Alan E. LANDMANN

Person

Woodinville, WA, US

People

Patents Grantslast 30 patents

Information Patent Grant
Molybdenum composite hybrid laminates and methods
- Patent number 9,862,175
- Issue date Jan 9, 2018
- The Boeing Company
- Marc R. Matsen
- B29 - WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Information Patent Grant
Methods and systems for determining a structural parameter for nois...
- Patent number 9,805,150
- Issue date Oct 31, 2017
- The Boeing Company
- Alan E. Landmann
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Grant
Molybdenum composite hybrid laminates and methods
- Patent number 9,090,043
- Issue date Jul 28, 2015
- The Boeing Company
- Marc R. Matsen
- B32 - LAYERED PRODUCTS
Information Patent Grant
Flight vehicle fairing having vibration-damping blankets
- Patent number 9,045,216
- Issue date Jun 2, 2015
- The Boeing Company
- Justin Christenson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Structural mode shape alignment
- Patent number 8,882,039
- Issue date Nov 11, 2014
- The Boeing Company
- Alan E Landmann
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Structural mode shape alignment
- Patent number 8,511,609
- Issue date Aug 20, 2013
- The Boeing Company
- Alan E Landmann
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Acoustic pressure load conversion method to vibration spectra
- Patent number 6,363,789
- Issue date Apr 2, 2002
- The Boeing Company
- Mostafa Rassaian
- G01 - MEASURING TESTING

Patents Applicationslast 30 patents

Information Patent Application
METHODS AND SYSTEMS FOR DAMPING A CABIN AIR COMPRESSOR INLET
- Publication number 20160031195
- Publication date Feb 4, 2016
- THE BOEING COMPANY
- Alan E. Landmann
- B32 - LAYERED PRODUCTS
Information Patent Application
METHODS AND SYSTEMS FOR DETERMINING A STRUCTURAL PARAMETER FOR NOIS...
- Publication number 20160034611
- Publication date Feb 4, 2016
- THE BOEING COMPANY
- Alan E. Landmann
- G06 - COMPUTING CALCULATING COUNTING
Information Patent Application
MOLYBDENUM COMPOSITE HYBRID LAMINATES AND METHODS
- Publication number 20150306859
- Publication date Oct 29, 2015
- The Boeing Company
- Marc R. Matsen
- B32 - LAYERED PRODUCTS
Information Patent Application
Flight Vehicle Fairing Having Vibration-Damping Blankets
- Publication number 20140361120
- Publication date Dec 11, 2014
- The Boeing Company
- Justin Christenson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Structural Mode Shape Alignment
- Publication number 20130233644
- Publication date Sep 12, 2013
- The Boeing Company
- Alan E. LANDMANN
- G10 - MUSICAL INSTRUMENTS ACOUSTICS
Information Patent Application
Molybdenum Composite Hybrid Laminates and Methods
- Publication number 20130034705
- Publication date Feb 7, 2013
- THE BOEING COMPANY
- Marc R. Matsen
- B32 - LAYERED PRODUCTS
Information Patent Application
Flight Vehicle Fairing Having Vibration-Damping Blankets
- Publication number 20120325966
- Publication date Dec 27, 2012
- The Boeing Company
- Justin Christenson
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
Structural mode shape alignment
- Publication number 20050253016
- Publication date Nov 17, 2005
- Alan E. Landmann
- G10 - MUSICAL INSTRUMENTS ACOUSTICS

Alan E. LANDMANN

Person

Patents Grantslast 30 patents

Molybdenum composite hybrid laminates and methods

Methods and systems for determining a structural parameter for nois...

Molybdenum composite hybrid laminates and methods

Flight vehicle fairing having vibration-damping blankets

Structural mode shape alignment

Structural mode shape alignment

Acoustic pressure load conversion method to vibration spectra

Patents Applicationslast 30 patents

METHODS AND SYSTEMS FOR DAMPING A CABIN AIR COMPRESSOR INLET

METHODS AND SYSTEMS FOR DETERMINING A STRUCTURAL PARAMETER FOR NOIS...

MOLYBDENUM COMPOSITE HYBRID LAMINATES AND METHODS

Flight Vehicle Fairing Having Vibration-Damping Blankets

Structural Mode Shape Alignment

Molybdenum Composite Hybrid Laminates and Methods

Flight Vehicle Fairing Having Vibration-Damping Blankets

Structural mode shape alignment