Abstract: According to the invention, there is provided seed and plants of the corn variety designated CV399333. The invention thus relates to the plants, seeds and tissue cultures of the variety CV399333, and to methods for producing a corn plant produced by crossing a corn plant of variety CV399333 with itself or with another corn plant, such as a plant of another variety. The invention further relates to corn seeds and plants produced by crossing plants of variety CV399333 with plants of another variety, such as another inbred line. The invention further relates to the inbred and hybrid genetic complements of plants of variety CV399333.

Abstract: According to the invention, there is provided seed and plants of the corn variety designated CV399175. The invention thus relates to the plants, seeds and tissue cultures of the variety CV399175, and to methods for producing a corn plant produced by crossing a corn plant of variety CV399175 with itself or with another corn plant, such as a plant of another variety. The invention further relates to corn seeds and plants produced by crossing plants of variety CV399175 with plants of another variety, such as another inbred line. The invention further relates to the inbred and hybrid genetic complements of plants of variety CV399175.

Abstract: Aspects disclosed herein provide an operator training system that can train an operator about basic machine movements, operations, and applications, such as asphalt compactor rolling patterns, paving-by-numbers, milling-by-numbers, etc. with the use of a virtual reality headset at any point or time on a work site. The operator training system uses data received from the virtual reality headset and associated hand controls to guide the operator via training scenarios. The operator training system also includes providing immediate feedback on the outcome of the training scenario and may also identify one or more areas of improvement.

Abstract: Embodiments of the present invention are directed to processes for the production of (R)-3-hydroxybutyl (R)-3-hydroxybyrate. Poly (R)-3-hydroxybyrate is transesterified with an alcohol, to form a first ester portion and a second ester portion. The first ester portion is reduced to the diol to form a diol portion and the diol portion is reacted with the second ester portion to produce (R)-3-hydroxybutyl (R)-3-hydroxybyrate.

Abstract: Embodiments of the present invention are directed to processes for the production of (R)-3-hydroxybutyl (R)-3-hydroxybyrate. Poly (R)-3-hydroxybyrate is transesterified with an alcohol, to form a first ester portion and a second ester portion. The first ester portion is reduced to the diol to form a diol portion and the diol portion is reacted with the second ester portion to produce (R)-3-hydroxybutyl (R)-3-hydroxybyrate.

Abstract: Novel compounds and compositions containing (R)-3-hydroxybutyrate derivatives are disclosed. The compounds and compositions can be used as nutritional supplements to increase physical performance and as therapeutics to ameliorate symptoms of medical conditions, particularly neurological conditions, such as Alzheimer's and similar conditions. Novel methods for making R-3-hydroxybutyrate derivatives also are disclosed. Exemplary methods employ a supercritical solvent, such as supercritical carbon dioxide, and employ a lipase catalyzed esterification or transesterification reaction to produce the (R)-3-hydroxybutyrate derivatives.

Abstract: Novel compounds and compositions containing (R)-3-hydroxybutyrate derivatives are disclosed. The compounds and compositions can be used as nutritional supplements to increase physical performance and as therapeutics to ameliorate symptoms of medical conditions, particularly neurological conditions, such as Alzheimer's and similar conditions. Novel methods for making R-3-hydroxybutyrate derivatives also are disclosed. Exemplary methods employ a supercritical solvent, such as supercritical carbon dioxide, and employ a lipase catalyzed esterification or transesterification reaction to produce the (R)-3-hydroxybutyrate derivatives.

Abstract: A self-aligning structural attachment and a corresponding method are disclosed. The self-aligning structural attachment includes a main body having a proximal end and a distal end, wherein the main body is attached to (i) a CIP of a support system and (ii) a clevis on an airframe of an aircraft. Further, the self-aligning structural attachment includes a first attachment fitting disposed on the proximal end, wherein the first attachment fitting is a slide-and-swivel attachment fitting. Still further, the self-aligning structural attachment includes a second attachment fitting disposed on the distal end, wherein the second attachment fitting is a slide attachment fitting. Yet still further, the self-aligning structural attachment includes a pivoting hinge disposed between the first attachment fitting and the second attachment fitting.

Abstract: A fan shroud assembly (10) includes a fan shroud (14) having a boss (54) formed thereon, and a shield (22) having an aperture (58) and at least one slot (62) communicating with the aperture to allow deflection of the shield in a region adjacent the aperture. The aperture is smaller than the boss such that the aperture receives the boss with an interference fit, causing deflection of the shield, to secure the shield on the fan shroud.

Abstract: A dual-bracketed support system and a corresponding method are disclosed. The dual-bracketed support system includes (i) a first bracket connected to a support structure for a crown portion of an aircraft, (ii) a second bracket, and (iii) a support rod having a proximal end and a distal end. The proximal end is connected to the first bracket and the distal end is connected to the second bracket. The second bracket is configured to allow the support rod to translate along a longitudinal axis defined by the support rod.

