Abstract: A structural assembly for a battery structure includes a lower wall and a pair of cross members. The lower wall is configured to support a cell stack. The cross members are spaced apart from each other in a longitudinal direction of a vehicle. Each cross member supports a respective side of the cell stack and is configured to extend substantially an entire width of the battery structure. Each cross member includes an outer wall, an inner wall, and connecting members that connect the outer wall to the inner wall. The outer wall, the inner wall, and the connecting members cooperate to define an internal cavity. The inner walls of the cross members are secured to the lower wall to form a unitized structure that houses the cell stack.

Abstract: A structural assembly for a battery structure of a vehicle includes a lower wall and a pair of cross members. The lower wall is configured to support a cell stack. The pair of cross members are spaced apart from each other in a longitudinal direction of the vehicle. Each cross member provides lateral support for a respective side of the cell stack and is configured to extend substantially an entire width of a battery enclosure. Each cross member of the pair of cross members includes an outer wall, an inner wall spaced apart from the outer wall, and connecting members. The outer wall, the inner wall, and connecting members cooperate with each other to define an internal cavity. The inner walls of the pair of cross members are secured to the lower wall and slidable relative to the outer walls of the pair of cross members.

Abstract: A structural assembly for a battery structure includes a first shell, a second shell and a cold plate. The first shell includes a first cross member portion providing lateral support for a respective side of a cell stack. The second shell is secured to the first shell to define a unitized structure that houses the cell stack. The second shell includes a second cross member portion providing lateral support for a respective side of the cell stack and is spaced apart along a longitudinal direction of the vehicle relative to the first cross member portion. The cold plate is housed within the unitized structure. Each of the first and second cross member portions includes an outer wall, an inner wall spaced apart from the outer wall, and connecting members that connect the outer wall to the inner wall.

Abstract: Systems and methods for displaying a map onboard an aircraft are disclosed. A method in accordance with one embodiment of the invention includes displaying a map of an area at least proximate to an aircraft at an aircraft flight deck during flight, with the map presenting a feature having a first position relative to a boundary of the map. The method can further include displaying at least one operator-selectable input element at least proximate to the display of the map and accessible to an operator of the aircraft. The method can still further include receiving via the at least one input element an operator-based request to change a position of the feature on the map relative to the boundary, and, in response to the request, updating the display of the map by shifting all points of the map so that the feature has a second position relative to the boundary, with the second position being different than the first position.

Abstract: A vertical situation display system for use in a vehicle such as, for example, an aircraft, is provided. A side view of an intended route of flight may be shown with altitude restrictions, airspace and instrument approach information, a projected flight path and range to airspeed symbol. The system may show terrain, weather, and traffic information along the intended route of flight. The system may be used in conjunction with a navigational display to enhance situational awareness. The system includes a computer, an electronic display device, an electronic entry device, a memory and a database. The database may contain terrain, airspace and flight planning data and may be updatable.

Abstract: Methods and systems for displaying the source of aircraft control instructions are disclosed. A method in accordance with one embodiment to the invention includes receiving a first target to which an aircraft will be automatically directed upon authorization from an operator, and receiving a second target to which the aircraft will automatically be directed upon meeting a threshold condition. The method can further include displaying the first and second targets at least proximate to each other, with a target to which the aircraft is currently being controlled being displayed in a different manner than a target to which the aircraft is not currently being controlled.