Water jet propulsion unit

Claim 2

A reverse thrust assembly for a watercraft jet propulsion unit having a steering nozzle disposed at the discharge end of said jet propulsion unit and supported for pivotal movement about a generally vertically extending steering axis for steering of the associated watercraft, a reverse thrust bucket supported for pivotal movement by said steering nozzle between a normal forward drive position and a reverse drive position, an actuating lever pivotally carried by said steering nozzle on opposites thereof, the pivot axis of said actuating lever being parallel to the pivot axis of said reverse thrust bucket and cooperating with said reverse thrust bucket for controlling the movement of said reverse thrust bucket between said positions, flexible cable, means extending along the upper portion of said jet propulsion unit for operating said actuating means from a remote location, and means interconnecting said actuating means and said reverse thrust bucket and operative to provide a self-locking effect in at least one position of the reverse thrust bucket under which water forces on said reverse thrust bucket will hold said reverse thrust bucket in said one position.

Claim 3

A reverse thrust assembly as set forth in claim 1 wherein motion is transmitted from the actuating lever to the reverse thrust bucket through a pin-and-slot connection.

Claim 4

A reverse thrust assembly as set forth in claim 2 wherein the pin-in-slot connection is self-locking in at least one position of the reverse thrust bucket.

Claim 5

A reverse thrust assembly as set forth in claim 3 wherein the self-locking operation is operative in both positions of the reverse thrust bucket.

Claim 6

A reverse thrust assembly as set forth in claim 1 further including linkage means for interconnecting the reverse thrust bucket and the actuating lever.

Claim 7

A reverse thrust assembly as set forth in claim 1 wherein the operative connection provides a self-locking of the reverse thrust bucket in both of its positions so that water forces acting on said reverse thrust bucket will hold said reverse thrust bucket in each of said positions.

Claim 8

A reverse thrust assembly as set forth in claim 1 wherein the operative connection between the actuating means and the reverse thrust bucket comprises pin-and-slot connection.

Claim 9

A reverse thrust assembly as set forth in claim 7 wherein the pin-and-slot connection has an end portion in the one position operative to provide the self-locking.

Claim 10

A reverse thrust assembly for a watercraft jet propulsion unit having a steering nozzle disposed at the discharge end of said jet propulsion unit and supported for pivotal movement about a generally vertically extending steering axis for steering of the associated watercraft, a reverse thrust bucket supported for pivotal movement by said steering nozzle between a normal forward drive position and a reverse drive position, actuating means carried by said steering nozzle and cooperating with said reverse thrust bucket for controlling the movement of said reverse thrust bucket between said positions, means for operating said actuating means, and means including a pin-and-slot connection interconnecting said actuating means and said reverse thrust bucket and operative to provide a self-locking effect in both positions of the reverse thrust bucket under which water forces on said reverse thrust bucket will hold said reverse thrust bucket in said positions, said pin-and-slot connection having two end portions to provide the self-locking in the respective position of the reverse thrust bucket.

Claim 11

A reverse thrust assembly for a watercraft jet propulsion unit having a steering nozzle disposed at the discharge end of said jet propulsion unit and supported for pivotal movement about a generally vertically extending steering axis for steering of the associated watercraft, a reverse thrust bucket supported for pivotal movement by said steering nozzle between a normal forward drive position and a reverse drive position, actuating means carried by said steering nozzle and cooperating with said reverse thrust bucket for controlling the movement of said reverse thrust bucket between said positions, means for operating said actuating means, and means including a pin-and-slot connection interconnecting said actuating means and said reverse thrust bucket and operative to provide a self-locking effect in both positions of the reverse thrust bucket under which water forces on said reverse thrust bucket will hold said reverse thrust bucket in said positions, said pin-and-slot connection having two end portions to provide the self-locking in the respective position of the reverse thrust bucket.

Claim 12

A reverse thrust assembly as set forth in claim 9 wherein the two end portions are straight portions extending generally parallel to each other and intersected by an angularly disposed portion that is effective to cause the movement of the reverse thrust bucket between its positions.

Claim 13

A reverse thrust assembly for a jet propulsion unit having a steering nozzle disposed at the discharge end of said jet propulsion unit and supported for pivotal movement about a generally vertically extending steering axis for steering of the associated watercraft, a reverse thrust bucket supported for pivotal movement by said steering nozzle between a normal forward drive position and a reverse drive position, actuating means carried by said steering nozzle and cooperating with said reverse thrust bucket for controlling the movement of said reverse thrust bucket between said positions, means for operating said actuating means, means interconnecting said actuating means and said reverse thrust bucket and operative to provide a self-locking effect in at least one position of the reverse thrust bucket under which water forces on said reverse thrust bucket will hold said reverse thrust bucket in said one position, and biasing spring means for holding said reverse thrust bucket in said one position.

Claim 14

A reverse thrust assembly for a jet propulsion unit having a steering nozzle disposed at the discharge end of said jet propulsion unit and supported for pivotal movement about a generally vertically extending steering axis for steering of the associated watercraft, a reverse thrust bucket supported for pivotal movement by said steering nozzle between a normal forward drive position and a reverse drive position, actuating means carried by said steering nozzle and cooperating with said reverse thrust bucket for controlling the movement of said reverse thrust bucket between said positions, means for operating said actuating means, means interconnecting said actuating means and said reverse thrust bucket and operative to provide a self-locking effect in at least one position of the reverse thrust bucket under which water forces on said reverse thrust bucket will hold said reverse thrust bucket in said one position, and biasing spring means for holding said reverse thrust bucket in said one position.

Claim 15

A reverse thrust assembly as set forth in claim 11 wherein the biasing spring means comprises a single spring for biasing the reverse thrust bucket in each of its positions.

Claim 16

A reverse thrust assembly for a watercraft jet propulsion unit having a steering nozzle disposed at the discharge end of said jet propulsion unit and supported for pivotal movement about a generally vertically extending steering axis for steering of the associated watercraft, a reverse thrust bucket supported for pivotal movement by said steering nozzle between a normal forward drive position and a reverse drive position, actuating means carried by said steering nozzle and cooperating with said reverse thrust bucket for controlling the movement of said reverse thrust bucket between said positions, means for operating said actuating means, and means including a pin-and-slot connection interconnecting said actuating means and said reverse thrust bucket, said pin-and-slot connection having an end portion operative to provide a self-locking effect in at least one position of the reverse thrust bucket under which water forces on said reverse thrust bucket will hold said reverse thrust bucket in said one position, said end portion of said pin-and-slot connection being a straight section of the pin-and-slot connection intersected by an angularly disposed section that is effective to cause the pivotal movement of said reverse thrust bucket.

Claim 17

A reverse thrust assembly for a watercraft jet propulsion unit having a steering nozzle disposed at the discharge end of said jet propulsion unit and supported for pivotal movement about a generally vertically extending steering axis for steering of the associated watercraft, a reverse thrust bucket supported for pivotal movement by said steering nozzle between a normal forward drive position and a reverse drive position, actuating means carried by said steering nozzle and cooperating with said reverse thrust bucket for controlling the movement of said reverse thrust bucket between said positions, means for operating said actuating means, and means including a pin-and-slot connection interconnecting said actuating means and said reverse thrust bucket, said pin-and-slot connection having an end portion operative to provide a self-locking effect in at least one position of the reverse thrust bucket under which water forces on said reverse thrust bucket will hold said reverse thrust bucket in said one position, said end portion of said pin-and-slot connection being a straight section of the pin-and-slot connection intersected by an angularly disposed section that is effective to cause the pivotal movement of said reverse thrust bucket.