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Patent
   D566032
Priority
Aug 17 2004
Filed
Aug 17 2004
Issued
Apr 08 2008
Expiry
Apr 08 2022
Inventors
Berthou, N…
Assg.orig
Thales Avi…
Airbus Fra…
Assg.curr
Thales Avi…
Airbus Fra…
Entity
unknown
Referenced by
7
References
6
Maint.:
n/a
The ornamental design for a pilot multipurpose cursor control unit for vibrations environment, as shown and described.

FIG. 1 is a front, left and top perspective view of a pilot multipurpose cursor control unit for vibrations environment showing our new design;

FIG. 2 is a partial back, left and top perspective view thereof;

FIG. 3 is a back, left and top perspective view thereof;

FIG. 4 is a top view thereof; and,

FIG. 5 is a back, right and top perspective view thereof.
INVENTORS:

Berthou, Nicolas, Dufal, Jérôme, Guegan, Malo

THIS PATENT IS REFERENCED BY THESE PATENTS:
Patent Priority Assignee Title
8184974, Sep 11 2006 ANUVU OPERATIONS LLC; ANUVU IP HOLDINGS LLC Fiber-to-the-seat (FTTS) fiber distribution system
8416698, Aug 20 2009 ANUVU OPERATIONS LLC; ANUVU IP HOLDINGS LLC Serial networking fiber optic inflight entertainment system network configuration
8424045, Aug 14 2009 ANUVU OPERATIONS LLC; ANUVU IP HOLDINGS LLC Video display unit docking assembly for fiber-to-the-screen inflight entertainment system
8659990, Aug 06 2009 ANUVU OPERATIONS LLC; ANUVU IP HOLDINGS LLC Serial networking fiber-to-the-seat inflight entertainment system
9036487, Aug 20 2009 ANUVU OPERATIONS LLC; ANUVU IP HOLDINGS LLC Serial networking fiber optic inflight entertainment system network configuration
9118547, Aug 06 2009 ANUVU OPERATIONS LLC; ANUVU IP HOLDINGS LLC Serial networking fiber-to-the-seat inflight entertainment system
9532082, Aug 06 2009 ANUVU OPERATIONS LLC; ANUVU IP HOLDINGS LLC Serial networking fiber-to-the-seat inflight entertainment system
THIS PATENT REFERENCES THESE PATENTS:
Patent Priority Assignee Title
4892273, Dec 30 1988 The United States of America as represented by the Administrator of the Active damping of spacecraft structural appendage vibrations
5427336, Feb 24 1993 Altair Corporation Dual control mechanism for aircraft
6224014, Oct 02 1997 Eurocopter Device for reducing line noise inside a rotary-wing aircraft, especially a helicopter
6467723, Oct 10 2000 Lord Corporation Active vibration control system for helicopter with improved actustor placement
D338186, Jul 30 1991 TEXTRON IPMP L P Enclosure for a helicopter vibration reduction system
D346146, Apr 15 1993 TEXTRON IPMP L P Vibration reduction system
ASSIGNMENT RECORDS    Assignment records on the USPTO
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Executed onAssignorAssigneeConveyanceFrameReelDoc
Aug 17 2004Thales Avionics SA(assignment on the face of the patent)
Aug 17 2004Airbus France(assignment on the face of the patent)
Nov 15 2004GUEGAN, MALOThales Avionics SAASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0160200086 pdf
Nov 15 2004DUFAL, JEROMEThales Avionics SAASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0160200086 pdf
Nov 15 2004GUEGAN, MALOAirbus FranceASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0160200086 pdf
Nov 15 2004DUFAL, JEROMEAirbus FranceASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0160200086 pdf
Nov 17 2004BERTHOU, NICOLASThales Avionics SAASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0160200086 pdf
Nov 17 2004BERTHOU, NICOLASAirbus FranceASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0160200086 pdf
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