Electric powered flying model airplane

• US 4,067,139 A
• Filed: 07/16/1976
• Issued: 01/10/1978
• Est. Priority Date: 07/16/1976
• Status: Expired due to Term

• Current Assignee: S-H Hobbies Incorporated
• Original Assignee: L M Cox Manufacturing Company Incorporated
• Inventors: Malewicki, Douglas J., Pinkerton, Kenneth R.
• Primary Examiner(s): Mancene, Louis G.
• Assistant Examiner(s): Cutting, Robert F.
• Application Number:
  US05/705,979
• Time in Patent Office: 543 Days
• Field of Search: 46/77, 46/249
• US Class Current: 446/31
• CPC Class Codes: A63H 27/04 Captive toy aircraft

Abstract

An electrically powered scale model airplane is disclosed in which a rechargeable electric storage battery is positioned within the aircraft fuselage to balance the weight of a nose mounted direct drive motor. A switch for energizing the motor driving the propeller is arranged to be adjusted from an "off" position to an "on" position by remotely operated control cables acting through a bellcrank assembly used to change the orientation of the aircraft elevator during flight, thus allowing the aircraft to be operated by a single individual. The switch may be manually operated to an "off" position from the outside of the aircraft fuselage in preparation for recharging of the battery. In addition, the entire connecting means between the storage batteries, the recharging battery switch assembly, and the propeller motor are made by only three rigid wires within the aircraft fuselage, two of these wires providing switch contacts for energizing the motor, thus greatly reducing the overall cost of assembling this device.

Claims

1. An electric powered model airplane comprising:

an electric motor mounted in the nose of said airplane, said motor including a short armature shaft extending through the nose of said airplane and supporting a driving propeller, said motor further including a pair of spring biased friction electrical contacts;

a rechargeable battery located in the fuselage of said airplane aft of the wings thereof;

a pair of nonconductive surfaces formed within the fuselage of said airplane adjacent to a pair of electrical terminals of said rechargeable battery;

a first semi-rigid conductor engaged at one end with one of said electrical contacts of said motor, extending from said one end to a position between one of said nonconductive surfaces and one of said pair of electrical battery terminals for contacting said one of said pair of battery terminals, and extending from said one of said battery terminals to a position outside the fuselage of said airplane for contact with a recharging source;

a second semi-rigid conductor engaged at one end with the other of said electrical contacts of said motor, and extending from said one end to form a resilient switch contact; and

a third semi-rigid conductor having a first end positioned adjacent said resilient switch contact, extending from said first end to a position outside the fuselage of said airplane for contact with said recharging source, and extending from said position outside the fuselage to a second end positioned between the other of said pair of nonconductive surfaces and the other of said pair of electrical battery terminals for contacting said other of said pair of battery terminals.

2. An electric powered model airplane as defined in claim 1 wherein the fuselage of said airplane comprises:

a pair of adjacent indentations;

and wherein the portion of said first and third semi-rigid conductors extending outside the fuselage of said airplane each extend across one of said indentations for providing contact with a recharging source.

3. An electric powered model airplane as defined in claim 1 wherein said fuselage indentations have different depths to prohibit reverse polarization of said recharging source.

4. An electric powered model airplane as defined in claim 1 wherein that portion of said first and third semi-rigid conductors positioned to contact the terminals of said rechargeable battery are each bent to form a spring contact resiliently biased between one of said pair of battery terminals and one of said pair of nonconductive surfaces, said resilience assuring electrical contact between said conductors and said rechargeable battery and holding said battery in place within the fuselage of said model airplane.

5. An electric powered model airplane as defined in claim 1 wherein each of said first, second and third semi-rigid conductors is supported within the fuselage of said model airplane at spaced locations and is sufficiently rigid to be self-supporting between said spaced locations.

6. An electric powered model airplane comprising:

a motor mounted in said airplane for driving a propeller;

a rechargeable battery mounted in said airplane for energizing said motor, said battery having a negative and a positive terminal;

a removable source for recharging said rechargeable battery from outside said airplane, said removable source being an electric battery having a permanent negative and a positive terminal; and

first, second and third conductive rods mounted in said airplane forming the sole electrical interconnection between said motor, said rechargeable battery and said removable recharging source, said first and said second conductive rods having adjacent ends forming contacts for a switch to selectively connect said motor to said rechargeable battery, said second conductive rod directly contacting both the positive terminal of said rechargeable battery and the positive terminal of said removable recharging source, and said third conductive rod directly contacting both the negative terminal of said rechargeable battery and the negative terminal of said removable recharging source.

7. An electric powered model airplane as defined in claim 6 wherein two of said three conductive rods which electrically interconnect rechargeable battery are bent to form resilient spring contacts for the terminals of said battery, said spring contacts partially supporting said rechargeable battery.

8. An electric powered model airplane as defined in claim 6 wherein one of said two adjacent conductive rod ends forming switch contacts is resilient to bias said switch to a closed circuit configuration.

