Title: EMBRAER VISION FOR IFE SYSTEMS
1EMBRAER VISION FORIFE SYSTEMS
- Aristides Cintra
- aristides.cintra_at_embraer.com.br
2EMBRAER Vision
- The several IFE technologies are becoming more
and more complex and it was EMBRAER decision to
offer the IFE system development and
certification as part of the aircraft basic
configuration.
3Why preference for Line-Fit?
- Embraer believes the line-fit solution is most
effective and elegant way to install IFE - All processes adopted are within Embraer
standards making easier the integration with
suppliers and system interfaces - System Installation is part of the aircraft
manufacturing, schedules, testing and planning - Based on experience gained with IFE systems
installation, Embraer can significantly reduce
the implementation time of an IFE Line-Fit program
4IFE System Design Phases
- Customer requirements
- LOPA definition
- System Development
- System Installation
- System Tests
- System Certification
- Entry in Service
5Customer Requirements and Wish List
- Audio
- AOD
- Satellite Radio
- PRA
- Video
- VOD
- Satellite TV
- Digital Broadcast
- Communications
- SATCOM
- Wireless Phone
- Cellular
- Wireless Internet Access
- SMS
- VoIP
6How to design the aircraft harnesses?
How will be the interface with seats and
monuments?
How to provide proper cooling to the equipment?
Human factors requirements
Where to install the LRUs?
Where to install the systems controls?
7LOPA Definition
CABIN HARNESSES
VIDEO MONITOR
SEAT BOXES
LRU RACK
8E-Jets
9System Development Strengths
AC
- All harnesses integrated with the aircraft basic
harnesses
DC
MISC
FBW
10System Development Strengths
- Electrical power supply and control logic defined
with the electrical system/avionics suppliers
INPUTS FROM AIRCRAFT
EPGS
IFE SYSTEM
LOGIC
AVIONICS
INPUTS FROM AIRCRAFT
11Strengths of the development
- Dedicated Avionics data bus interface
- Electrical/Structural hardware are the same
specified for the whole airplane - Interface with systems and interior under Embraer
standards - All provisions certified as part of the basic
aircraft certification
12Thinking about space and harnesses installation
- Comply with segregation, voltage drop, type of
wiring, interface with other essential systems
(electrical, avionics, AMS, etc)
13Thinking about space and harnesses installation
- Comply with weight and balance requirements to
locate LRUs - Comply with customer requirements for spacious
and comfortable cabin
14Concept
15CATIA model
- All models are created in CATIA, minimizing
installation errors (lengths, structural
supports, etc)
16Actual Wiring Installation
CATIA Model
17Seats
- Integration, design and try-out to reach
perfection
18Study for Monitor Installation
19Satellite TV antenna design
?
HOISTING POINTS
RADOME
?
?
SKIRT
ADAPTER
20From manufacturing to Results
ADAPTER PLATE
SKIRT
ANTENNA
RADOME
21Seats Interface
22Rack Design
- Rack design should consider
- Accessibility, Maintainability
- Light weight, Small size
23HSD / WIRELESS
- Embraer has developed a HSD and Wireless Internet
access system - Challenges
- to have the same performance as encountered at
home - Costs for the passengers and airlines should be
kept low
24HSD System Architecture
VoIP
MPDS
ISDN
PC Network
25Coverage Map
26Phased-Array Beam type Antenna
- No aerodynamics, ice or interference problems
27PC Power Outlets
- A solution for Business/First Class seats
28PC Power Outlets
- A solution for Economy Class seats
29115/220 VAC Outlets
- Customers are requesting outlets for other
applications and different standards
30System Certification
- Although the majority of the IFE Systems are
optional, the certification must comply with
RBHA/FAA/EASA and other authorities requirements.
- Authorities are concerned about functionalities
and integration with essential aircraft systems.
31Entry in Service
- The airlines are getting excited with the new IFE
systems and new technologies. - The passengers are changing their habits giving
preference to fly with the airlines that offer
more options of services. - Statistically, the tickets sales are increasing
10 due to the IFE systems implementation.
32RESULTS
33Lineage 1000
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