Anchor device for propeller rotator

• US 4,296,898 A
• Filed: 12/21/1978
• Issued: 10/27/1981
• Est. Priority Date: 12/23/1977
• Status: Expired due to Term

• Current Assignee: Ronald S. Watson
• Original Assignee: Ronald S. Watson
• Inventors: Watson, Ronald S.
• Primary Examiner(s): Frankfort, Charles E.
• Application Number:
  US05/974,169
• Time in Patent Office: 1,041 Days
• Field of Search: 244/115, 244/116, 244/53 A, 244/114 R, 188/32, 188/36, 180/14 C
• US Class Current: 244/115
• CPC Class Codes: B64F 1/12 for anchoring aircraft
• CPC Class Codes: B64F 1/34 for starting propulsion plant

Abstract

A device for starting an aircraft engine which is capable of being started by rotating a propeller connected to the crankshaft of the engine. The device comprises an anchor device for fixedly positioning on the landing surface below the propeller; this anchor device can be held in place by a portion of the aircraft itself; in one case, the nose wheel and in another case, a separate extension arrangement. A holding device is provided for connection to the anchor device for holding the propeller and the crankshaft of the engine against rotation in a proper starting position while a rotative device is provided for connection to the anchor device for placing a biasing force on the propeller for rotating it. The anchor device has forwardly extending arms, or members, with an attaching device fixed below the propeller, the holding device and rotative device are each fixed between the propeller and the attaching device. The arms, or members, can be made adjustable to adapt to different width tires and can be foldable lengthwise and in a sidewise overlapping manner to be compact for storing.

Claims

1. An anchor means for placing between a forward portion of a propeller driven aircraft and a landing surface including, a section of said anchor means located behind the plane of a propeller of said aircraft and engaged by said aircraft to hold the anchor means fixedly against said landing surface, a pair of arms extending forwardly from said section held by said aircraft, said arms having forward ends for positioning substantially under a propeller, said forward ends of said arms having holding means for positioning substantially under the center mounting of the propeller adapted to be connected to said propeller.

2. A device as set forth in claim 1 wherein each arm is formed of two sections, means pivotally mounting one section to the other so said arms can be placed in a more compact manner for storing.

3. A device as set forth in claim 1 wherein each arm has a side, said sides being formed so that they can be positioned against the tire of a nose wheel on said aircraft with a portion under said tire.

4. A device as set forth in claim 1 wherein said pair of arms are pivotally mounted to each other at a point intermediate their ends, said arms having two upper adjacent ends connected by a strap means, said strap means being adapted to be positioned beneath the forward portion of said aircraft with said forward ends of said arms being positioned on said landing surface forwardly thereof, means connecting the forward ends of said arms to a lower portion of said aircraft for holding said arms in place.

5. A device as set forth in claim 4 wherein said means connecting the forward ends of said arms to a lower portion of said aircraft for holding said arms in place comprises an adjustable strap for positioning between said holding means of said arms and landing gear of said aircraft.

6. A device as set forth in claim 1 wherein said pair of arms extend forwardly in a side-by-side relationship.

7. A device as set forth in claim 1 wherein said holding means includes a metal loop on each forward end of each arm, said metal loops being located adjacent each other, each metal loop being adapted to be connected to said propeller.

8. A device as set forth in claim 7 wherein said propeller has two blades, one metal loop being adapted to be connected to one blade, the other metal loop being adapted to be connected to the other blade.

9. An anchor means for fixedly positioning on a landing surface below an aircraft having a propeller including, plate means for positioning between said landing surface and a tire of said aircraft to fixedly hold said plate means in place with said plate means contacting said landing surface and said tire, said tire holding said plate means in place on said landing surface by contact, said plate means being located behind the plane of said propeller, an extension means extending from said plate means to a position substantially under said propeller of said aircraft, holding means on said extension means adapted to fixedly hold means attached to said propeller for rotating said propeller.

10. A device as set forth in claim 9 wherein said extension means comprises two forwardly extending members, each member being adapted to be positioned against the side of said tire, said extension members being movable to accept different width tires.

11. A device as set forth in claim 10 wherein said members are pivoted along their length so the members can be folded and placed in a more compact manner for storing.

12. A device as set forth in claim 11 wherein said plate means comprises a short plate connected to each member, means on the rearward ends of said members to hold them together on each side of said tire, means connecting the forward ends of said members together.

13. A device as set forth in claim 12 wherein said means connecting the forward ends of said members is a pivotal connection so the members can be brought closer together in a more compact manner for storing.

14. A device as set forth in claim 9 wherein said aircraft has a nose wheel, said tire being on said nose wheel, and said extension means including arm means extending forwardly from said plate means to a position substantially under said propeller, said holding means including loop means on the end of said arm means for positioning substantially under the center mounting of the propeller.