Multifunction aircraft windscreen wiper control system

• US 5,404,085 A
• Filed: 07/10/1992
• Issued: 04/04/1995
• Est. Priority Date: 07/10/1992
• Status: Expired due to Term

• Current Assignee: Rosemount Incorporated (Emerson Electric Company)
• Original Assignee: Rosemount Aerospace, Inc. (Raytheon Technologies Corporation d/b/a RTX)
• Inventors: Benson, Roger R., Resch, William
• Primary Examiner(s): Shoop, Jr., William M.
• Assistant Examiner(s): Cabeca, John W.
• Application Number:
  US07/910,910
• Time in Patent Office: 998 Days
• Field of Search: 318/443, 318/444, 318/480, 318/483, 318/DIG. 2, 318/466
• US Class Current: 318/443
• CPC Class Codes: B60S 1/08 electrically driven conjoint control of windscreen wiper motor and liquid supply of windscreen washer B60S1/482; conjoint control of windscreen wiper motor and means for cleaning parts o parts other than windscreens or front windows B60S1/56, B60S1/58, B60S1/606
• CPC Class Codes: B60S 1/0807 using electronic control means, e.g. tubes, semiconductors B60S1/0818, B60S1/0896 take precedence
• CPC Class Codes: Y10S 318/02 Windshield wiper controls

Abstract

A wiper control system which includes dual wiper control circuits operating from a single rotary control switch, which is mounted in a cockpit of an aircraft remote from the rest of the wipers and system components which are mounted near an aircraft windscreen in a housing from which a motor converter drive shaft protrudes generally normal to a portion of the airframe surface. The drive shaft is connected to one end of a wiper arm and the second end of the wiper arm is rotatably attached to the wiper blade. The dual wiper control circuits are electrically isolated from each other. The rotary switch includes dual voltage dividers and a single axial rotating member to create an analog voltage output signal representative of the control switch position which is interpreted by a controller circuit. The rotary switch speed selections include a HIGH speed, a LOW speed, an INTERMITTENT delay selection, and also a selection for PARK and OFF. The control circuit provides a digital signal input to a logic circuit which determines the rotary switch position and produces a digital output signal to an amplifier circuit that drives the windscreen wiper motor, which in turn drives the wiper arm at the selected speed. A function decoder and commutation logic device prevents motor overheating and power amplifier overheating.

Claims

1. A multifunction aircraft windscreen wiper control system comprising:

manually operated switch means having a multiple position switch providing at least HIGH, LOW, OFF and PARK positions;

voltage control means responsive to each of said positions for providing an analog input voltage at a different level dependent upon the respective positions;

logic means for providing digital control signals in response to the analog input voltage;

a brushless motor coupled to a shaft for driving an aircraft windshield wiper and responsive to the control signals, said control signals including a run signal for energizing the motor to run and a signal providing a motor brake activation;

means for determining the position of the motor rotor and for providing a motor direction signal as a function of motor position, the means for determining position providing a plurality of groups of output pulses in a pulse train indicative of position;

speed control means for controlling speed of the motor; and

gating means for selectively gating one of the plurality of groups of pulses in the pulse train, the speed control means controlling the speed of the motor based on ungated pulses in the pulse train.

2. The system of claim 1 wherein the switch means comprises a rotating shaft moving a switch arm in a voltage divider resistance network to provide different voltage output to the voltage control means at each of the positions.

3. The system of claim 2 wherein the manually operated switch means include the voltage divider resistance network packaged as a unit and fitted into a switch housing forming part of an existing aircraft windscreen wiper control system.

4. The system of claim 1 and current sensing means to provide an overcurrent signal to the logic means to disable the motor drive when the current exceeds a preselected level.

5. The system of claim 1 and a housing for the motor mounted to the aircraft frame, an amplifier for driving the motor, the amplifier having a metal casing in heat conducting relation to the housing.

6. A windscreen wiper controller for selecting a wiper function comprising:

a wiper function switch, having an input electrical potential and a selectable analog electrical output potential having a level indicative of a desired wiper function the selectable level being variable to indicate the desired one of a plurality of wiper functions;

logic means for receiving the analog electrical output potential and providing a digital output signal indicative of the desired wiper function;

amplifier means for providing a power signal in response to the digital output signal;

wiper driving means for cycling an output shaft in periodic arcuate motion in response to the power signal;

a wiper arm coupled to an end of the output shaft opposite the wiper driving means;

a magnet attached to the output shaft; and

magnetic field sensing means for detecting the presence of the magnetic field associated with the magnet and providing an input to the logic means indicative of the position of the output shaft.

7. The windscreen wiper controller of claim 6 wherein the logic means comprises an array of comparators and a programmable logic device for receiving and converting the analog electrical output potential to the digital output signal.

8. The windscreen wiper controller of claim 6 wherein the wiper function switch is a rotary switch and further comprises:

a rotating member;

a selection arm connected to the rotating member;

a voltage ladder constructed of a plurality of equivalent impedance electrical elements; and

a plurality of electrical contacts that establish electrical communication with the selection arm when the rotating arm is rotated, each electrical contact connected to a selection of the voltage ladder between the impedance electrical elements of the voltage ladder, wherein the electrical signal thus established comprises the analog electrical output potential.

9. The windscreen wiper controller of claim 8 wherein the wiper function comprises:

a LOW wiper speed selection;

an INTERMITTENT wiper selection;

a HIGH wiper speed selection;

a wiper OFF selection wherein brake means for slowing the brushless electric motor is applied; and

a momentary PARK wipers selection, wherein the rotary switch is biased to automatically return to the OFF selection following the PARK selection.

10. The windscreen wiper controller of claim 6 wherein the magnetic field sensing means is a Hall Effect sensor which provides a digital input signal to the logic means.

11. A windscreen wiper controller for selecting a wiper function comprising:

a three-wire rotary selection switch for providing an analog wiper function signal having an analog signal level indicative of a desired wiper function;

a comparator array for converting the analog wiper function signal to a digital wiper function signal based on the analog signal level;

a programmable erasable logic device for receiving the digital wiper function signal and providing a logic signal;

a brushless electric motor responding to the driver signal by generating rotating motion within the motor and

a motor-converter connected to the brushless electric motor for converting the rotating motion of the motor to a periodic arcuate motion output.

12. The windscreen wiper controller of claim 11 wherein the motor-converter arcuate motion output is relayed through an output shaft, the output shaft comprising:

a dipole magnet fixed to a portion of the shaft; and

a Hall Effect sensor attached to the motor-converter proximate the shaft for accurately sensing the location of the dipole magnet.