RU2011102684A - INTEGRATED RESERVE SYSTEM - Google Patents
INTEGRATED RESERVE SYSTEM Download PDFInfo
- Publication number
- RU2011102684A RU2011102684A RU2011102684/28A RU2011102684A RU2011102684A RU 2011102684 A RU2011102684 A RU 2011102684A RU 2011102684/28 A RU2011102684/28 A RU 2011102684/28A RU 2011102684 A RU2011102684 A RU 2011102684A RU 2011102684 A RU2011102684 A RU 2011102684A
- Authority
- RU
- Russia
- Prior art keywords
- landing
- integrated system
- backup devices
- flight
- entering
- Prior art date
Links
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- Navigation (AREA)
- Devices For Checking Fares Or Tickets At Control Points (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
- Traffic Control Systems (AREA)
Abstract
1. Интегрированная система резервных приборов летательного аппарата (Л.А.), содержащая соединенные последовательно блок датчиков информации, блок обработки информации, блок индикации, отображающий информацию о скорости, высоте, курсе, пространственном положении Л.А., отличающаяся тем, что в нее дополнительно введены устройство для смены кадров в блоке индикации на время полета Л.А. и его посадки и устройство для ввода величины давления в точках взлета и посадки Л.А., соединенные с блоком обработки информации. ! 2. Интегрированная система резервных приборов Л.А. по п.1, отличающаяся тем, что устройство для смены кадров в блоке индикации на время полета Л.А. и его посадки содержит преобразующее устройство, соединенное с первым устройством управления. ! 3. Интегрированная система резервных приборов Л.А. по п.1, отличающаяся тем, что устройство для ввода величины давления в точках взлета и посадки Л.А. содержит преобразователь угла поворота в цифровой код, соединенный со вторым устройством управления, подключенным к коммутирующему устройству. 1. An integrated system of backup devices of the aircraft (L.A.), containing a series of information sensors, an information processing unit, an indication unit that displays information about the speed, altitude, course, spatial position of L.A., characterized in that she additionally introduced a device for changing frames in the display unit for the flight L.A. and its landing and a device for entering the pressure at the take-off and landing points of LA, connected to the information processing unit. ! 2. The integrated system of backup devices L.A. according to claim 1, characterized in that the device for changing frames in the display unit for the flight L.A. and its landing comprises a conversion device connected to the first control device. ! 3. The integrated system of backup devices L.A. according to claim 1, characterized in that the device for entering the pressure at the take-off and landing points L.A. comprises a rotation angle converter into a digital code connected to a second control device connected to the switching device.
Claims (3)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2011102684/28A RU2461800C1 (en) | 2011-01-24 | 2011-01-24 | Integrated system of backup devices |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2011102684/28A RU2461800C1 (en) | 2011-01-24 | 2011-01-24 | Integrated system of backup devices |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2011102684A true RU2011102684A (en) | 2012-07-27 |
RU2461800C1 RU2461800C1 (en) | 2012-09-20 |
Family
ID=46850419
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2011102684/28A RU2461800C1 (en) | 2011-01-24 | 2011-01-24 | Integrated system of backup devices |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2461800C1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2541727C2 (en) * | 2013-02-12 | 2015-02-20 | Открытое акционерное общество Арзамасское научно-производственное предприятие "ТЕМП-АВИА" (ОАО АНПП "ТЕМП-АВИА") | Method of installing backup altitude controller of navigation system on aircraft instrument panel |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2784457B1 (en) * | 1998-10-13 | 2001-01-05 | Sextant Avionique | COMBINED EMERGENCY INSTRUMENTS FOR AIRCRAFT |
RU2184683C1 (en) * | 2001-12-20 | 2002-07-10 | Акционерное общество открытого типа "ОКБ Сухого" | Multi-functional two-seat highly-maneuverable tactical-purpose aircraft |
RU2219108C1 (en) * | 2002-11-11 | 2003-12-20 | ОАО "ОКБ им. А.С. Яковлева" | Complex electronic display system for light multi- purpose aircraft |
FR2873989B1 (en) * | 2004-08-09 | 2006-11-17 | Airbus France Sas | DEVICE FOR DISPLAYING EMERGENCY RESPONSE OF AN AIRCRAFT |
-
2011
- 2011-01-24 RU RU2011102684/28A patent/RU2461800C1/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
RU2461800C1 (en) | 2012-09-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20160125 |