VORflash

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By: ekbert007 (14 month(s) ago)

Dear Sir , Can you please share your ppt via mail..My mail:ekbert007@yahoo.com thanks n regrds Bertin

By: shagutin (28 month(s) ago)

dear sir, i m a aviation instructor and want to use your VOR presentaion in teaching my students. can u please mail me a copy of this on my email id 'shashwat.shagutin@gmail.com' . regards shashwat.

By: llovres (32 month(s) ago)

HI, I have to teach my students regarding VOR theory. Would u share ur ppt via email. My mail: llovres@gmail.com

By: skmanocha (32 month(s) ago)

Dear Fello Instructor, Thanks for your interest. I am inviting you to join my Yahoo Group to download the presentation. You will have to log in with Yahoo ID. Best wishes, manocha

 

By: sharm44 (35 month(s) ago)

Hi there, i am navy pilot...I found that ur ppt is very sound and knowledegable. Simple and easy to understand the whole chapter of a VOR. I have to teach my junior pilots regarding VOR theory. Would u share ur ppt via email. Ur cooperation is very much appreciated. my email : mdsharm@yahoo.com

By: skmanocha (34 month(s) ago)

Dear Instructor, I had invited you to join Yahoo Group to download the presentation, when I received your request. It was as you already have Yahoo ID. I am trying to send a copy on your Email ID. Hope it will be received and helpful. Best wishes, manocha

 

By: amrs (36 month(s) ago)

i am avionics instructor it will be very kind of you to send this unvaluable presentation to me at amr_sayed_av@yahoo.com

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Presentation Transcript

Slide 1: 

VOR Very High Frequency Omni Radio Range

Slide 2: 

Bearing by Phase Comparison Ground VHF Transmitter and Airborne Receiver Unit Night Effect and Static Interference (NDB/ ADF) NOT Present BASIC PRINCIPLE Of Operation Continuous Magnetic Bearing Indication Short Range Navigational Aid

Slide 3: 

† 30 Hz FM Cw 108 to 117.95 MHz Sub Carrier 9960 Hz AM Phase of 30 Hz FM Signal is SAME at A,B,C and D At any INSTANT PRINCIPLE OF OPERATION

Slide 4: 

† Amplitude Modulated “Figure of 8” Transmission Combined Result is LIMACON Differs from Cardiod Polar Diagram of Loop Aerial at Minimum Combination of Omni Signal with Figure of Eight Directional Transmission

Slide 5: 

Directional Transmission Rotation through 90°: Clock-wise

Slide 6: 

LIMACON Rotates 90° Clock-wise

Slide 7: 

Clock-wise Rotation by Further 90°

Slide 8: 

LIMACON Rotates another 90° Clock-wise

Slide 9: 

Directional Aerial Rotation through360° Clock-wise results in Limacon rotation through same angle simultaneously. Effect of Limacon Rotation on Signal Reception at A, B, C and D

Slide 10: 

Effect of Limacon Rotation on Signal Reception at A, B, C and D

Slide 11: 

Amplitude Modulated Signal Reception at A, B, C and D after 180° Limacon Rotation

Slide 12: 

Amplitude Modulated Signal Reception at A, B, C and D after 270° Rotation

Slide 13: 

PHASE DIAGRAMS of AM Directional Signal Reception at A, B, C and D after Two Rotations Phase of Received Signal is Different at A,B,C and D

Slide 14: 

PHASE COMPARISON of AM and FM Signal Receptions at A, B, C and D Variable Signal Reference Signal Phase Diff = 0° Phase Diff = 90° Phase Diff = 180° Phase Diff = 270°

Slide 15: 

Station Identification: Keyed AM audio frequency Every Ten Seconds Three Characters in Morse code Voice Transmission: Weather, AFIS Cone of Confusion: 40°

Slide 16: 

GROUND EQUIPMENT: Transmitter and Aerial

Slide 17: 

Transmitter Switched Off/ No Ident : Bearing Wrong by More Than 1° Reduced Signal Strength (15% below Normal) Failure of Monitor STANDBY TRANSMITTER: GROUND EQUIPMENT: MONITORING

Slide 18: 

Aerial and Receiver Unit Control Unit RMI [Radio Magnetic Indicator] AIRBORNE EQUIPMENT: Indicators: OBS [Omni Bearing Selector] OBI {Omni Bearing Indicator} and CDI {Course Deviation Indicator}

Slide 19: 

Aerials AIRBORNE EQUIPMENT:

Slide 20: 

Receiver Unit AIRBORNE EQUIPMENT:

Slide 21: 

AIRBORNE EQUIPMENT: Control Units

Slide 22: 

Omni Bearing Selector (OBS) and OBI AIRBORNE EQUIPMENT: Indicators To - From Indicator Course Deviation Indicator (CDI) Full Scale Deflection ± 10° Each Dot = 2.0 ° On FOUR DOT Indicator Each Dot = 2.5 °

Slide 23: 

Warning Flag No/ Low Power to a/c Equipment Failure of a/c Equipment Failure of Ground Equipment May appear during Turns and Tuning Failure of Indicator Weak Reference or Variable Signal Characteristics VHF 108.00 to 117.97 MHz Only even first decimals up to 111.79 MHz Emission: A9W

Slide 24: 

AIRBORNE EQUIPMENT: Indicators (RMI)

Slide 25: 

Range Line of Sight Designated Operational Coverage Protected Range and Altitude Protected Range and Altitude

Slide 26: 

HIGH ALTITUDE LOW ALTITUDE TERMINAL VOR 1,000 ft + 40 nm 14,500 ft 1,000 ft + 40 nm 1,000 ft + 25 nm 18,000 ft 12,000 ft Designated Operational Coverage Not to Scale

Slide 27: 

Factors Affecting Range Transmitter Power Station Elevation and Aircraft Altitude D - Range (Nm), Ht - Transmitter Elevation (Ft) Ha - Aircraft Altitude (Ft) Accuracy (95% of occasions) Transmitter Signal ± 3° Overall ± 5°

Slide 28: 

Factors Affecting Accuracy Beam Alignment Site Error : less than ± 1° Propagation Error Airborne Equipment Error Pilotage Error Use and Interpretation Position Line Homing Tracking In/ Out on Radial Aggregate Error: Propagation and Equipment Error Combined

Slide 30: 

HOMING

Slide 33: 

Tracking in on Required Radial 220° CDI Bar central Maintain A/c Hdg 040 ± Drift to track in on Required Radial OBS Selected 040° To-From TO

Slide 34: 

VOR QDM 040 RADIAL 220

Slide 35: 

OTHER DISPLAYS Rnav (AREA NAVIGATION) HSI ( Horizontal Situation Indicator)

Slide 36: 

DOPPLER VOR Difficult Sites - Site Error > ± 1° Principle of Operation: 52 Antennas tx 30 times/ sec Accuracy: Compatible at Difficult Sites Rotating (Variable) Signal FM Anti- clockwise Rotation: Standard Airborne Equipment

Slide 37: 

VOT Test VOR : Ground check of aircraft equipment 000 FROM or 180 TO within ± 4° 000 zerO frOm 180 eighT To BOTH, REFERENCE AND VARIABLE SIGNALS IN PHASE IN ALL DIRECTIONS

Slide 38: 

SERVICEABILITY CHECK AT R/W HOLDING POINT