The Boeing Company

Mcdonnell Douglas Corporation

John Dorris, Iii

David Michael Smith

William Worden Cleary

John Anthony Skorupa

Valdis Kibens

David Espineli Parekh

A pneumatic deployment device ('PDD') assists in ejecting containerized cargo bundles from a cargo aircraft during an airdrop. The PDD includes a first structure affixed to the aircraft and a second moveable structure, and which is positioned against a cargo bundle, referred to as a CDS bundle. Typically, a series of CDS bundles are positioned along a line in the cargo hold of the aircraft. A pressurized tank provides compress gas to an airbag that is positioned between the first structure and the second structure. Upon reaching the drop location, the gas is release from the tank to the airbag via a hose, inflating the airbag. The airbag pushes the second structure against the CDS bundle, so that the cargo bundles are ejected faster from the aircraft than would otherwise occur.

Container delivery system rapid deployment device

Mixing of a subsonic exhaust plume from a nozzle is induced and enhanced, and shaping of the plume is controlled, by periodic pulsed jets of fluid injected into the plume from two or more locations spaced circumferentially about the plume. The jets are pulsed out of phase relative to one another. An active flow control apparatus includes at least first and second pulsed jet nozzles circumferentially spaced apart about the exhaust plume near an exit plane of the exhaust nozzle, and a pulse generator operable to supply periodic pulses of fluid to each of the pulsed jet nozzles such that the pulses to each nozzle are out of phase relative to the pulses to the other nozzle or nozzles.

Apparatus and methods for active flow control of a nozzle exhaust plume

An aircraft engine apparatus with a reduced inlet vortex is provided which utilizes a vortex disruption system that periodically discharges pulses of engine bleed fluid through at least one outlet port opening through the inlet of the engine nacelle to disrupt the engine inlet vortex. The vortex disruption system thereby prevents ingestion of foreign matter into the engine inlet without sacrificing engine power, efficiency, or aircraft cruise performance.

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Cypress, CA, United States of America

John Dorris, Iii