9. An electric powered model airplane as defined in claim 6 wherein each of said three conductive rods is connected at spaced locations to said model airplane, said conductive rods being sufficiently rigid to be self-supporting between said spaced locations.

10. An electric powered model airplane as defined in claim 6 wherein said motor is mounted in the nose of said airplane and wherein said rechargeable battery is mounted within said airplane aft of the wings of said airplane to counterbalance the weight of said nose mounted motor.

11. An electric powered model airplane comprising:

a pair of control lines for controlling the flight of said airplane from a remote location;

a bellcrank mounted within said airplane, attached to said pair of control lines and connected to adjust the position of an elevator of said airplane;

a battery mounted within said airplane;

an electric motor mounted within said airplane for driving the propeller thereof, said motor energized by said battery;

a switch mounted within said airplane electrically connected to said electric motor and said battery to selectively interconnect the motor to the battery, said switch comprising;

a stationary contact; and

a resilient, movable contact, said resilient contact biased toward a closed circuit configuration; and

a switch actuator extending from a position adjacent said bellcrank to a position outside said airplane, said actuator having a first position maintained by the bias of said resilient, movable contact for opening said switch and a second position for closing said switch, said switch actuator positioned to be moved by said bellcrank from said first to said second position but not from said second to said first position.

12. An electric powered model airplane as defined in claim 11 wherein said switch actuator, when in said first position, is removed from the normal path of movement of said bellcrank.

13. An electric powered model airplane as defined in claim 11 wherein said battery is mounted aft of the wings of said airplane and wherein said electric motor is mounted in the nose of said airplane, the armature shaft of said motor supporting the propeller of said airplane.

14. An electric powered model airplane as defined in claim 11 wherein said switch actuator is additionally maintained by the bias of said resilient movable contact in said second position.

15. In an electric powered model airplane having a rotatable bellcrank for remote controlled flight and a resilient contact switch for interconnecting an internally mounted battery to an electric motor, the improvement comprising:

a switch actuator movably mounted on said airplane between a first position opening said switch and a second position closing said switch, said actuator extending outside said airplane to permit manipulation thereof, said actuator held in both said first and second positions by the resilience of said resilient spring contact; and

means on said bellcrank for overcoming the resilience of said spring to move said actuator from said first to second position.

16. An electric powered model airplane as defined in claim 15 wherein said means on said bellcrank comprises a surface for contacting and moving said switch actuator, said surface of said bellcrank having a normal path of movement during controlled flight of said aircraft, said switch actuator in said second position being out of the normal path of movement of said bellcrank surface.

17. An electric powered model airplane as defined in claim 15 wherein said means on said bellcrank for overcoming the resilience of said spring is incapable of moving said actuator from said second position to said first position.

18. A rechargeable electric powered model airplane, comprising:

a pair of fuselage indentations adjacent one another;

a pair of electrical conductors, one positioned in each of said indentations;

a rechargeable battery mounted within said airplane and connected to said pair of electrical conductors;

a recharging battery including terminals for extending into said pair of indentations, said terminals mounted unsymmetrically on said recharging battery; and

means on said airplane removed from said indentations for prohibiting reverse polarity contact of said recharging battery terminals with said electrical conductors.

19. A rechargeable electric powered model airplane as defined in claim 18 wherein said prohibiting means comprises a surface extension on said model airplane.

20. A rechargeable electric powered model airplane as defined in claim 19 wherein said surface extension comprises a wheel of said airplane.

21. A rechargeable electric powered model airplane as defined in claim 18 wherein said terminals of said recharging battery comprise spring contact members for resiliently contacting said pair of electrical conductors.

22. A rechargeable electric powered model airplane conprising:

a rechargeable battery mounted within said airplane and connected to drive said airplane;

a pair of electrical conductors attached to said rechargeable battery and extending outside the fuselage of said model airplane at spaced locations;

a recharging battery removable from said airplane, said recharging battery including a pair of terminals in the form of resilient springs, said terminals being separated by a distance equal to the separation of said spaced locations to permit said recharging battery to be held against said pair of electrical conductors for recharging said rechargeable battery, said terminals mounted unsymmetrically on said recharging battery; and

means positioned on said airplane for contacting said recharging battery and thereby prohibiting reverse polarity contact of said recharging battery terminals with said electrical conductors when said pair of resilient spring terminals are placed on said pair of conductors in a reverse orientation, said means clearing said battery when said pair of resilient spring terminals are placed on said pair of conductors in a proper orientation.

23. A rechargeable electric powered model airplane as defined in claim 22 wherein said recharging battery terminals are mounted on a face of said recharging battery, one of said recharging battery terminals centrally mounted on said face and the remaining terminal mounted at one edge of said face, the opposite edge of said face contacting said surface irregularity means for prohibiting reverse polarization connection.