Abstract: Thermal control system for aircraft main landing gear wheel wells and related methods are disclosed. An example thermal control system includes a conduit defining a fluid passageway between an inlet and an outlet. The inlet of the conduit positioned in fluid communication with a landing gear wheel well and the outlet of the conduit positioned in fluid communication with the atmosphere. The conduit generates a pressure differential through the fluid passageway between the inlet and the outlet to exhaust heat from the landing gear wheel well to the atmosphere.

Abstract: The present invention relates to a medical device for intradermal or subcutaneous treatment of a patient, comprising: a piercing element to penetrate a skin portion of the patient; an illumination arrangement to illuminate the piercing element and/or to illuminate the skin portion prior and/or during a treatment process, wherein the illumination arrangement is further adapted to visually indicate a predefined treatment sequence of the treatment process.

Abstract: An aircraft passenger suite including a seat configured for movement between an upright position and a horizontal bed position, an ottoman positioned apart from the passenger seat, and at least one armrest assembly configured for vertical movement, wherein the seat, ottoman and at least one armrest reside in horizontal alignment to form a bed in the horizontal bed position.

Abstract: The present invention relates to a medical device for intradermal or subcutaneous treatment of a patient, comprising: a piercing element to penetrate a skin portion of the patient; an illumination arrangement to illuminate the piercing element and/or to illuminate the skin portion prior and/or during a treatment process, wherein the illumination arrangement is further adapted to visually indicate a predefined treatment sequence of the treatment process.

Abstract: An aircraft passenger suite including a seat configured for movement between an upright position and a horizontal bed position, an ottoman positioned apart from the passenger seat, and at least one armrest assembly configured for vertical movement, wherein the seat, ottoman and at least one armrest reside in horizontal alignment to form a bed in the horizontal bed position.

Abstract: A deployable in-flight entertainment monitor attached to a supporting fixture and configured to move between a stowed position wherein the monitor is in a portrait orientation, to a deployed position wherein the monitor is in a landscape orientation, wherein in the deployed position a portion of the monitor overhangs the supporting fixture.