Integrated standby instrument system

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An integrated standby instrument system (ISIS) is an electronic aircraft instrument. It is intended to serve as backup in case of a failure of the standard glass cockpit instrumentation, allowing pilots to continue to receive key flight-related information. Prior to the use of ISIS, this was performed by individual redundant mechanical instrumentation instead. Such systems have become common to be installed in various types of aircraft, ranging from airliners to helicopters and smaller general aviation aircraft. While it is common for new-built aircraft to be outfitted with ISIS, numerous operators have opted to have their fleets retrofitted with such apparatus as well.

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An ISIS is designed to combine the functions of separate equivalent mechanical instruments that had previously been included as backup in such cockpits, including altimeter, airspeed indicator, and attitude indicator. Various aspects of ISIS are defined by its function of being a backup to conventional instrumentation. In accordance with this principal, it has been designed to operate with a high level of availability and reliability, as well as being as independent as possible from the aircraft's primary instrumentation and sensors alike. It is commonplace for an ISIS to work in conjunction with provisions for auxiliary power (typically a battery unit), as well as harnessing embedded sensors for its readings wherever possible. [1] [2] When all onboard instrumentation is performing normally, the readings indicated by an ISIS are identical to that of the primary flight display. [3] Advantages presented by ISIS over traditional systems include improved safety, greater ease of operation, and reduced operating costs. [4]

A number of aircraft have been produced with relatively sophisticated integrated standby systems which may include additional functions. For example, the Rockwell Collins Pro Line 21 flight deck, which is fitted to aircraft such as the Cessna Citation XLS+ business jet, features a standby navigation display and engine gauges. [5] [6] Thales Group produce their own ISIS, which is installed on the Airbus A320 narrow-body and Airbus A330 wide-body airliners amongst other aircraft; it allowed for one single instrument to replace four standby instruments that had been traditionally used. [7] [8] Thales also produced an Integrated Electronic Standby Instrument (IESI) dedicated for use on helicopters; in excess of 6,000 such units have reportedly been sold as of July 2020. [9] Another such system is manufactured by L3Harris Technologies, intended for both helicopters and general aviation purposes. [3] [10] Additional companies specialising in avionics, such as GE Aviation, Smiths Group, and Meggitt, have also marketed ranges of standby instrumentation using both standalone and ISIS-compliance principles. [11] [12] [13]

Several companies have produced patentable innovations related to ISIS, including large aerospace players such as Airbus Group. [14] In addition to such technology being adopted upon new-build aircraft, several operators have opted to retrofit their existing aircraft fleets with current generation ISIS, such as UPS's Airbus A300 freighters. [15] Along these lines, Rockwell Collins developed a retrofit package for the Boeing 757 and Boeing 767 that incorporates ISIS. [16] During the 2010s, the cost of performing such cockpit display retrofits reportedly dropped substantially. [17]

See also

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References

  1. ↑ Collinson, R. P. G. (31 December 2002). "Chapter 2.6: Head Down Displays". Introduction to Avionics Systems. Springer. pp. 76–77. ISBN   1402072783 . Retrieved 8 July 2012.
  2. ↑ Chen, Kai., Yan, Jie and Huang, Panfeng (June 2006). "Design of Air Data System of an Aircraft Integrated Electronic Standby Instrument". 2006 International Conference on Mechatronics and Automation. pp. 1147–1151. doi:10.1109/ICMA.2006.257787. ISBN   1-4244-0465-7. S2CID   17045514.{{cite book}}: CS1 maint: multiple names: authors list (link)
  3. 1 2 "ESI-500". l3commercialaviation.com. Retrieved 29 July 2020.
  4. ↑ "Pilot's Guide for the Electronic Standby Instrument System: Model GH-3100" (PDF). silviopini.ch. Retrieved 29 July 2020.
  5. ↑ "Pro Line Fusion®". Rockwell Collins . Retrieved 29 July 2020.
  6. ↑ "Operational Suitability Data (OSD)" (PDF). support.cessna.com. Retrieved 29 July 2020.
  7. ↑ "Integrated Standby Instrument System". a320simulator.be. Retrieved 3 February 2019.
  8. ↑ "Airworthiness Directive: Airbus Industrie A330 Series Aeroplanes" (PDF). services.casa.gov.au. 1998.
  9. ↑ "Integrated Electronic Standby Instrument Fully featured for helicopters - IESI". Thales Group . Retrieved 29 July 2020.
  10. ↑ "L-3 Avionics Intros Glass Standby Instrument For Part 23 Aircraft". aero-news.net. 6 August 2008.
  11. ↑ "Avionics". geaviation.com. Retrieved 29 July 2020.
  12. ↑ "integrated Secondary Flight Display (iSFD)" (PDF). meggitt-avionics.co.uk. Retrieved 29 July 2020.
  13. ↑ "Chinese opt for Smiths instrument standby". Flight International. 19 July 2004.
  14. ↑ "US7415330B2: Aircraft standby display device and system". 2004.
  15. ↑ Bellamy III, Woodrow (16 May 2017). "UPS Brings Epic Avionics to Airbus A300s". aviationtoday.com.
  16. ↑ "767/757 Large Format Display System Flight Deck Retrofit". rockwellcollins.com. Retrieved 29 July 2020.
  17. ↑ "What Pilots Need to Know about Retrofit Avionics". flyingmag.com. Retrieved 4 June 2020.
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