Peter JONES

Person

Erie, PA, US

People

Patents Grantslast 30 patents

Information Patent Grant
Lead-lag dampers and assemblies for an articulated rotor and method...
- Patent number 11,091,255
- Issue date Aug 17, 2021
- Lord Corporation
- Peter Jones
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Rotary wing aircraft rotary lead lag damper
- Patent number 8,356,977
- Issue date Jan 22, 2013
- Lord Corporation
- Peter J. Jones
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Helicopter aircraft vehicle rotor damper
- Patent number 8,167,561
- Issue date May 1, 2012
- Lord Corporation
- Peter Jones
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Fluid-elastomeric damper assembly including internal pumping mechanism
- Patent number 7,931,258
- Issue date Apr 26, 2011
- Lord Corporation
- Donald Russell
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Fluid-elastomeric damper assembly including internal pumping mechanism
- Patent number 7,137,624
- Issue date Nov 21, 2006
- Lord Corporation
- Donald Russell
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Flexbeam damper assembly having transition shim clamp device
- Patent number 6,827,553
- Issue date Dec 7, 2004
- Lord Corporation
- Peter J. Jones
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Fluid damper including flexible damping plate
- Patent number 6,045,328
- Issue date Apr 4, 2000
- Lord Corporation
- Peter J. Jones
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Active fluid mounting
- Patent number 5,957,440
- Issue date Sep 28, 1999
- Lord Corporation
- Peter J. Jones
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Fluid-filled active vibration absorber
- Patent number 5,947,457
- Issue date Sep 7, 1999
- Lord Corporation
- Douglas A. Swanson
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Method and apparatus for reducing transient motion between an aircr...
- Patent number 5,788,372
- Issue date Aug 4, 1998
- Lord Corporation
- Peter J. Jones
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Flexible composite coupling
- Patent number 5,551,918
- Issue date Sep 3, 1996
- Lawrie Technology Incorporated
- Peter J. Jones
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Grant
Adaptive fluid mount
- Patent number 5,197,692
- Issue date Mar 30, 1993
- Lord Corporation
- Peter J. Jones
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Fluid mount with active vibration control
- Patent number 5,174,552
- Issue date Dec 29, 1992
- Lord Corporation
- Douglas A. Hodgson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Volume compensated fluid mount
- Patent number 4,811,919
- Issue date Mar 14, 1989
- Lord Corporation
- Peter J. Jones
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
HIGH DEGREE OF FREEDOM RISER TENSIONER SYSTEM
- Publication number 20190178040
- Publication date Jun 13, 2019
- LORD CORPORATION
- Peter JONES
- E21 - EARTH DRILLING MINING
Information Patent Application
GIMBAL SYSTEM
- Publication number 20190009866
- Publication date Jan 10, 2019
- LORD CORPORATION
- Peter JONES
- B63 - SHIPS OR OTHER WATERBORNE VESSELS RELATED EQUIPMENT
Information Patent Application
LEAD-LAG DAMPERS AND ASSEMBLIES FOR AN ARTICULATED ROTOR AND METHOD...
- Publication number 20170081024
- Publication date Mar 23, 2017
- LORD CORPORATION
- Peter JONES
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FLUID-ELASTOMERIC DAMPER ASSEMBLY INCLUDING INTERNAL PUMPING MECHANISM
- Publication number 20110193275
- Publication date Aug 11, 2011
- Donald Russell
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
HELICOPTER AIRCRAFT VEHICLE ROTOR DAMPER
- Publication number 20090110555
- Publication date Apr 30, 2009
- PETER JONES
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FLUID-ELASTOMERIC DAMPER ASSEMBLY INCLUDING INTERNAL PUMPING MECHANISM
- Publication number 20080143028
- Publication date Jun 19, 2008
- Donald Russell
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
ROTARY WING AIRCRAFT ROTARY LEAD LAG DAMPER
- Publication number 20080069695
- Publication date Mar 20, 2008
- Peter J. Jones
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Fluid-elastomeric damper assembly including internal pumping mechanism
- Publication number 20040145102
- Publication date Jul 29, 2004
- Donald Russell
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
FLEXBEAM DAMPER ASSEMBLY HAVING TRANSITION SHIM CLAMP DEVICE
- Publication number 20040136829
- Publication date Jul 15, 2004
- Peter J. Jones
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Peter JONES

Person

Patents Grantslast 30 patents

Lead-lag dampers and assemblies for an articulated rotor and method...

Rotary wing aircraft rotary lead lag damper

Helicopter aircraft vehicle rotor damper

Fluid-elastomeric damper assembly including internal pumping mechanism

Fluid-elastomeric damper assembly including internal pumping mechanism

Flexbeam damper assembly having transition shim clamp device

Fluid damper including flexible damping plate

Active fluid mounting

Fluid-filled active vibration absorber

Method and apparatus for reducing transient motion between an aircr...

Flexible composite coupling

Adaptive fluid mount

Fluid mount with active vibration control

Volume compensated fluid mount

Patents Applicationslast 30 patents

HIGH DEGREE OF FREEDOM RISER TENSIONER SYSTEM

GIMBAL SYSTEM

LEAD-LAG DAMPERS AND ASSEMBLIES FOR AN ARTICULATED ROTOR AND METHOD...

FLUID-ELASTOMERIC DAMPER ASSEMBLY INCLUDING INTERNAL PUMPING MECHANISM

HELICOPTER AIRCRAFT VEHICLE ROTOR DAMPER

FLUID-ELASTOMERIC DAMPER ASSEMBLY INCLUDING INTERNAL PUMPING MECHANISM

ROTARY WING AIRCRAFT ROTARY LEAD LAG DAMPER

Fluid-elastomeric damper assembly including internal pumping mechanism

FLEXBEAM DAMPER ASSEMBLY HAVING TRANSITION SHIM CLAMP DEVICE