The Boeing Company

Ross E Rockstad

Paul Nelsen Stavig, Jr

Stephen F Thompson

A fluid dispenser is described that includes a dispenser, a cap, and an insert. The dispenser is flexible and includes a body portion and a cylindrical mouth portion extending from the body portion. The mouth portion has an opening defining a lip. The cap is operable to engage the mouth portion of the dispenser, said cap has an aperture therethrough operable to dispense a fluid stored within the dispenser. The insert is sized for placement within the opening, between the mouth portion and the cap and includes a substantially solid plug having a first and a second axial hole therethrough, a first reed valve operably attached to the plug to close the first axial hole from an outside of the dispenser, and a second reed valve operably attached to the plug to close the second axial hole from an inside of the dispenser.

Self-sealing dispenser insert and method for assembling the same

An installation tool for installing a support hanger in an aircraft, where the support hanger includes a main hook body and a complimentary hook body slidably coupled with the main hook body. The support hanger further includes a locking mechanism for selectively locking the main hook body and the complimentary hook body. The installation tool comprises a handle having a pivot surface that engages the main hook body of the support hanger. A wedge-shaped slot is formed in the handle and includes a pair of surfaces. An interfering member is then disposed within the wedge-shaped slot. This interfering member is positionable in a first position where the interfering member engages at least one of the pair of surfaces and a free end of the complimentary hook body and a second position where the interfering member is disengaged from the pair of surfaces so as to permit simple and convenient tightening of the support hanger.

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Maple Valley, WA, United States of America

Ross E Rockstad