WE INNOVATE FOR THOSE WHO MOVE THE WORLD

BAE Systems Controls Inc.

Application Filed: 2015-07-30

Trademark Application Details

Status

602

Dead/Abandoned

ABANDONED-FAILURE TO RESPOND OR LATE RESPONSE

Research	OneLook Acronym Finder
Serial Number	86709383
Mark Drawing Code	4000: Illustration: Drawing with word(s)/letter(s)/number(s) in Block form
Attorney Name	Scott J. Asmus
Attorney Docket Number	BAET-1334
Law Office Assigned	L20
Employee Name	GARTNER, JOHN M

Timeline

2015-07-30	Application Filed
2016-05-24	Abandon
2016-06-24	Location: TMEG LAW OFFICE 102 - EXAMINING ATTORNEY ASSIGNED
2016-06-24	Status: Dead/Abandoned
2018-07-08	Transaction Date

Trademark Applicants & Owners

Owner:	BAE Systems Controls Inc.
Address	1098 Clark St Endicott DE 13760
Legal Entity Type	Corporation
Legal Entity State	DE

Documents

Click the blue "Refresh" button to load certificates, specimines, application, and other documents.

Attorney of Record

Scott J. Asmus
NHQ1-719
PO Box 868
Nashua NH 03061-0868

Good, Services, and Codes

International Codes:	9
U.S. Codes:	021,023,026,036,038

Type Code	Type
GS0091	Flight control electronics for commercial aircraft, namely, primary flight control computers consisting of electronic modules for system power conditioning and battery backup, flight surface actuator control, autoflight and autoland modules for primary and high lift flight controls, inertial rate and air data sensors for flight data input, and containing flight critical software for overall system control of aircraft flight surfaces; actuator control electronics consisting of power supplies and programmable logic electronic control modules, under command of the primary or high-lift flight control computers, to provide power and positional inputs to electric, hydraulic, or pneumatic actuators for the control of various aircraft flight surfaces; high-lift control and monitoring electronics consisting of electronic control modules to provide positional inputs to electric, hydraulic, or pneumatic actuators controlling wing flaps and slats to increase lift for aircraft control; rudder and yaw control electronics consisting of electronic control modules to provide positional inputs to electric, hydraulic, or pneumatic actuators controlling directional (yaw) stability for aircraft control; stabilizer control and monitoring electronics consisting of electronic control modules to provide positional inputs to electric, hydraulic, or pneumatic actuators controlling the horizontal and/or vertical stabilizers that provide longitudinal stability and control (pitch) and/or directional (yaw) stability and control of an aircraft; spoiler-control and monitoring electronics consisting of electronic control modules to provide positional inputs to electric, hydraulic, or pneumatic actuators controlling the spoiler control surfaces on an aircraft used to disrupt airflow over the wing and greatly reduce lift; engine controls for commercial aircraft, namely, full authority digital engine controls consisting of electronic modules for system power, computational controls, input and output interface modules, and lightning/EMI protection to control multiple data input variables of the current flight condition including air density, throttle lever position, engine temperatures, and engine pressures; engine health and prognostics systems consisting of electronic modules for system power, computational controls, input and output interface modules to receive data from various aircraft engine sensors strategically positioned throughout the engine to record key technical parameters several times each flight

