Abstract: A stand for positioning a mobile device comprises a quick attach mount configured to receive a mobile device and a height-adjustable upright member connected to support the quick attach mount and adjustable to position the quick attach mount within a desired height range for users.

Abstract: A stand for positioning a mobile device comprises a quick attach mount configured to receive a mobile device and a height-adjustable upright member connected to support the quick attach mount and adjustable to position the quick attach mount within a desired height range for users.

Abstract: A hinge pin for pivotally mounting at least one of a toilet seat and a lid to a toilet or surrounding structure comprises a first hinge pin component, a second hinge pin component a linking member and fasteners. The first hinge pin component and the second hinge pin component each has a cylindrical outer end, a semicylindrical inner end with a flat joining surface and a shoulder between the outer end and the inner end. The linking member is semicylindrical and has a flat linking surface dimensioned to link the first hinge pin component and the second hinge component when they are axially aligned with their inner ends facing each other and the linking surface is in contact with each joining surface and secured by the fasteners. The assembled linking member and first and second hinge components define a center section of the hinge pin having a circular cross section.

Abstract: A method of establishing a runway approach procedure for an aircraft at a selected runway, comprises, for obstacles in the final approach segment of the flightpath and having obstacle range values greater than the datum range, calculating a missed approach surface height at a projected intersection of a missed approach surface with a descending vertical error budget surface and a corresponding Distance to Height of Missed Approach Surface from the runway (DHMAS). For obstacles in the final approach segment and having obstacle range values less than the datum range, a missed approach surface height and a corresponding DHMAS are calculated using ascending climb gradient requirements. All DHMAS values are compared, and a controlling obstacle is determined as the obstacle having a greatest DHMAS. A decision altitude for the controlling obstacle is calculated, and the runway approach procedure is updated with the decision altitude. Relativistic metadata other obstacles can also be calculated and stored.

Abstract: An air seal assembly for an aircraft control surface comprises a bulb-type air seal, a mounting bracket and a fastener. The bulb-type air seal has a hollow bulb portion, a T-shaped mounting extension, and a first through hole extending through the T-shaped mounting extension. The mounting bracket has a T-shaped channel configured to slidingly receive the T-shaped mounting extension of the air seal and a second through hole. The fastener has a head at one end and an opposite exposed end sized for extending through the first through hole in the T-shaped mounting extension and through the second through hole in the mounting bracket. The exposed end is accessible to tighten the fastener against the bracket to keep the air seal in place within the T-shaped channel.

Abstract: A method for improving fuel economy on a passenger jet aircraft comprises automatically receiving a communication from the aircraft to a ground station comprising at least one subsystem operating parameter measured during the current flight, detecting whether the operating parameter meets predetermined criteria and, if the criteria are met, automatically sending a communication to indicate the aircraft's status for a next flight. If the criteria are not met, a status of the aircraft is automatically changed and a communication is sent. Other methods and systems are also described.

Abstract: An air seal assembly for an aircraft control surface comprises a bulb-type air seal, a mounting bracket and a fastener. The bulb-type air seal has a hollow bulb portion, a T-shaped mounting extension, and a first through hole extending through the T-shaped mounting extension. The mounting bracket has a T-shaped channel configured to slidingly receive the T-shaped mounting extension of the air seal and a second through hole. The fastener has a head at one end and an opposite exposed end sized for extending through the first through hole in the T-shaped mounting extension and through the second through hole in the mounting bracket. The exposed end is accessible to tighten the fastener against the bracket to keep the air seal in place within the T-shaped channel.

Abstract: A method for improving fuel economy on a passenger jet aircraft comprises automatically receiving a communication from the aircraft to a ground station comprising at least one subsystem operating parameter measured during the current flight, detecting whether the operating parameter meets predetermined criteria and, if the criteria are met, automatically sending a communication to indicate the aircraft's status for a next flight. If the criteria are not met, a status of the aircraft is automatically changed and a communication is sent. Other methods and systems are also described.

Abstract: A hinge pin for pivotally mounting at least one of a toilet seat and a lid to a toilet or surrounding structure comprises a first hinge pin component, a second hinge pin component a linking member and fasteners. The first hinge pin component and the second hinge pin component each has a cylindrical outer end, a semicylindrical inner end with a flat joining surface and a shoulder between the outer end and the inner end. The linking member is semicylindrical and has a flat linking surface dimensioned to link the first hinge pin component and the second hinge component when they are axially aligned with their inner ends facing each other and the linking surface is in contact with each joining surface and secured by the fasteners. The assembled linking member and first and second hinge components define a center section of the hinge pin having a circular cross section.

Abstract: A method for improving fuel economy on a passenger jet aircraft comprises automatically receiving a communication from the aircraft to a ground station comprising at least one subsystem operating parameter measured during the current flight, detecting whether the operating parameter meets predetermined criteria and, if the criteria are met, automatically sending a communication to indicate the aircraft's status for a next flight. If the criteria are not met, a status of the aircraft is automatically changed and a communication is sent. Other methods and systems are also described.

Abstract: A method for improving boarding of passengers and baggage onto a flight, comprises, at a predetermined time before the scheduled departure of the flight, determining an eligible carry-on baggage items count of carry-on baggage items eligible for treatment as checked baggage items. The eligible carry-on baggage items count is based on predetermined criteria comprising at least one of an aircraft type for the flight, a passenger load factor for the flight and carrier historical data relevant to the flight. If the eligible carry-on items count is greater than zero, then an offer to a passenger on the flight to have the passenger's carry-on baggage item treated as a checked baggage item is communicated, and the passenger's communication in response to the offer is received. For each accepted offer, decrementing the eligible carry-on items count.

Abstract: A vehicle pneumatic system training aid comprises simulated controls and indicators and a pneumatic circuit. The simulated controls and indicators correspond to at least a portion of controls and indicators on an actual vehicle. The pneumatic circuit comprises a connection to a source of pressurized fluid, and at least one fluid flow control device. The fluid flow control device is positionable in at least two different positions corresponding to different actual vehicle conditions that are simulatable. The simulated controls are actuatable to change a condition of the pneumatic circuit and the simulated indicators are operable to display an indication of the condition of the pneumatic circuit.

Abstract: An improved airport check-in system includes a central conveyor and a plurality of outwardly-extending conveyors. Airline agents operate workstations adjacent the outwardly extending conveyors, which are accessible by passengers so that passengers can deposit their own bags directly onto the conveyors. A number of electronic kiosks are provided to obtain boarding passes having encoded passenger information. Check-in is accomplished in two steps, including first obtaining a boarding pass and then proceeding to a baggage check station to check bags. At the baggage check station, the boarding pass is scanned to quickly retrieve key information that would otherwise have been gathered verbally, hastening the check-in process.