Aircraft battery charging device

• US 4,926,106 A
• Filed: 08/09/1988
• Issued: 05/15/1990
• Est. Priority Date: 07/22/1986
• Status: Expired due to Term

• Current Assignee: COLE Krueger Investments Incorporated
• Original Assignee: Peter G. Tanis
• Inventors: Tanis, Peter G.
• Primary Examiner(s): HICKEY, ROBERT
• Application Number:
  US07/230,300
• Time in Patent Office: 644 Days
• Field of Search: 219/209, 219/202, 320/35, 320/36, 320/2, 320/39, 361/99
• US Class Current: 320/150
• CPC Class Codes: H02J 7/1438 in combination with power supplies for loads other than batteries
• CPC Class Codes: H05B 1/0227 Applications
• CPC Class Codes: H05B 2203/017 Manufacturing methods or apparatus for heaters
• CPC Class Codes: H05B 2203/035 Electrical circuits used in resistive heating apparatus
• CPC Class Codes: H05B 3/36 heating conductor embedded in insulating material
• CPC Class Codes: H05B 3/58 Heating hoses; Heating collars

Abstract

A battery charging device is operable in conjunction with a battery heater to simultaneously heat and recharge the battery of an aircraft which has been stored under cold weather conditions. A thermostat energizes a power supply when the ambient air temperature drops below a given value. A transformer is connected with a power supply to produce an output voltage and a pair of transistors are connected with the transformer for converting the transformer output voltage to a given charging voltage which is supplied to the battery. A voltage control device including a rheostat and a voltage regulator is connected in a feedback circuit with the first and second transistors to control the transistors to produce a constant charging voltage. Thus as the battery is heated, the charging voltage supplied to the battery recharges the battery to full capacity.

Claims

1. Apparatus for charging an aircraft battery, comprising

(a) a power supply;

(b) transformer means connected with said power supply for producing an output voltage;

(c) transistor means including first and second transistors connected with said transformer means for converting said transformer output voltage to a given charging voltage which is supplied to the battery;

(d) voltage control means connected with said first transistor for controlling said first transistor to produce an amplified output used to control said second transistor for producing a constant charging voltage, said voltage control means comprising a feedback circuit including

(1) means for producing a reference voltage proportional to the output voltage of said second transistor; and

(2) voltage regulator means connected with said reference voltage producing means for controlling said first transistor in accordance with said reference voltage;

(e) a thermostat for sensing when the ambient temperature drops below a given value; and

(f) a relay for connecting the output of said second transistor with the positive terminal of the battery, said relay being operated in response to operation of said thermostat, thereby to supply charging voltage to the battery.

6. Apparatus for charging and heating an aircraft battery, comprising

(a) a power supply;

(b) transformer means connected with said power supply for producing an output voltage;

(c) transistor means including first and second transistors connected with said transformer means for converting said transformer output voltage to a given charging voltage which is supplied to the battery;

(d) voltage control means connected with said first transistor for controlling said first transistor to produce an amplified output used to control said second transistor for producing a constant charging voltage, said voltage control means comprising a feedback circuit including

(1) means for producing a reference voltage proportional to the output voltage of said second transistor; and

(2) voltage regulator means connected with said reference voltage producing means for controlling said first transistor in accordance with said reference voltage;

(e) heater means arranged adjacent the battery for heating the battery;

(f) a thermostat for connecting said heater means with said power supply, said thermostat energizing said heater means when the ambient temperature drops below a given value; and

(g) a relay for connecting the output of said second transistor with the positive terminal of the battery, said relay being operated in response to operation of said thermostat, thereby to supply charging voltage to the battery simultaneously with heating of the battery.

7. Apparatus as defined in claim 6, wherein said reference voltage producing means comprises a rheostat.

9. Apparatus as defined in claim 6, wherein said power supply comprises an AC power supply, and further comprising a full wave rectifier connected with the output of said transformer means for converting AC voltage to DC voltage.

10. Apparatus as defined in claim 9, wherein said transformer means comprises a step-down transformer.

11. Apparatus as defined in claim 10, wherein said voltage regulator means includes voltage reducing means connected with the input thereof, whereby output voltage from said rectifier means is used to power said voltage regulator means.

12. Apparatus as defined in claim 11, and further comprising filter means for filtering variation from said charging voltage.

13. Apparatus as defined in claim 9, wherein said filter means comprises

(1) a first filter capacitor connected between the output of said rectifier means and ground;

(2) a second filter capacitor connected between the input to said integrated circuit and ground; and

(3) a third filter capacitor and a resistor both connected between the output of said second transistor and ground.

14. Apparatus as defined in claim 19, wherein said heater means comprises

(1) a battery heater including an elongate, flat, generally rectangular jacket approximately 0.075" thick wrapped around the battery, having a width less than the height of the battery and a length approximately equal to the circumference of the battery, said jacket having first and second vertical edges having vertically aligned eyelets and lace means interconnecting the eyelets on the first and second edges of the jacket to secure the jacket to the battery;

(2) said jacket comprised of inner and outer layers of silicon rubber impregnated glass fiber fabric and a flexible heating element of nichrome wire grid embedded in a layer of silicon rubber disposed between the inner and outer layers of flexible material, said nichrome wire grid providing a watt density of 0.5 w per square inch of jacket area; and

(3) a heating jacket power lead extending from said heating jacket to said power supply.

2. Apparatus as defined in claim 14, and further comprising a mounting plate fixed to said thermostat, said mounting plate being secured to the side wall of the aircraft.

3. Apparatus as defined in claim 14, and further comprising a silicone rubber sheath encapsulating the thermostat, and means for securing said sheath to the side wall of the aircraft.

4. Apparatus as defined in claim 14, wherein said jacket provides a total wattage of between 0.9 and 2.0 watts per pound of battery.

5. Apparatus as defined in claim 14, wherein said thermostat is mounted proximate the top of the battery to sense ambient temperature immediately proximate the battery.

8. Apparatus as defined in claim 4, and further comprising voltage divider means connected with said rheostat for dividing said second transistor output voltage, whereby said rheostat provides a proper reference voltage.