Abstract: A grabber assembly including a carriage, a pin, a first adapter, a second adapter, and a sleeve. The pin extends through a bushing of a grabber arm. The bushing is pivotally coupled with the pin. The first adapter is coupled with the carriage and configured to receive a first end of the pin. The second adapter is coupled with the carriage and configured to receive a second end of the pin. The sleeve extends co-cylindrically with the pin, the sleeve positioned within a central bore of the bushing between the bushing and the pin.

Abstract: A grabber assembly including a carriage, a pin, a first adapter, a second adapter, and a sleeve. The pin extends through a bushing of a grabber arm. The bushing is pivotally coupled with the pin. The first adapter is coupled with the carriage and configured to receive a first end of the pin. The second adapter is coupled with the carriage and configured to receive a second end of the pin. The sleeve extends co-cylindrically with the pin, the sleeve positioned within a central bore of the bushing between the bushing and the pin.

Abstract: A grabber assembly including a carriage, a pin, a first adapter, a second adapter, and a sleeve. The pin extends through a bushing of a grabber arm. The bushing is pivotally coupled with the pin. The first adapter is coupled with the carriage and configured to receive a first end of the pin. The second adapter is coupled with the carriage and configured to receive a second end of the pin. The sleeve extends co-cylindrically with the pin, the sleeve positioned within a central bore of the bushing between the bushing and the pin.

Abstract: A grabber assembly including a carriage, a pin, a first adapter, a second adapter, and a sleeve. The pin extends through a bushing of a grabber arm. The bushing is pivotally coupled with the pin. The first adapter is coupled with the carriage and configured to receive a first end of the pin. The second adapter is coupled with the carriage and configured to receive a second end of the pin. The sleeve extends co-cylindrically with the pin, the sleeve positioned within a central bore of the bushing between the bushing and the pin.

Abstract: A grabber assembly includes a carriage, an adapter assembly, and a grabber arm. The adapter assembly is coupled to the carriage and includes a pin, a first member, a second member, and a sleeve. The first member is configured to receive a first end of the pin and removably fixedly couple with the first end of the pin. The second member is configured to receive a second end of the pin and removably fixedly couple with the second end of the pin. The sleeve extends co-cylindrically with the pin. The grabber arm includes a bushing. The bushing is fixedly coupled with the grabber arm and is pivotally coupled to the pin. The sleeve is positioned within a central bore of the bushing, between the bushing and the pin.

Abstract: The present invention relates to a composition comprising one or more perovskite precursors dissolved in a mixture of solvents comprising: i. one or more polar aprotic solvents, each selected in such a way that it can, when used in absence of other components, dissolve said one or more perovskite precursors, ii. one or more linear alcohols of general formula CnH2n+1OH, wherein n is from 1 to 12, and iii. optionally, one or more acids wherein the polar aprotic solvent or mixture of polar aprotic solvents represent between 50 and 95 vol % of the mixture of solvents, wherein the vol % of the mixture of solvents not occupied by polar aprotic solvents is occupied for at least 90 vol %, preferably for 100 vol %, by the one or more linear alcohols, and the one or more acids if present.

Abstract: A grabber assembly includes a carriage, an adapter assembly, and a grabber arm. The adapter assembly is coupled to the carriage and includes a pin, a first member, a second member, and a sleeve. The first member is configured to receive a first end of the pin and removably fixedly couple with the first end of the pin. The second member is configured to receive a second end of the pin and removably fixedly couple with the second end of the pin. The sleeve extends co-cylindrically with the pin. The grabber arm includes a bushing. The bushing is fixedly coupled with the grabber arm and is pivotally coupled to the pin. The sleeve is positioned within a central bore of the bushing, between the bushing and the pin.

Abstract: The present invention relates to a composition comprising one or more perovskite precursors dissolved in a mixture of solvents comprising: i. one or more polar aprotic solvents, each selected in such a way that it can, when used in absence of other components, dissolve said one or more perovskite precursors, ii. one or more linear alcohols of general formula CnH2n+1OH, wherein n is from 1 to 12, and iii. optionally, one or more acids wherein the polar aprotic solvent or mixture of polar aprotic solvents represent between 50 and 95 vol % of the mixture of solvents, wherein the vol % of the mixture of solvents not occupied by polar aprotic solvents is occupied for at least 90 vol %, preferably for 100 vol %, by the one or more linear alcohols, and the one or more acids if present.

Abstract: A folding wing for an aircraft comprises first and second inboard wing sections, and first and second outboard wing sections. The first and second inboard wing sections rotate about a centerline hinge, and a centerline spring applies force to the first and second inboard wing sections to rotate the first and second inboard wing sections from a stowed position to a deployed position. At least one of the first and second inboard wing sections translates along the axis of rotation of the first and second inboard wing sections as they move from the stowed to the deployed positions. The first and second outboard wing sections rotate between the stowed and the deployed positions about first and second outboard hinges.

Abstract: A folding wing for an aircraft comprises first and second inboard wing sections, and first and second outboard wing sections. The first and second inboard wing sections rotate about a centerline hinge, and a centerline spring applies force to the first and second inboard wing sections to rotate the first and second inboard wing sections from a stowed position to a deployed position. At least one of the first and second inboard wing sections translates along the axis of rotation of the first and second inboard wing sections as they move from the stowed to the deployed positions. The first and second outboard wing sections rotate between the stowed and the deployed positions about first and second outboard hinges.