Digital gas sensing system

• US 4,555,930 A
• Filed: 02/14/1984
• Issued: 12/03/1985
• Est. Priority Date: 02/14/1984
• Status: Expired due to Fees

• Current Assignee: Instruments & Controls, Inc.
• Original Assignee: Instruments & Controls, Inc.
• Inventors: Schaeffer, James, Leach, Thomas W.
• Primary Examiner(s): Kreitman, Stephen A.
• Application Number:
  US06/580,028
• Time in Patent Office: 658 Days
• Field of Search: 73/23, 73/27 R, 73/1 G, 340/534, 340/538, 340/632, 340/633, 340/634, 364/497, 364/498, 364/499, 422/94, 422/98, 204/406, 204/401
• US Class Current: 73/23.2
• CPC Class Codes: G01N 27/122 Circuits particularly adapted therefor, e.g. linearising circuits
• CPC Class Codes: G01N 33/0062 concerning the measuring method or the display, e.g. intermittent measurement or digital display
• CPC Class Codes: H04Q 9/14 Calling by using pulses

Abstract

A digital gas sensing system comprises a plurality of satellite subassembly units each including a central processing unit (CPU) and a plurality of "intelligent" sensors connected to the satellite subassembly units by a single pair of leads. The satellite subassembly units communicate to the sensors in a code having a predetermined number of digital bits. Each sensor has internal "intelligence" and recognizes its own unique address and responds to the satellite subassembly unit in a predetermined code that varies from the satellite subassembly unit code by one parity bit. This arrangement makes it possible for other sensors to distinguish between transmissions from the satellite subassembly unit and transmissions from other sensors. The net result is that the system is able to operate very reliably using only two leads to connect all of the sensors to the satellite sub subassembly unit thereby greatly reducing the wiring and installation costs of the system. To further expand the potential of the system it is also possible to link a plurality of satellite subassembly units together to a single master control unit.

Claims

1. A gas sensing system comprising:

a satellite means including a central processing unit (CPU) means for controlling said system and for transmitting information in a digital code having a predetermined number of bits;

a single pair of information leads;

sensor means attached to said satellite means by said single pair of information leads;

a source of zero calibration gas;

a source of span gas;

valve means for applying said zero calibration gas and said span gas to said sensor means;

a master controller means for controlling a plurality of satellite means;

a parity determining means within said sensor means for generating a digital word in response to interrogation from said satellite means which differs by one parity bit from the digital word generated by said satellite means so that said satellite means can recognize that it is getting a response from the addressed sensor means and so that the non-addressed sensor means recognizes that the digital word is not coming from said satellite means;

a sensor universal receiver/transmitter means (UART) for sending and receiving signals to and from said satellite means and for generating a parity error bit signal and a data ready bit signal;

an address selection means for generating a digital address for a given sensor means different from the digital address of other sensor means associated with a given satellite means;

comparator means for comparing the address of an incoming digital signal with the address selected by the address selection means and for producing an output if the address of the incoming digital signal is the same as the address selected by the address selection means; and

,

gate means for producing an output in response to an input from said comparator means and the presence of a parity error bit signal and a data ready bit signal from said sensor UART,

wherein said satellite means communicates to said sensor means and said sensor means communicates with said satellite means exclusively on said single pair of information leads and wherein the application of said zero calibration gas sets a zero point for said sensor means and application of said span gas sets an intermediate range point for said sensor means whereby said CPU takes both said zero point and said intermediate range point and extrapolates the actual value of subsequent gas measurements from said two points.

2. The system of claim 1 wherein said sensor means further comprises:

sensor elements whose electrical characteristics respond to gas in the environment;

analog to digital conversion means for converting electrical signals from analog signals to digital signals; and

,

logic means for converting said digital signal into two 8 bit digital words for transmission through said sensor UART back to said satellite means.

3. The system of claim 2 further comprising:

a zero adjustment means for setting said sensor elements to a zero value.

4. The system of claim 3 wherein said satellite means comprises:

a satellite UART for communicating to and from said sensor means;

address decoding and control logic means being connected to said satellite UART;

microprocessor means connected to said address decoding and control logic means;

active RAM storage means connected to said address decoding and control logic means; and

,

programmable read only memory means (PROM) connected to said sensor UART and to said address decoding and control logic means.

5. The system of claim 4 further including:

time out means for indicating a malfunctioning sensor means,

wherein said time out means will indicate a sensor malfunction if a given sensor does not respond to its address from said satellite means within a given predetermined period of time.

6. The system of claim 5 further including:

a power failure memory check means including a timing element for saving memory in case of a power failure,

wherein said check means adds up all of the memory in RAM upon the identification of a power failure and compares the pre failure number with the post failure RAM memory to determine if memory has been lost during the power failure interval.

7. The system of claim 6 wherein said timing element is a monostable multivibrator.

8. The system of claim 7 wherein said valve means comprise solenoid valves and a plurality of sensor means are fed zero and span gas by no more than two solenoid valves respectively.

9. A gas sensing system comprising:

a satellite means including a central processing unit (CPU) means for controlling said system and for transmitting information in a digital code having a predetermined number of bits;

a single pair of information leads;

sensor means for sensing a gas attached to said satellite means by said single pair of information leads;

a source of zero calibration gas;

a source of span gas;

valve means for applying said zero calibration gas and said span gas to said sensor means;

a master controller means for controlling a plurality of satellite means; and

,

a parity determining means within said sensor means for generating a digital word in response to interrogation from said satellite means which differs by one parity bit from the digital word generated by said satellite means so that said satellite means can recognize that it is getting a response from the addressed sensor means and so that the non-addressed sensor means recognizes that the digital word is not coming from said satellite means,

wherein said satellite means communicates to said sensor means and said sensor means communicates with said satellite means exclusively on said single pair of information leads and further wherein application of said zero calibration gas sets a zero point for said sensor means and application of said span gas sets an intermediate range point for said sensor means whereby said CPU takes both said zero point and said intermediate range point and extrapolates the actual value of subsequent gas measurements from said two points.

10. A gas sensing system comprising:

a satellite means including a central processing unit (CPU) means for controlling said system and for transmitting information in a digital code having a predetermined number of bits;

a single pair of information leads;

sensor means for sensing a gas attached to said satellite means by said single pair of information leads; and

,

a parity determining means within said sensor means for generating a digital word in response to interrogation from said satellite means which differs by one parity bit from the digital word generated by said satellite means so that said satellite means can recognize that it is getting a response from the addressed sensor means and so that the non-addressed sensor means recognizes that the digital word is not coming from said satellite means, wherein said satellite means communicates to said sensor means and said sensor means communicates with said satellite means exclusively on said single pair of information leads.

11. The system of claim 10 further comprising:

a master controller means for controlling a plurality of satellite means.