Abstract: An inlet for use with a nacelle having an axis includes an outer barrel. The inlet further includes a lip skin defining a plurality of elongated exit holes including a first circumferential outer hole, a second circumferential outer hole, and a plurality of center holes located between the first circumferential outer hole and the second circumferential outer hole, the first circumferential outer hole being located at least 10 degrees of an entire circumference of the inlet away from the second circumferential outer hole.

Abstract: An inlet for use with a nacelle having an axis includes an outer barrel. The inlet further includes a lip skin defining a plurality of elongated exit holes including a first circumferential outer hole, a second circumferential outer hole, and a plurality of center holes located between the first circumferential outer hole and the second circumferential outer hole, the first circumferential outer hole being located at least 10 degrees of an entire circumference of the inlet away from the second circumferential outer hole.

Abstract: A thermal blanket system is provided on an aircraft component to protect the component, for example, from engine heat. The component has a latch half attached thereto, which is also covered by the thermal blanket system. In some scenarios, the latch half may need to be detached from the component because the latch was stuck closed. The thermal blanket system includes a portion thereof which overlaps the latch half and breaks away from the remainder of the thermal blanket system when the latch half is detached.

Abstract: A thermal blanket system is provided on an aircraft component to protect the component, for example, from engine heat. The component has a latch half attached thereto, which is also covered by the thermal blanket system. In some scenarios, the latch half may need to be detached from the component because the latch was stuck closed. The thermal blanket system includes a portion thereof which overlaps the latch half and breaks away from the remainder of the thermal blanket system when the latch half is detached.

Abstract: A carrier for heart valves allows the removal of a heart valve from the carrier without manual manipulation. In addition, the carrier minimizes or substantially eliminates leaking of preserving fluid during transportation and storage. The carrier includes ajar, a rinse cage, and a holder to which a heart valve is attachable. The rinse cage includes a first engagement structure, for example, a channel, and the holder includes a second engagement structure, for example, a groove, complementary to the first engagement structure for releasably engaging therewith. A heart valve attached to the holder is disposed or suspended within the rinse cage when the engagement structures are engaged. A heart valve attached to the holder is protected not only when within the jar but also when removed from the jar. The holder has a socket for engaging with a surgical handle used to remove the valve from the jar for rinsing and implantation.