Abstract: A method for treating a salt solution, the method comprising (i) introducing a liquid motive fluid into an eductor; (ii) drawing vapor from a distillation tank into the eductor, where said drawing reduces the pressure within the distillation tank; (iii) mixing the motive fluid and the vapor within the eductor to produce a liquid stream, where the vapor condenses within said eductor and thereby releases heat and at least a portion of the heat is transferred to the liquid stream; (iv) transferring at least a portion of the heat associated with the liquid stream to a salt solution; and (v) distilling the salt solution within the distillation tank.

Abstract: A system includes a mandrel having an exterior surface configured to receive composite material, a first end, and a second end opposite the first end, an end support coupled to the first end of the mandrel such that the mandrel is rotatable about an axis of rotation, and an intermediate support configured to support the mandrel between the first end and the second end such that at least a portion of the exterior surface is exposed while the mandrel is supported by the intermediate support, a vertical distance between the intermediate support and the axis of rotation defining a support distance, and the intermediate support being adjustable between a first position having a first support distance and a second position having a second support distance greater than the first support distance.

Abstract: According to an aspect, a method of assembling a mandrel includes assembling a plurality of members via interlocking features arranged at opposing edges of each member of the plurality of members to form a compartment, the assembled members having a collective outer surface that conforms to an inner surface of the spar. A support member is inserted into the compartment formed radially inward from the assembled members, the support member making contact with a portion of each member of the plurality of members.

Abstract: According to an aspect, a method of assembling a mandrel includes assembling a plurality of members via interlocking features arranged at opposing edges of each member of the plurality of members to form a compartment, the assembled members having a collective outer surface that conforms to an inner surface of the spar. A support member is inserted into the compartment formed radially inward from the assembled members, the support member making contact with a portion of each member of the plurality of members.

Abstract: According to an aspect, a method of assembling a mandrel includes assembling a plurality of members via interlocking features arranged at opposing edges of each member of the plurality of members to form a compartment, the assembled members having a collective outer surface that conforms to an inner surface of the spar. A support member is inserted into the compartment formed radially inward from the assembled members, the support member making contact with a portion of each member of the plurality of members.

Abstract: A pitch beam movable by a pitch change shaft to adjust a pitch of at least one rotor blade of a rotor system via a pitch linkage includes a first surface having a generally planar configuration, a smooth second surface disposed opposite the first surface, and a sidewall extending between the first surface and the second surface. A pitch linkage connection point is disposed at the sidewall to which the pitch linkage is attachable. An interior is defined between the first surface and the second surface and an opening extends through the first and second surface at a rotational axis of the rotor system to which the pitch change shaft is attached. Movement of the pitch change shaft moves the pitch beam and adjusts the pitch of the at least one rotor blade via the pitch linkage attached at the pitch linkage connection point.

Abstract: A system includes a mandrel having an exterior surface configured to receive composite material, a first end, and a second end opposite the first end, an end support coupled to the first end of the mandrel such that the mandrel is rotatable about an axis of rotation, and an intermediate support configured to support the mandrel between the first end and the second end such that at least a portion of the exterior surface is exposed while the mandrel is supported by the intermediate support, a vertical distance between the intermediate support and the axis of rotation defining a support distance, and the intermediate support being adjustable between a first position having a first support distance and a second position having a second support distance greater than the first support distance.

Abstract: According to an aspect, a method of assembling a mandrel includes assembling a plurality of members via interlocking features arranged at opposing edges of each member of the plurality of members to form a compartment, the assembled members having a collective outer surface that conforms to an inner surface of the spar. A support member is inserted into the compartment formed radially inward from the assembled members, the support member making contact with a portion of each member of the plurality of members.

Abstract: An aircraft rotor blade assembly includes a rotor blade rotatable about an axis of rotation and a weighted assembly mounted to the aircraft rotor blade. The weighted assembly includes an actuator which moves a mass to adjust a moment of the rotor blade assembly when the rotor blade is rotated about the axis of rotation.

Abstract: A pitch beam movable by a pitch change shaft to adjust a pitch of at least one rotor blade of a rotor system via a pitch linkage includes a first surface having a generally planar configuration, a smooth second surface disposed opposite the first surface, and a sidewall extending between the first surface and the second surface. A pitch linkage connection point is disposed at the sidewall to which the pitch linkage is attachable. An interior is defined between the first surface and the second surface and an opening extends through the first and second surface at a rotational axis of the rotor system to which the pitch change shaft is attached. Movement of the pitch change shaft moves the pitch beam and adjusts the pitch of the at least one rotor blade via the pitch linkage attached at the pitch linkage connection point.

