| Marine 1, LLC Patent applications |
| Patent application number | Title | Published |
|---|
| 20100221964 | ADJUSTABLE PROPELLER - An adjustable propeller assembly that includes a propeller housing and a drive shaft. A propeller shaft is linked with a propeller. The propeller is linked with a pivotal housing. A coupling member is connected to the drive shaft and propeller shaft. The coupling member pivotally transmits a torque from the drive shaft to the propeller shaft. An actuator is connected to the pivotal housing. The actuator moves the pivotal housing and propeller wherein a thrust vector of the propeller is adjusted relative to the propeller housing | 09-02-2010 |
| 20100054641 | ACTUATOR MOUNT ASSEMBLY - An actuator mounting assembly includes an actuator and a bearing removably attached to the actuator. A bearing plate includes a hole formed therein for receiving the bearing. A bearing mounting plate includes a hole formed therein for receiving the bearing. First and second bearing inserts are removably disposed about the holes formed in the bearing plate and bearing mounting plate. The bearing mounting plate and bearing plate are coupled to retain the bearing and bearing inserts therebetween firming a seal wherein the actuator is angularly movable about the bearing. | 03-04-2010 |
| 20100043691 | TRIM TAB - A trim tab assembly for a watercraft includes a enclosure. A support structure is positioned in the enclosure. At least one trim tab is disposed in the enclosure. The trim tab includes a generally planar top, bottom, side and front surfaces linked by a curved surface defining a wedge shaped body. An actuator is linked to the trim tab pivotally moving the trim tab relative to the enclosure. | 02-25-2010 |
| 20090203270 | REVERSE MECHANISM FOR A JET SYSTEM - A jet propulsion system includes an inlet receiving a fluid, and a housing defining a discharge nozzle through which fluid is discharged to provide propulsion of a vehicle in a first direction. The jet propulsion system also includes a reverse mechanism movable between a deployed position redirecting fluid from the discharge nozzle toward the first direction and providing propulsion of the vehicle in a second direction substantially opposite the first direction and a non-deployed position allowing fluid to exit the discharge nozzle and provide propulsion of the vehicle in the first direction. The reverse mechanism produces a flow entrainment that enhances forward thrust while the reverse mechanism is in the non-deployed position which results in a net thrust gain over the thrust attributed to the discharge nozzle alone. | 08-13-2009 |
