Ronald G Cox

US Patent:

49843478, Jan 15, 1991

Filed:

May 5, 1989

Appl. No.:

7/348872

Inventors:

Ronald L. Cox - Long Beach CA

Assignee:

McDonnell Douglas Corporation - Long Beach CA

International Classification:

B23P 1908

US Classification:

2940206

Abstract:

A method and the resulting structure for attaching a doubler to the damaged skin of an airplane, using the original fastener holes, where the fastener countersinks are filled with interference fitted washers and the new fasteners have an interference fit with the airplane skin, doubler and washers.

US Patent:

58685448, Feb 9, 1999

Filed:

Oct 11, 1996

Appl. No.:

8/730003

Inventors:

Ronald L. Cox - Long Beach CA

Assignee:

McDonnell Douglas Corporation - Hunington Beach CA

International Classification:

B65G 3912

US Classification:

414659

Abstract:

An aircraft cargo loader is provided including a platform having a plurality of rollers for supporting cargo thereon. A base member is disposed below the platform and a plurality of telescoping jacks are disposed between the platform and the base member for lifting the platform. A supply of pressurized gas is connected to the plurality of telescoping jacks. An automatic load balancing system is provided for balancing the load on the platform. The cargo loader is designed to be lightweight and portable so that it can be loaded onto the aircraft and transported therewith.

US Patent:

44351003, Mar 6, 1984

Filed:

Dec 21, 1981

Appl. No.:

6/333114

Inventors:

Ronald L. Cox - Long Beach CA

Assignee:

McDonnell Douglas Corporation - Long Beach CA

International Classification:

B25G 300
F16D 100
F16G 1100

US Classification:

403 27

Abstract:

A fail-safe zero-load hinge or pivot-joint having a first load primary support path comprising a sleeve and nut combination and a secondary or redundant load support path comprising a shaft, sized to be inserted axially through the sleeve with diametrical clearance, for threaded engagement with a nut providing axial clearance from said primary members. The secondary shaft and nut combination holds the joint intact after the primary load members have failed permitting the joint assembly to perform its normal designed function of load carrying with the continued full range of movement without the risk of restricted operation seizure or jamming. A locking cap is provided for simple, safe holding of the nuts of primary and secondary member from disengagement, or even partial back off. A dye indicator may be used to indicate failure of the primary load carrying members.

US Patent:

50590596, Oct 22, 1991

Filed:

Apr 27, 1990

Appl. No.:

7/515583

Inventors:

Ronald L. Cox - Long Beach CA

Assignee:

McDonnell Douglas Corporation - Long Beach CA

International Classification:

F16D 100

US Classification:

4034081

Abstract:

A method and the resulting structure for attaching a doubler to the skin of an airplane, using the original fastener holes, where the fastener countersinks are filled with interference fitted washers and the new fasteners have an interference fit with the airplane skin, doubler and washers.