Portable testing apparatus for airplane engines

• US 5,198,980 A
• Filed: 11/05/1990
• Issued: 03/30/1993
• Est. Priority Date: 11/05/1990
• Status: Expired due to Fees

• Current Assignee: James D. Patrick
• Original Assignee: James D. Patrick
• Inventors: Patrick, James D.
• Primary Examiner(s): Black, Thomas G.
• Application Number:
  US07/609,474
• Time in Patent Office: 876 Days
• Field of Search: 364/424.03, 364/424.04, 364/424.06, 364/431.03, 364/431.02, 364/551.01, 364/557, 364/558, 73/116, 73/117.2
• US Class Current: 701/29
• CPC Class Codes: G01M 15/05 by combined monitoring of two or more different engine parameters

Abstract

A self-powered and self-contained portable testing apparatus for monitoring critical operating parameters of an aircraft reciprocating engine. The portable testing apparatus is typically used for the running-in of aircraft engines after overhaul, before returning the engines to service. The portable testing apparatus includes a plurality of sensors for sensing and generating analog signals corresponding to temperature at various locations inside and outside the engine. A multiposition selector switch electrically connects to each of the sensors. The switch is designed to select one of the analog temperature signals and to transmit the selected signal to a computer having a display. The computer converts the selected signal into a digital temperature signal and indicates the digital signal in corresponding numerical representation on its display. Also included is a tachometer for measuring and displaying the operating speed of the engine. The tachometer has a memory, and can calculate and store in its memory the average operating speed of the engine and the maximum operating speed achieved during the run-in of the engine. A manifold pressure gauge senses and displays intake manifold pressure and an oil pressure gauge senses and displays engine oil pressure. A run time monitor electrically connects to an oil pressure switch which, in turn, connects to the oil pressure circuit. The oil pressure switch closes when the engine is turned on and develops oil pressure. The monitor is supplied with electrical power upon oil pressure switch closure and commences to monitor engine run time.

Claims

1. A portable testing apparatus for monitoring the operating parameters of an aircraft reciprocating engine having cylinders, an intake manifold circuit, magnetos, and oil flowing through an oil pressure circuit and through an oil temperature port, the portable testing apparatus comprising:

a plurality of sensors detachably attached to the cylinders and to the oil temperature port to facilitate deployment of the testing apparatus and for sensing the temperature thereof and for generating analog temperature signals corresponding to the sensed temperature;

a multiposition selector switch connected to each of said sensors, said selector switch being adapted for receiving and selecting one of said analog temperature signals so that indicia of said signals may be displayed singularly for ready analysis by an operator;

a temperature indicating computer connected to said multiposition selector switch, said temperature indicating computer being adapted for converting said analog temperature signals into digital signals and for displaying said digital signals;

a tachometer connected to the magnetos, said tachometer being adapted for measuring an operating speed of the engine;

a manifold pressure gauge in communication with the intake manifold circuit, said manifold pressure gauge being adapted for measuring intake manifold pressure;

an oil pressure gauge in communication with the oil pressure circuit, said oil pressure gauge being adapted for measuring oil pressure;

an oil pressure switch in communication with the oil pressure circuit, said oil pressure switch being adapted to close when the engine develops oil pressure; and

a rechargeable power supply means for providing the portable testing apparatus with a self-contained source of electrical energy so that said portable testing apparatus may monitor operating parameters of the engine.

2. The portable testing apparatus of claim 1 further comprising a pressure line connecting means for connecting said manifold pressure gauge and said oil pressure gauge to the intake manifold and oil pressure circuits, respectively.

3. The portable testing apparatus of claim 2 wherein said pressure line connecting means further comprises:

an intake manifold pressure tap having one output port and two input ports, said two input ports being disposed within the intake manifold circuit;

an intake manifold pressure line provided between said intake manifold pressure gauge and said output port;

an oil pressure tap having one output port and two input ports, the two input ports being disposed within the oil pressure circuit;

an oil pressure splitter having one input and two exit ports, one exit port being connected to said oil pressure switch and one exit port being connected to said oil pressure gauge;

an oil pressure line provided between said input port of said oil pressure splitter and said output port of said oil pressure tap; and

a pressure line umbilical cord being adapted for encasing said intake manifold pressure line and said oil pressure line extending from said portable testing apparatus to the engine thereby protecting said lines from abrasion, puncture and other destructive forces,

whereby said intake manifold pressure gauge and said oil pressure gauge are placed in pressure sensing contact with the intake manifold circuit and the oil pressure circuit.

