Abstract: Disclosed is a pedal drive system for use with a watercraft that facilitates propelling of the watercraft. The pedal drive system of the present invention is placed through an opening in the bottom of the watercraft and affixed to the body of the watercraft. The propeller is then attached to a drive shaft. The user provides mechanical input (e.g., rotational force) by rotating pedals of a pedal arrangement of the pedal drive system. The rotational force is transferred from the drive assembly through the gears to the drive shafts that rotates the propeller, thus driving the watercraft forward as well as backward.

Abstract: Disclosed is a pedal drive system for use with a watercraft that facilitates propelling of the watercraft. The pedal drive system of the present invention is placed through an opening in the bottom of the watercraft and affixed to the body of the watercraft. The propeller is then attached to a drive shaft. The user provides mechanical input (e.g., rotational force) by rotating pedals of a pedal arrangement of the pedal drive system. The rotational force is transferred from the drive assembly through the gears to the drive shafts that rotates the propeller, thus driving the watercraft forward as well as backward.

Abstract: A system and method for filtering various targets (such as ground vehicles, stationary objects, and aircraft) from display on a display screen within the cockpit of an “Own Ship” aircraft. The system and method withhold from display any non-exempt targets that have an altitude that is either: (1) greater than an upper-threshold altitude; or (2) less than a lower-threshold altitude. The upper-threshold altitude and the lower-threshold altitude may be set to user-specified, customized values as desired to accommodate current flying conditions. In addition, the system and method may also be configured to operate in a plurality of operating modes, each of which features a different upper threshold altitude/lower threshold altitude combination. The system and method are preferably configured to reset certain threshold altitudes to pre-defined default altitudes in response to the aircraft landing.

Abstract: A system and method for filtering various targets (such as ground vehicles, stationary objects, and aircraft) from display on a display screen within the cockpit of an “Own Ship” aircraft. The system and method withhold from display any non-exempt targets that have an altitude that is either: (1) greater than an upper-threshold altitude; or (2) less than a lower-threshold altitude. The upper-threshold altitude and the lower-threshold altitude may be set to user-specified, customized values as desired to accommodate current flying conditions. In addition, the system and method may also be configured to operate in a plurality of operating modes, each of which features a different upper threshold altitude/lower threshold altitude combination. The system and method are preferably configured to reset certain threshold altitudes to pre-defined default altitudes in response to the aircraft landing.

Abstract: The present invention provides an aircraft navigational system including a graphical user interface that is capable of displaying navigational information in a split-screen format. The split-screen format includes displaying multiple graphical user panels, each depicting different traffic information. For example, one of the panels displays a plurality of air traffic symbols corresponding to airborne obstacles and another of the panels simultaneously displays ground traffic symbols representing ground obstacles. The obstacles can include other aircraft in the air and on runways as the pilot's aircraft approaches for a landing. The navigational system also is capable of switching between a single graphical user panel and multiple panels in response to a triggering event, such as a change in the course of the aircraft.

Abstract: The present invention provides an aircraft navigational system including a graphical user interface that is capable of displaying navigational information in a split-screen format. The split-screen format includes displaying multiple graphical user panels, each depicting different traffic information. For example, one of the panels displays a plurality of air traffic symbols corresponding to airborne obstacles and another of the panels simultaneously displays ground traffic symbols representing ground obstacles. The obstacles can include other aircraft in the air and on runways as the pilot's aircraft approaches for a landing. The navigational system also is capable of switching between a single graphical user panel and multiple panels in response to a triggering event, such as a change in the course of the aircraft.

Abstract: The present invention provides an aircraft navigational system including a graphical user interface that is capable of displaying navigational information in a split-screen format. The split-screen format includes displaying multiple graphical user panels, each depicting different traffic information. For example, one of the panels displays a plurality of air traffic symbols corresponding to airborne obstacles and another of the panels simultaneously displays ground traffic symbols representing ground obstacles. The obstacles can include other aircraft in the air and on runways as the pilot's aircraft approaches for a landing. The navigational system also is capable of switching between a single graphical user panel and multiple panels in response to a triggering event, such as a change in the course of the aircraft.

Abstract: A communications system provides subfleet calls for both voice and data communications using a secondary identification (301, 303, 305, 307, 309) incorporating a plurality of subfleets in a hierarchical arrangement. A message including the secondary identification (301, 303, 305, 307, 309) is transmitted to a communication unit (117) having a stored secondary identification (301, 303, 305, 307, 309). If the transmitted secondary identification sufficiently matches the stored secondary identification, the communication unit (117) responds to the instructions in the transmitted message.

Abstract: A mercury switch has two spaced apart electrical contacts mechanically supported by its glass envelope and electrically connected to external terminals. A third conductor passes through the glass envelope at the opposite end. A housing for mercury is formed by divergent plates supported on the third conductor, which housing extends into the mercury reservoir near its support so as to draw mercury into the space between the divergent plates. A magnetic partition is supported from the third conductor by a flexible hinge which allows the partition to move back and forth between the divergent plates of the housing alternately into each of a pair of stops between said two spaced apart electrical contacts. Whichever wall of the housing the partition is closest to, the space is narrowed so that the mercury rises under capillary attraction and contacts the electrical contact between the wall and the partition.

Abstract: A movable magnetic armature of a size to nest within stepped faces on a fixed magnetic pole piece and on the armature support, respectively, is attached to the armature support by a conductive spring member which normally biases the armature away from the nested position in which it contacts a contact and stop member on the fixed pole. Imposition of the magnetic field causes the armature to move into closed contact position. The position of the armature even when in open contact position is close to the steps of the fixed pole piece as well as the armature support providing a low reluctance, short throw, quick action switch.

Abstract: The magnetic elements of a mercury reed switch are supported within their non-magnetic capsule so that, instead of coming into contact in initially overlapping relationship, under the influence of a magnetic field they become essentially aligned with one another. The reeds are so constructed that by selection of the size or shape of their respective opposed ends, the magnetic flux pattern is modified to maintain desired relative alignment to achieve desired spacing between solid contacts. In a preferred form at least one of the magnetic elements carries a substantially non-magnetic conductive extension means, conductively affixed to its supporting element in position to complete an electrical circuit from its supporting element through intermediate conductive liquid and the other reed element in some switch condition.

Abstract: The magnetic elements of a reed switch are supported within their non-magnetic capsule so that, instead of coming into contact in initially overlapping relationship, under the influence of a magnetic field they become essentially aligned with one another. The reeds may be so constructed that by selection of the size or shape of their respective opposed ends, the magnetic flux pattern is modified to maintain desired relative alignment to achieve desired contact. The invention relates to a mercury wetted switch which employs mercury to complete electrical contact between the non-contacting ends of the reeds.