Airship and vectored propeller drive therefor
View Patent ↗A propulsion unit for an airship comprises a driveshaft, having a gimbal mount to a mounting frame attachable to a fuselage, the gimbal being mounted in the mounting frame and comprising an inner ring and an outer ring having orthogonal rotational axes, the inner ring including a propeller unit having a conical housing pivotable on trunnions with the gimbal and a propeller affixed to a propeller shaft coaxial with the axis of the conical housing. The outer ring includes a toroidal Orientation of the conical housing and propeller shaft is accomplished by actuators, a first actuator controlling the angle of the outer ring relative to the framework and a second actuator controlling the angle of the conical housing relative to the outer ring.
1. A propulsion unit for an airship, comprising:
a gimbal assembly having a mounting frame adapted to be mounted on the airship, the gimbal assembly comprising an inner ring and an outer ring, the inner ring being pivotable on a first pivot axis relative to the outer ring, and the outer ring being pivotable relative to the mounting frame on a second pivot axis at substantially right angles to the first axis;
a driveshaft having an inner section coupled to a prime mover for rotation, and an outer section coaxial with an axis of the gimbal assembly coupled to the inner section by a constant velocity joint at a pivot centre of the gimbal assembly;
a propeller unit mounted to the inner ring on the gimbal, and including a propeller affixed to the second section of the drive shaft;
a first actuator to adjust the orientation of the inner ring relative to the outer ring; and
a second actuator to adjust the orientation of the outer ring relative to the mounting frame;
whereby the axis of rotation of the propeller can be controlled about a position coinciding with the axis of the first section of the driveshaft.
2. A propulsion unit as defined in claim 1 , wherein orientation of the propeller unit is controlled by a first actuator controlling the inclination of the outer ring relative to the gimbal mount and by a second actuator controlling the inclination of the inner ring relative to the outer ring.
3. A propulsion unit as defined in claim 1 , wherein the prime mover is in a fixed position relative to the mounting frame.
4. A propulsion unit as defined in claim 1 , wherein the inner ring is carried on the outer ring by a first pair of trunnions, and the outer ring is carried on the mounting frame by a second pair of trunnions.
5. An airship having an envelope and a propulsion unit, said propulsion unit comprising:
a gimbal assembly having a mounting frame adapted to be mounted on the airship, the gimbal assembly comprising an inner ring and an outer ring, the inner ring being pivotable on a first pivot axis relative to the outer ring, and the outer ring being pivotable relative to the mounting frame on a second pivot axis at substantially right angles to the first axis;
a driveshaft having an inner section coupled to a prime mover for rotation, and an outer section coaxial with an axis of the gimbal assembly coupled to the inner section by a constant velocity joint at a pivot centre of the gimbal assembly;
a propeller unit mounted to the inner ring on the gimbal, and including a propeller affixed to the second section of the drive shaft;
a first actuator to adjust the orientation of the inner ring relative to the outer ring; and
a second actuator to adjust the orientation of the outer ring relative to the mounting frame;
whereby the axis of rotation of the propeller can be controlled about a position coinciding with the axis of the first section of the driveshaft.
6. An airship as defined in claim 5 , wherein the propulsion unit is mounted on the envelope of the airship.
7. An airship as defined in claim 6 , wherein the propulsion unit is removably mounted on the envelope by high-strength hook-and-loop fasteners that are airtightly attached to the fuselage and fastened to the mounting frame members.
8. An airship as defined in claim 6 , wherein the propulsion unit is removably mounted to a framework attached to the envelope.
9. An airship according to claim 5 , wherein a first of said propulsion units is mounted forward on the airship and a second of said propulsion units is mounted aft on the airship.