Abstract: A self-aligning structural attachment and a corresponding method are disclosed. The self-aligning structural attachment includes a main body having a proximal end and a distal end, wherein the main body is attached to (i) a CIP of a support system and (ii) a clevis on an airframe of an aircraft. Further, the self-aligning structural attachment includes a first attachment fitting disposed on the proximal end, wherein the first attachment fitting is a slide-and-swivel attachment fitting. Still further, the self-aligning structural attachment includes a second attachment fitting disposed on the distal end, wherein the second attachment fitting is a slide attachment fitting. Yet still further, the self-aligning structural attachment includes a pivoting hinge disposed between the first attachment fitting and the second attachment fitting.

Abstract: A system for adjusting a height of a ceiling panel in an aircraft and a corresponding method is disclosed. The system includes an arm and at least one ceiling support latch, wherein each of the at least one ceiling support latches is attached to the arm. The system further includes an adjustable fitting attached to the arm, wherein the adjustable fitting includes (i) a first sliding block attached to the arm, (ii) a second sliding block attached to a support structure, and (iii) an adjustment screw. Adjustment of the adjustment screw forces the first and second sliding blocks to move relative to one another.

Abstract: Novel compounds and compositions containing (R)-3-hydroxybutyrate derivatives are disclosed. The compounds and compositions can be used as nutritional supplements to increase physical performance and as therapeutics to ameliorate symptoms of medical conditions, particularly neurological conditions, such as Alzheimer's and similar conditions. Novel methods for making R-3-hydroxybutyrate derivatives also are disclosed. Exemplary methods employ a supercritical solvent, such as supercritical carbon dioxide, and employ a lipase catalyzed esterification or transesterification reaction to produce the (R)-3-hydroxybutyrate derivatives.

Abstract: A self-aligning structural attachment and a corresponding method are disclosed. The self-aligning structural attachment includes a main body having a proximal end and a distal end, wherein the main body is attached to (i) a CIP of a support system and (ii) a clevis on an airframe of an aircraft. Further, the self-aligning structural attachment includes a first attachment fitting disposed on the proximal end, wherein the first attachment fitting is a slide-and-swivel attachment fitting. Still further, the self-aligning structural attachment includes a second attachment fitting disposed on the distal end, wherein the second attachment fitting is a slide attachment fitting. Yet still further, the self-aligning structural attachment includes a pivoting hinge disposed between the first attachment fitting and the second attachment fitting.

Abstract: A support system for a crown area of an aircraft and a corresponding method is disclosed. The support system includes a crown integration panel (CIP). The CIP is configured to provide a mounting surface for a plurality of aircraft equipment and to provide an electrical ground for at least one of the aircraft equipment of the plurality of aircraft equipment. The system further includes a first attachment and a second attachment attached to the CIP. The first attachment and the second attachment are configured to attach to an airframe of the aircraft. The system further includes a crown raceway support (CRS) having a first end and a second end, where the first end is attached to a first end of the CIP and the second end is configured to attach to an outboard rail of the aircraft.

Abstract: A fan shroud assembly (10) includes a fan shroud (14) having a boss (54) formed thereon, and a shield (22) having an aperture (58) and at least one slot (62) communicating with the aperture to allow deflection of the shield in a region adjacent the aperture. The aperture is smaller than the boss such that the aperture receives the boss with an interference fit, causing deflection of the shield, to secure the shield on the fan shroud.

Abstract: A support system for a crown area of an aircraft and a corresponding method is disclosed. The support system includes a crown integration panel (CIP). The CIP is configured to provide a mounting surface for a plurality of aircraft equipment and to provide an electrical ground for at least one of the aircraft equipment of the plurality of aircraft equipment. The system further includes a first attachment and a second attachment attached to the CIP. The first attachment and the second attachment are configured to attach to an airframe of the aircraft. The system further includes a crown raceway support (CRS) having a first end and a second end, where the first end is attached to a first end of the CIP and the second end is configured to attach to an outboard rail of the aircraft.

Abstract: A dual-bracketed support system and a corresponding method are disclosed. The dual-bracketed support system includes (i) a first bracket connected to a support structure for a crown portion of an aircraft, (ii) a second bracket, and (iii) a support rod having a proximal end and a distal end. The proximal end is connected to the first bracket and the distal end is connected to the second bracket. The second bracket is configured to allow the support rod to translate along a longitudinal axis defined by the support rod.

Abstract: A self-aligning structural attachment and a corresponding method are disclosed. The self-aligning structural attachment includes a main body having a proximal end and a distal end, wherein the main body is attached to (i) a CIP of a support system and (ii) a clevis on an airframe of an aircraft. Further, the self-aligning structural attachment includes a first attachment fitting disposed on the proximal end, wherein the first attachment fitting is a slide-and-swivel attachment fitting. Still further, the self-aligning structural attachment includes a second attachment fitting disposed on the distal end, wherein the second attachment fitting is a slide attachment fitting. Yet still further, the self-aligning structural attachment includes a pivoting hinge disposed between the first attachment fitting and the second attachment fitting.

Abstract: A system for adjusting a height of a ceiling panel in an aircraft and a corresponding method is disclosed. The system includes an arm and at least one ceiling support latch, wherein each of the at least one ceiling support latches is attached to the arm. The system further includes an adjustable fitting attached to the arm, wherein the adjustable fitting includes (i) a first sliding block attached to the arm, (ii) a second sliding block attached to a support structure, and (iii) an adjustment screw. Adjustment of the adjustment screw forces the first and second sliding blocks to move relative to one another.