DE934144C - Blind landing procedure for fired approach lines and runways - Google Patents
Blind landing procedure for fired approach lines and runwaysInfo
- Publication number
- DE934144C DE934144C DEL16864A DEL0016864A DE934144C DE 934144 C DE934144 C DE 934144C DE L16864 A DEL16864 A DE L16864A DE L0016864 A DEL0016864 A DE L0016864A DE 934144 C DE934144 C DE 934144C
- Authority
- DE
- Germany
- Prior art keywords
- runways
- landing procedure
- blind landing
- approach lines
- fired
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/18—Visual or acoustic landing aids
- B64F1/20—Arrangement of optical beacons
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Traffic Control Systems (AREA)
- Road Paving Structures (AREA)
Description
Blindlandeverfahren bei befeuerten Anfluglinien und Startbahnen Gegenstand des Patents 924 252 ist ein Blindlandeverfahren bei befeuerten Anfluglinien und Startbahnen, bei dem unsichtbares Licht, vorzugsweise infrarotes Licht, für die Befeuerung der Anfluglinien in Startbahnen verwendet wird und das Bild der Befeuerung mittels eines an sich bekannten elektronischen Bildwandlers dem Piloten sichtbar gemacht wird.Blind landing procedure for fired approach lines and runways subject of patent 924 252 is a blind landing procedure for fired approach lines and Runways in which invisible light, preferably infrared light, for the Lighting of the approach lines in runways is used and the image of the lighting visible to the pilot by means of an electronic image converter known per se is made.
Nach Anspruch 2 des Hauptpatents soll auf dem Bildschirm des Biwa-Rohres ein Fadenkreuz vorgesehen sein, das nach den Achsen des Flugzeuges ausgerichtet ist. Durch dieses Fadenkreuz ist es möglich, ohne weitere Instrumente die Lage des Flugzeuges in der horizontalen Ebene, bezogen auf die gleiche Ebene der Landebahn, und die richtige Richtung auf der Landebahn durch Mittehaltung des Senkrechtstriches zwischen den auf dem Bildschirm abgebildeten Leuchtpunkten zu erkennen.According to claim 2 of the main patent should be on the screen of the Biwa pipe a crosshair can be provided which is aligned with the axes of the aircraft is. With this crosshair it is possible to determine the position of the Aircraft in the horizontal plane, related to the same plane of the runway, and the right direction on the runway by keeping the vertical line in the middle between the luminous dots shown on the screen.
Nach der Erfindung ist dieses Fadenkreuz mit zwei parallelen Horizont4lfäden versehen, deren Abstand je nach Typ des Flugzeuges so geeicht ist, daB sich zwischen den beiden Horizontalfäden stets eine bestimmte Anzahl von Leuchten beim Aufsetzen abbildet. Da der Abstand der Startbahnleuchten untereinander gleich und international festgelegt, also auf allen Flughäfen gleich ist, bleibt die Zahl der abgebildeten Leuchten zwischen den geeichten Horizontalfäden stets gleich. Hierdurch ist dem Piloten eine unfehlbare; einfach -ablesbare Hilfe beim Abfangen des Flugzeuges gegeben:" Es hat sich nun als vorteilhaft erwiesen, die Marlcierung zwischen den beiden Horizontalfäden durch lichtempfindliche Zellen abzutasten und diese Abtastung gegebenenfalls über Verstärker zur Beeinflussung der Selbststeuerung so zu verwenden, daß das Flugzeug sich automatisch selbst abfängt. .According to the invention, this crosshair is with two parallel horizontal threads provided, the distance between which is calibrated, depending on the type of aircraft, that between the two horizontal threads always a certain number of lights when putting on maps. Because the distance between the runway lights is the same and international fixed, i.e. the same at all airports, the number of those shown remains Always glow the same between the calibrated horizontal threads. Through this is an infallible to the pilot; easy-to-read help when intercepting the aircraft given: "It has now proven to be advantageous to march between the to scan both horizontal threads through light-sensitive cells and this scan if necessary to be used via amplifiers to influence the self-control in such a way that that the aircraft automatically intercepts itself. .
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEL16864A DE934144C (en) | 1953-10-16 | 1953-10-16 | Blind landing procedure for fired approach lines and runways |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEL16864A DE934144C (en) | 1953-10-16 | 1953-10-16 | Blind landing procedure for fired approach lines and runways |
Publications (1)
Publication Number | Publication Date |
---|---|
DE934144C true DE934144C (en) | 1955-10-13 |
Family
ID=7260561
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DEL16864A Expired DE934144C (en) | 1953-10-16 | 1953-10-16 | Blind landing procedure for fired approach lines and runways |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE934144C (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2546471A1 (en) * | 1974-10-22 | 1976-05-06 | Nikolai Gennadievitsch Basov | TAKE-OFF AND LANDING SYSTEM FOR AIRCRAFT AND A CORRESPONDING TAKE-OFF AND LANDING PROCEDURE |
-
1953
- 1953-10-16 DE DEL16864A patent/DE934144C/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2546471A1 (en) * | 1974-10-22 | 1976-05-06 | Nikolai Gennadievitsch Basov | TAKE-OFF AND LANDING SYSTEM FOR AIRCRAFT AND A CORRESPONDING TAKE-OFF AND LANDING PROCEDURE |
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