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Browse by: INVENTOR PATENT HOLDER PATENT NUMBER DATE
 
 
Inventor:
Gruensfelder; Cynthia Ann
Address:
St. Louis, MO
No. of patents:
10
Patents:












Patent Number Title Of Patent Date Issued
6260567 Mission adaptive inlet July 17, 2001
A mission adaptive inlet (42) for an aircraft (40) has a rigid lip panel (56) pivotally attached to an inlet (42) of the aircraft (40). An actuation mechanism is coupled to the rigid lip panel (56) and causes the rigid lip panel (56) to pivot from a first position to a second position.
6231006 Mission adaptive inlet May 15, 2001
A mission adaptive inlet (42) for an aircraft (40) has a rigid lip panel (56) pivotally attached to an inlet (42) of the aircraft (40). An actuation mechanism is coupled to the rigid lip panel (56) and causes the rigid lip panel (56) to pivot from a first position to a second position.
6213433 Leading edge for an aircraft April 10, 2001
A leading edge (50) for an aircraft has a hard durometer elastomer tip (52). An elastomer panel (54) has a first end attached to the hard durometer elastomer tip (52) and has a plurality of reinforcing members capable of freely sliding inside the elastomer panel (54). A rigid block (
6089505 Mission adaptive inlet July 18, 2000
A mission adaptive inlet (42) for an aircraft (40) has a rigid lip panel (56) pivotally attached to an inlet (42) of the aircraft (40). An actuation mechanism is coupled to the rigid lip panel (56) and causes the rigid lip panel (56) to pivot from a first position to a second position.
6079667 Auxiliary inlet for a jet engine June 27, 2000
An auxiliary inlet (60) for a jet engine has a first rod block (62) attached to a first side (64) of a hole (66) in a skin (68) of an inlet of the jet engine. A second rod block (80) is attached to an opposing side (82) of the hole (66) in the skin (68) of the inlet of the jet engine. A
6076766 Folding wing for an aircraft June 20, 2000
A wing fold (50) for an aircraft has inner wing (74) connected to the aircraft and an outer wing (76) connected to the inner wing (74) by a hinge (72). An actuator (72) is capable of rotating the outer wing (76) over ninety degrees with respect to the inner wing (74). A first reinfor
6068215 Expandable aircraft cargo bay and method May 30, 2000
An aircraft (50) with a variable cargo bay (52) includes a frame (60) having an inner surface and an outer skin (64) covering the frame (60). The frame (60) has a pair of faceted fairings (54, 56) coupled to the frame (60) and a door assembly (58) between the pair of faceted fairings
5979828 Apparatus for eliminating gaps in an aircraft November 9, 1999
An apparatus (30) for eliminating gaps (20) in a door of an airplane has an elastaueric bladder (32) bonding along an edge (24) of a door gap (20). The elastomeric bladder (32) includes a port providing for access to an interior cavity (34). A pneumatic actuator is coupled to the port.
5975463 Expandable aircraft bay and method November 2, 1999
An aircraft (50) with a variable cargo bay (52) includes a frame (60). A pair of fairing assemblies (54, 56) is coupled to the frame (60). Each of the pair of fairing assemblies (54, 56) has a ramp (100) connected to the frame (60) by a front sliding pivoting mechanism (106). A door asse
5931422 Active reinforced elastomer system August 3, 1999
An active reinforced elastomer system (50) has a rigid attachment block (56). A stiffening member (58) slides through an opening in the rigid attachment block (56). A shape memory alloy structure (62) is attached to the rigid attachment block (56). An elastomer panel (52) is attached to










 
 
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