Type Code

Type

GS0091

Flight control electronics for commercial aircraft, namely, primary flight control computers consisting of electronic modules for system power conditioning and battery backup, flight surface actuator control, autoflight and autoland modules for primary and high lift flight controls, inertial rate and air data sensors for flight data input, and containing flight critical software for overall system control of aircraft flight surfaces; actuator control electronics consisting of power supplies and programmable logic electronic control modules, under command of the primary or high-lift flight control computers, to provide power and positional inputs to electric, hydraulic, or pneumatic actuators for the control of various aircraft flight surfaces; high-lift control and monitoring electronics consisting of electronic control modules to provide positional inputs to electric, hydraulic, or pneumatic actuators controlling wing flaps and slats to increase lift for aircraft control; rudder and yaw control electronics consisting of electronic control modules to provide positional inputs to electric, hydraulic, or pneumatic actuators controlling directional (yaw) stability for aircraft control; stabilizer control and monitoring electronics consisting of electronic control modules to provide positional inputs to electric, hydraulic, or pneumatic actuators controlling the horizontal and/or vertical stabilizers that provide longitudinal stability and control (pitch) and/or directional (yaw) stability and control of an aircraft; spoiler-control and monitoring electronics consisting of electronic control modules to provide positional inputs to electric, hydraulic, or pneumatic actuators controlling the spoiler control surfaces on an aircraft used to disrupt airflow over the wing and greatly reduce lift; engine controls for commercial aircraft, namely, full authority digital engine controls consisting of electronic modules for system power, computational controls, input and output interface modules, and lightning/EMI protection to control multiple data input variables of the current flight condition including air density, throttle lever position, engine temperatures, and engine pressures; engine health and prognostics systems consisting of electronic modules for system power, computational controls, input and output interface modules to receive data from various aircraft engine sensors strategically positioned throughout the engine to record key technical parameters several times each flight

Trademark Filing History

Description	Date	Event Coding
NEW APPLICATION ENTERED IN TRAM	2015-08-03	1 NWAP I:Incoming Correspondence
NEW APPLICATION OFFICE SUPPLIED DATA ENTERED IN TRAM	2015-08-04	2 NWOS I:Incoming Correspondence
TEAS REVOKE/APP/CHANGE ADDR OF ATTY/DOM REP RECEIVED	2015-10-26	3 REAP I:Incoming Correspondence
ATTORNEY/DOM.REP.REVOKED AND/OR APPOINTED	2015-10-26	4 ARAA I:Incoming Correspondence
ASSIGNED TO EXAMINER	2015-11-11	5 DOCK D:Assigned to Examiner
NON-FINAL ACTION WRITTEN	2015-11-23	6 CNRT R:Renewal
NON-FINAL ACTION E-MAILED	2015-11-23	7 GNRT F:First Action
NOTIFICATION OF NON-FINAL ACTION E-MAILED	2015-11-23	8 GNRN O:Outgoing Correspondence
TEAS REVOKE/APP/CHANGE ADDR OF ATTY/DOM REP RECEIVED	2016-05-12	9 REAP I:Incoming Correspondence
ATTORNEY/DOM.REP.REVOKED AND/OR APPOINTED	2016-05-12	10 ARAA I:Incoming Correspondence
ABANDONMENT - FAILURE TO RESPOND OR LATE RESPONSE	2016-06-24	11 ABN2 O:Outgoing Correspondence
ABANDONMENT NOTICE MAILED - FAILURE TO RESPOND	2016-06-24	12 MAB2 O:Outgoing Correspondence

Similar Marks

Mark Image Registration \| Serial	Company Trademark Application Date
WE INNOVATE FOR THOSE WHO MOVE THE WORLD 86709383 not registered Dead/Abandoned	BAE Systems Controls Inc. 2015-07-30
WE INNOVATE FOR THOSE WHO MOVE THE WORLD 85913464 not registered Dead/Abandoned	BAE Systems Controls Inc. 2013-04-24

uspto.report is an independent third-party trademark research tool that is not affiliated, endorsed, or sponsored by the United States Patent and Trademark Office (USPTO) or any other governmental organization. The information provided by uspto.report is based on publicly available data at the time of writing and is intended for informational purposes only.

While we strive to provide accurate and up-to-date information, we do not guarantee the accuracy, completeness, reliability, or suitability of the information displayed on this site. The use of this site is at your own risk. Any reliance you place on such information is therefore strictly at your own risk.

All official trademark data, including owner information, should be verified by visiting the official USPTO website at www.uspto.gov. This site is not intended to replace professional legal advice and should not be used as a substitute for consulting with a legal professional who is knowledgeable about trademark law.