GB865596A - Safe landing of aircraft - Google Patents
Safe landing of aircraftInfo
- Publication number
- GB865596A GB865596A GB13416/57A GB1341657A GB865596A GB 865596 A GB865596 A GB 865596A GB 13416/57 A GB13416/57 A GB 13416/57A GB 1341657 A GB1341657 A GB 1341657A GB 865596 A GB865596 A GB 865596A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- photo
- infra
- altitude
- april
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Acoustics & Sound (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Traffic Control Systems (AREA)
Abstract
865,596. Photo-electric aircraft guidance. BRAGA, M. A. P. DE A. April 26, 1957 [April 26, 1956], No. 13416/57. Class 40(3) Apparatus for facilitating the landing of aircraft comprises firstly an infra-red beacon on the runway and a photo-electric device on the aircraft which can be adjusted manually to assist in locating the line of descent, and secondly a mast on the runway carrying a series of vertically spaced infra-red lamps each modulated at a different frequency by shutters and a photoelectric cell on the aircraft which in combination with a frequency meter indicates the altitude of the aircraft. The photo-electric device for indicating line of descent comprises four photocells e and a concave mirror d axially movable within a tube c to maintain alignment between aircraft and beacon. The infra-red lamps of the altitude indication system may each be modulated in accordance with signals from a tape which are translated in the aircraft into audible statements of altitude.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PT865596X | 1956-04-26 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB865596A true GB865596A (en) | 1961-04-19 |
Family
ID=20084146
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB13416/57A Expired GB865596A (en) | 1956-04-26 | 1957-04-26 | Safe landing of aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB865596A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2122044A (en) * | 1982-06-14 | 1984-01-04 | Inst Phys Tech Auftragsforsch | Apparatus for transmitting and receiving infrared signals |
-
1957
- 1957-04-26 GB GB13416/57A patent/GB865596A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2122044A (en) * | 1982-06-14 | 1984-01-04 | Inst Phys Tech Auftragsforsch | Apparatus for transmitting and receiving infrared signals |
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