Thomas Childs

Person

Bristol, GB

People

Patents Grantslast 30 patents

Information Patent Grant
Annular member, method, and assembly for component displacement con...
- Patent number 11,005,334
- Issue date May 11, 2021
- Saint-Gobain Performance Plastics Rencol Limited
- Thomas Childs
- B62 - LAND VEHICLES FOR TRAVELLING OTHERWISE THAN ON RAILS
Information Patent Grant
Cover panel for an aircraft wing and a method of forming thereof
- Patent number 8,267,353
- Issue date Sep 18, 2012
- Airbus Operations Limited
- Thomas Childs
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Stringer for an aircraft wing and a method of forming thereof
- Patent number 8,091,830
- Issue date Jan 10, 2012
- Airbus Operations Limited
- Thomas Childs
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Stringer for an aircraft wing and a method of forming thereof
- Patent number 8,087,614
- Issue date Jan 3, 2012
- Airbus Operations Limited
- Thomas Childs
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Grant
Stringer for an aircraft wing and a method of reinforcing thereof
- Patent number 7,677,496
- Issue date Mar 16, 2010
- Airbus Operations Limited
- Thomas Childs
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Patents Applicationslast 30 patents

Information Patent Application
TOLERANCE RING WITH MODIFIED SURFACE PROPERTIES
- Publication number 20230213051
- Publication date Jul 6, 2023
- SAINT-GOBAIN PERFORMANCE PLASTICS RENCOL LIMITED
- Alejandro PENA
- B05 - SPRAYING OR ATOMISING IN GENERAL APPLYING LIQUIDS OR OTHER FLUENT MATER...
Information Patent Application
TOLERANCE RING FOR DRIVE MOTOR STATOR
- Publication number 20230055134
- Publication date Feb 23, 2023
- Saint-Gobain Performance Plastics Rencol Limited
- Thomas CHILDS
- H02 - GENERATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
Information Patent Application
TOLERANCE RING, ASSEMBLY, AND METHOD OF MAKING AND USING THE SAME
- Publication number 20220106986
- Publication date Apr 7, 2022
- Saint-Gobain Performance Plastics Rencol Limited
- Thomas CHILDS
- F16 - ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINT...
Information Patent Application
ANNULAR MEMBER, METHOD, AND ASSEMBLY FOR COMPONENT DISPLACEMENT CON...
- Publication number 20190190345
- Publication date Jun 20, 2019
- Saint-Gobain Performance Plastics Rencol Limited
- Thomas CHILDS
- B32 - LAYERED PRODUCTS
Information Patent Application
STRINGER FOR AN AIRCRAFT WING AND A METHOD OF FORMING THEREOF
- Publication number 20100230542
- Publication date Sep 16, 2010
- AIRBUS UK Limited
- Thomas CHILDS
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
STRINGER FOR AN AIRCRAFT WING AND A METHOD OF FORMING THEREOF
- Publication number 20090194636
- Publication date Aug 6, 2009
- AIRBUS UK Limited
- Thomas CHILDS
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
STRINGER FOR AN AIRCRAFT WING AND A METHOD OF REINFORCING THEREOF
- Publication number 20080105786
- Publication date May 8, 2008
- AIRBUS UK Limited
- Thomas CHILDS
- B64 - AIRCRAFT AVIATION COSMONAUTICS
Information Patent Application
COVER PANEL FOR AN AIRCRAFT WING AND A METHOD OF FORMING THEREOF
- Publication number 20080042011
- Publication date Feb 21, 2008
- AIRBUS UK Limited
- Thomas CHILDS
- B64 - AIRCRAFT AVIATION COSMONAUTICS

Thomas Childs

Person

Patents Grantslast 30 patents

Annular member, method, and assembly for component displacement con...

Cover panel for an aircraft wing and a method of forming thereof

Stringer for an aircraft wing and a method of forming thereof

Stringer for an aircraft wing and a method of forming thereof

Stringer for an aircraft wing and a method of reinforcing thereof

Patents Applicationslast 30 patents

TOLERANCE RING WITH MODIFIED SURFACE PROPERTIES

TOLERANCE RING FOR DRIVE MOTOR STATOR

TOLERANCE RING, ASSEMBLY, AND METHOD OF MAKING AND USING THE SAME

ANNULAR MEMBER, METHOD, AND ASSEMBLY FOR COMPONENT DISPLACEMENT CON...

STRINGER FOR AN AIRCRAFT WING AND A METHOD OF FORMING THEREOF

STRINGER FOR AN AIRCRAFT WING AND A METHOD OF FORMING THEREOF

STRINGER FOR AN AIRCRAFT WING AND A METHOD OF REINFORCING THEREOF

COVER PANEL FOR AN AIRCRAFT WING AND A METHOD OF FORMING THEREOF