator upon detection of an attempt to start said at least one engine.
  • 13. An apparatus as recited in claim 10, wherein said controller is comprised of circuitry selected from the group consisting of relay logic circuitry, analog circuitry, digital logic circuitry, microprocessor circuitry, and microcontroller circuitry.
  • 14. An apparatus as recited in claim 10, further comprising a by-pass switch that allows said engine to be started immediately.
  • 15. A boat ignition safety apparatus for use with at least one engine housed in an engine compartment, comprising:means for controlling said boat ignition safety apparatus; means for detecting an attempt to start said at least one engine; means for ventilating fumes from within said engine compartment; means for monitoring air flow within said engine compartment created by said ventilating means; wherein said monitoring means senses air flow by determining the air pressure within said engine compartment and then communicates said air pressure to said controlling means; and wherein said controlling means prevents said at least one engine from starting until said controlling means determines that sufficient air flow was continually present within said engine compartment for a predetermined period of time.
  • 16. An apparatus as recited in claim 15, wherein said controlling means actuates said ventilating means upon detection of an attempt to start said at least one engine.
  • 17. An apparatus as recited in claim 15, further comprising means for bypassing said apparatus thereby allowing said at least one engine to be started immediately.
  • 18. An apparatus as recited in claim 15, wherein said ventilating means is activated by said controlling means whenever said by-pass means is employed.
  • 19. A method of removing fumes from at least one engine housed in an engine compartment, comprising the steps of:detecting an attempt to start said at least one engine; ventilating fumes from within said engine compartment; monitoring air flow within said engine compartment by determining the air pressure within said engine compartment; and preventing said at least one engine from starting until sufficient air flow has been continually present within said engine compartment for a predetermined period of time.
  • 20. A method as recited in claim 19, wherein said fumes are automatically ventilated from within said engine compartment upon detection of an attempt to start said at least one engine.
Parent Case Info

The present invention relates to marine safety equipment, and more particularly to a safety apparatus and method that prevents ignition of a boat's gasoline engine until an engine compartment has received proper ventilation for a predetermined period of time. This application is a C-I-P of U.S. application Ser. No. 09/634,432, filed on Aug. 8, 2000, which claims the benefit of U.S. Provisional Application No. 60/147,797, filed on Aug. 9, 1999. The present invention is also the subject of Disclosure Document No. 455,716 dated Apr. 26, 1999, which was received by the U.S. Patent and Trademark Office on Apr. 30, 1999.

US Referenced Citations (18)
Number Name Date Kind
1285659 Ford Nov 1918 A
3489912 Hoffman Jan 1970 A
3652868 Hunt Mar 1972 A
3948202 Yoshikawa Apr 1976 A
3951091 Doench Apr 1976 A
4037578 Dersch et al. Jul 1977 A
4134112 Kercheval et al. Jan 1979 A
4185605 Largent, Sr. Jan 1980 A
4235181 Stickney Nov 1980 A
4473025 Elliott Sep 1984 A
4944241 Carter Jul 1990 A
4991532 Locke Feb 1991 A
5050520 Ballard Sep 1991 A
5069154 Carter Dec 1991 A
5185568 Mothersbaugh et al. Feb 1993 A
5233226 Hanover et al. Aug 1993 A
5664515 Hattori et al. Sep 1997 A
5787833 Lewis Aug 1998 A
Provisional Applications (1)
Number Date Country
60/147797 Aug 1999 US
Continuation in Parts (1)
Number Date Country
Parent 09/634432 Aug 2000 US
Child 09/950032 US