Abstract: A method and computer program product for identifying errors in a computerized preparation of an electronic financial document to be submitted to an agency. A financial document preparation program is executed, a first connection is initiated with a computer of the agency, the schema requirements are received from the agency via the first connection, data entry fields are generated, data entered into the data entry fields is received, error rules are generated from the schema requirements, each error rule associated with a respective one of the data entry fields associated with the electronic financial document, the data entered into the data entry fields is checked against the respective error rules to identify schema errors in the data entered into the data entry fields, the electronic financial document is generated based on the data entered into the data entry fields, and the electronic financial document is electronically transmitted to the agency.

Abstract: A bushing assembly for receiving a fastener includes a first bushing portion and a second bushing portion arranged coaxially with the first bushing portion. The second bushing portion defines at least part of an opening for receiving the fastener. The second bushing portion is rotatable relative to the first bushing portion about an axis of rotation to adjust a position of the opening about a first axis and a second axis independently relative to the first bushing portion and the second bushing portion. The first axis is coplanar with and perpendicular to the second axis.

Abstract: A bushing assembly for receiving a fastener includes a first bushing portion and a second bushing portion arranged coaxially with the first bushing portion. The second bushing portion defines at least part of an opening for receiving the fastener. The second bushing portion is rotatable relative to the first bushing portion about an axis of rotation to adjust a position of the opening about a first axis and a second axis independently relative to the first bushing portion and the second bushing portion. The first axis is coplanar with and perpendicular to the second axis.

Abstract: An aircraft rotor blade assembly includes a rotor blade rotatable about an axis of rotation and a weighted assembly mounted to the aircraft rotor blade. The weighted assembly includes an actuator which moves a mass to adjust a moment of the rotor blade assembly when the rotor blade is rotated about the axis of rotation.

Abstract: A method and computer program product for identifying errors in a computerized preparation of an electronic financial document to be submitted to an agency. A financial document preparation program is executed, a first connection is initiated with a computer of the agency, the schema requirements are received from the agency via the first connection, data entry fields are generated, data entered into the data entry fields is received, error rules are generated from the schema requirements, each error rule associated with a respective one of the data entry fields associated with the electronic financial document, the data entered into the data entry fields is checked against the respective error rules to identify schema errors in the data entered into the data entry fields, the electronic financial document is generated based on the data entered into the data entry fields, and the electronic financial document is electronically transmitted to the agency.

Abstract: The present invention augments an application update with an automatic sequence of steps for instantiating the updated application in place of the currently running application, without unintended loss of the end-user generated data that comprises all or part of the current application state. The new version may consume most or all of the previously entered data to enter a state of needing a minimal amount of new information (which may be different from being in the state of ready to submit).

Abstract: The present invention provides a method, system, and program product for indicating a state of a value of an application. Specifically, under the present invention a graphical state indicator is displayed for a property (e.g., background screen color) of an application. The graphical state indicator will indicate a “state” of a value of the property. That is, the graphical state indicator will indicate whether the value is a user-defined value, or is a default value. Under the present invention, a graphical state indicator can be provided for any property of the application. As such, multiple graphical state indicators may be simultaneously displayed. The present invention can also display a graphical value indicator for indicating the current value (e.g., blue) of the property (e.g., background screen color). This value can be changed based upon an interaction with the graphical value indicator by a user.

Abstract: The present invention provides visual inspection and physical access into the space of a fluid containment system consisting of an inner storage container or vessel, and an outer, reinforced precast structure, or vault, having a top cover. Visual inspection ports and physical access assemblies, with easily removable covers, are cast into the vault top corners for direct, or remote viewing, such as with a periscope or video camera device, of the exterior surfaces of the inner storage container; the interior surfaces of the outer, vaulted structure; and the space between the two structures. Sufficient physical access and physical maneuverability is provided by the visual inspection port assemblies, and corresponding visual inspection chambers directly below each port assembly, that proactive inspection to verify primary vessel integrity and removal of fluids from the interior space between the two containers can be achieved without personnel entry or removal of the vault top.