Method and apparatus for sensing, storing, and graphically displaying over-temperature conditions of jet engines

• US 3,946,364 A
• Filed: 01/08/1975
• Issued: 03/23/1976
• Est. Priority Date: 01/08/1975
• Status: Expired due to Term

• Current Assignee: Eldec Corporation (Crane Company)
• Original Assignee: Eldec Corporation (Crane Company)
• Inventors: Thorson, Eric K., Codomo, Joseph
• Primary Examiner(s): Zache, Raulfe B.
• Application Number:
  US05/539,393
• Time in Patent Office: 440 Days
• Field of Search: 340/172.5, 73/340, 73/342, 73/343.5
• US Class Current: 701/3
• CPC Class Codes: G01K 1/02 Means for indicating or recording specially adapted for thermometers
• CPC Class Codes: G01R 13/408 Two or three dimensional representation of measured values

Abstract

The required frequency of inspection, servicing and overhauling of jet engines is to a large extent determined by the history of excessive or over-temperature conditions of each engine. In order to monitor and record each such over-temperature condition, an indicator device is provided having electronic circuitry for processing a temperature signal from the jet engine and a light emitting diode matrix for graphically displaying each over-temperature incident. When the jet engine temperature exceeds a threshold over-temperature point, this occurrence is sensed and the circuitry of the indicator functions to automatically store and visually display the engine temperature as a function of time for the succeeding several seconds after the over-temperature condition has commenced. All the diodes of the matrix lying under the temperature versus time profile are energized so as to present a histogram display of the severity of the condition, where the severity is a function of the duration and magnitude of the over-temperature. In one embodiment disclosed herein, a plurality of over-temperature events are automatically sensed, graphically displayed and stored for later retrieval, such that the maintenance crew may subsequently interrogate the indicator device causing it to sequentially display each recorded or electronically stored over-temperature event.

Claims

1. Apparatus for receiving an electrical signal representing a temperature condition of a jet engine and sensing, storing, and displaying an over-temperature event incurred by such engine, comprising:

an analog to digital converter means adapted to receive said electrical temperature signal and convert it to a digital temperature signal;

over-temperature sensing means responsive to said temperature signal and having an electrical output indicating that said engine has commenced an over-temperature event;

digital storage means;

electrically energized, light emitting, solid state matrix display means; and

time base generator means connected and responsive to said electrical output of said over-temperature sensing means and connected to and for conditioning said storage means to store said temperature signal at each of a plurality of time intervals in response to said over-temperature sensing means indicating the commencement of said over-temperature event, and said display means connected to said storage means and to said time base generator means for graphically displaying said stored temperature signals as a function of time.

2. The apparatus as defined in claim 1, wherein said display means comprises:

a light emitting diode matrix including a plurality of rows and columns of diodes being selectively energized by said storage means and said time base generator means to graphically represent said temperature signals as a function of time, and said digital storage means including means for energizing all said diodes representing a temperature signal equal to and less than said stored temperature signal for each said time interval, whereby said diode matrix presents a histogram graph of said over-temperaature as a function of time.

3. The apparatus of claim 1, wherein said analog to digital converter means includes parallel multiple bit outputs;

and said digital storage means includes a plurality of parallel recirculating shift register stages, one for each said bit output; and

said time base generator means includes a clock generator connected to and for continuously clocking said plurality of shift register stages with a succession of clock pulses, whereby said digital temperature signal is fed as a multiple bit digital signal to and for storage in said plurality of shift register stages.

4. The apparatus of claim 3, wherein said display means comprises a plurality of light emitting diodes arranged in multiple rows and columns defining temperature and time axes of a matrix;

said diodes being connected for selective electrical energization along said temperature axis by said shift register stages; and

an electrical driver having an input connected to said time base generator means and having a plurality of outputs connected to and for selective electrical energization of said diodes along said time axis at said time intervals.

5. The apparatus of claim 3, said digital storage means further including data entry control gate means connected between said converter means outputs and said shift register stages;

and said time base generator means further including a time base counter circuit means connected to said clock generator and to said data entry control gate means for conditioning said gate means to enter said digital temperature signal from said converter means into said shift register stages upon counting a predetermined number of said clock pulses plus one additional said clock pulse;

whereby said time base counter circuit means serves to shift said register stages by said predetermined number plus one state each time a new digital temperature signal is stored in said recirculating shift register stages to provide a unique storage location in said digital storage means for a succession of said digital temperature signals.

6. The apparatus of claim 1, further comprising:

power loss sensing circuit means adapted to be connected to a source of electrical power for said apparatus; and

memory battery circuit means including an emergency battery said memory circuit means connected and responsive to said power loss sensing circuit means for connecting said emergency battery to at least said digital storage means for sustaining operation thereof after loss of said source of power for retaining all temperature signal data stored therein.

7. The apparatus as defined in claim 1, wherein said digital storage means and said time base generator means include additional means for registering each of a plurality of N over-temperature events and storing the temperature signals as a function of time in said digital storage means for each such over-temperature event.

8. The apparatus as defined in claim 1, wherein said digital storage means includes means for storing digital temperature signals at each said time interval for a plurality of successive N over-temperature events and means for counting each such N event;

and said time base generator means further including event multiplexer means responsive to said means for counting each said N event for conditioning said digital storage means to store each said digital temperature signal at each of said plurality of time intervals for each said plurality of events N, whereby a plurality of over-temperature events are successively graphically displayed on said solid state matrix display means and recorded in said digital storage means.

9. The apparatus as set forth in claim 8, further comprising:

event display means connected and responsive to said means for counting said events for displaying a symbol uniquely representing each said plurality of N events.

10. An instrument adapted to be mounted on the instrument panel of a jet engine aircraft for receiving an electrical signal representing a temperature condition of one or more of the aircraft jet engines and, in response thereto, sensing, storing, and displaying an over-temperature event incurred by such jet engine, comprising:

means for receiving said electrical signal and for sensing an over-temperature represented thereby indicating that said engine has commenced an over-temperature event;

means for digitally storing the condition of said electrical signal at each of a plurality of time intervals subsequent to said means sensing said over-temperature conditon; and

solid state matrix display means connected to said means for digitally storing said electrical signal for graphically displaying the temperature of said jet engine as represented by said electrical signal as a function of time represented by said time intervals.

11. Method for sensing, storing, and displaying an over-temperature event incurred by an aircraft jet engine, comprising the steps of:

sensing an over-temperature condition of said jet engine by detecting a threshold level of an electrical signal representing the engine temperature;

storing said jet engine temperature as a digital signal at each of a plurality of time intervals following said step of sensing said over-temperature condition; and

graphically displaying said engine temperature as a function of said time intervals on a light emitting diode matrix display by selectively energizing the diodes of said display in accordance with the digitally stored temperature signal at each of said plurality of time intervals.

12. The method as set forth in claim 11, wherein said step of graphically displaying said engine temperature is further defined by selectively energizing all those diodes lying within a jet engine temperature versus time profile, so as to present a temperature versus time histogram display of said jet engine over-temperature event.

13. The method set forth in claim 11, further comprising the steps of:

detecting a plurality of successive, N over-temperature events of said jet engine and visually displaying a unique symbol for each such over-temperature event; and

said step of digitally storing said jet engine temperature including the substep of digitally storing said jet engine temperature at each of a plurality of time intervals for each one of said plurality of events N; and

said step of graphically displaying said over-temperature event including the substep of graphically displaying the over-temperature as a function of time for each one of said plurality of N over-temperature events in succession on said light emitting diode matrix display.