4. The portable testing apparatus of claim 1 further comprising electrical wiring connecting means for electrically connecting said sensors to said selector switch and for electrically linking said magnetos to said tachometer.

5. The portable testing apparatus of claim 4 wherein said electrical wiring connecting means further comprises:

a plurality of sensor leads, said sensor leads each having a first end with a male connector and a second end connected to one of said sensors;

a plurality of signal wires, said signal wires each having a first end with a female connector and a second end connected to said multiposition selector switch, each female connector detachably connecting to one of said male connectors thereby placing multiposition selector switch into electrical contact with said sensors;

three tachometer wires, said tachometer wires each having two ends, the first wire at one end thereof having a clip and at the other end connecting to a left magneto terminal of said tachometer, the second wire at one end thereof having a clip and at the other end connecting to a right magneto terminal of said tachometer, the third wire at one end thereof having a clip and at the other end connecting to a ground terminal of said tachometer, the clips of the first and second wires being adapted for detachably attaching respectively to left and right magnetos and the clip of the third wire being adapted for detachably attaching to a grounding point of the engine, thereby permitting said tachometer to measure the operating speed of the engine; and

an electrical wiring umbilical cord encasing said signal wires and said tachometer wires extending from said portable testing apparatus to the engine, thereby protecting said signal wires and said tachometer wires from entanglement, abrasion and other destructive forces.

6. The portable testing apparatus of claim 1 further comprising means for monitoring total run time of the engine, said monitoring means being electrically connected to said oil pressure switch so that when said oil pressure switch closes, said monitoring means records engine run time until said oil pressure switch opens.

7. The portable testing apparatus of claim 6 wherein the said means for monitoring total engine run time further comprises an elapsed time meter having a digital display.

8. The portable testing apparatus of claim 1 further comprising an on/off switch for connecting and disconnecting said rechargeable power supply means to and from said portable testing apparatus.

9. The portable testing apparatus of claim 1 wherein said tachometer further includes a battery power supply and removably attaches to said portable testing apparatus, said battery power supply providing said tachometer with a self-contained source of electrical energy so that said tachometer may be used away from and independent of said portable testing apparatus.

10. The portable testing apparatus of claim 1 wherein said rechargeable power supply means further comprises:

a rechargeable power supply for storing electrical energy; and

an adaptor plug having a converter for converting alternating current into direct current storable by said rechargeable power supply.

11. The portable testing apparatus of claim 1 wherein said rechargeable power supply means further comprises:

a rechargeable power supply for storing electrical energy, said rechargeable power supply having a converter for converting alternating current into direct current; and

an adaptor plug for transmitting alternating current to said converter.

12. The portable testing apparatus of claim 1 further comprising electrical wiring encased in a first cable for connecting to said plurality of sensors, and pressure lines encased in a second cable for connecting to said manifold pressure gauge and said oil pressure gauge.

13. A portable testing apparatus for monitoring the operating parameters of an aircraft reciprocating engine having cylinders, an intake manifold pressure circuit, magnetos, and oil flowing through an oil pressure circuit and through an oil temperature port, the portable testing apparatus comprising:

a plurality of sensors detachably attached to the cylinders and to the oil temperature port for sensing the temperature thereof;

a temperature indicating computer connected to said plurality of sensors;

a tachometer connected to the magnetos for measuring an operating speed of the engine; and

pressure sensing means in communication with the intake manifold and oil pressure circuits, the portable testing apparatus enabling operating parameters of the engine to be monitored when the engine is mounted in the aircraft.

14. The portable testing apparatus of claim 13 wherein said pressure sensing means include a manifold pressure gauge in communication with the intake manifold pressure circuit and an oil pressure gauge in communication with the oil pressure circuit.

15. The portable testing apparatus of claim 14 further including a multiposition selector switch connected to said sensors.

16. The portable testing apparatus of claim 15 further including an oil pressure switch in communication with the oil pressure circuit, said oil pressure switch being adapted to close when the engine develops oil pressure.