GB819727A - Improvements in or relating to aircraft warning system - Google Patents
Improvements in or relating to aircraft warning systemInfo
- Publication number
- GB819727A GB819727A GB33764/55A GB3376455A GB819727A GB 819727 A GB819727 A GB 819727A GB 33764/55 A GB33764/55 A GB 33764/55A GB 3376455 A GB3376455 A GB 3376455A GB 819727 A GB819727 A GB 819727A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- lamp
- degrees
- light
- relating
- 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
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B5/00—Visible signalling systems, e.g. personal calling systems, remote indication of seats occupied
- G08B5/22—Visible signalling systems, e.g. personal calling systems, remote indication of seats occupied using electric transmission; using electromagnetic transmission
- G08B5/36—Visible signalling systems, e.g. personal calling systems, remote indication of seats occupied using electric transmission; using electromagnetic transmission using visible light sources
- G08B5/38—Visible signalling systems, e.g. personal calling systems, remote indication of seats occupied using electric transmission; using electromagnetic transmission using visible light sources using flashing light
Landscapes
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- General Physics & Mathematics (AREA)
- Audible And Visible Signals (AREA)
Abstract
819,727. Signal lamps for aircraft. ATKINS, H. W. Nov. 24, 1955 [Aug. 2, 1955], No. 33764/55. Class 75(4) [Also in Group XXXVIII] Apparatus for use on an aircraft for warning an observer on another aircraft of the degree of probability of collision between the two aircraft comprises a stream-lined plastic bubble 21 situated at the top of the tail 19 of an aircraft and enclosing three lamps 25, 26 and 27 flashing at different predetermined rates (see Group XXXVIII). Baffles 23 and 24 are arranged as shown to limit the forward light from the lamp 25 to a sector of 120 degrees, the rearward light from lamp 27 to a sector of 120 degrees and light from lamp 26 to left and right sectors of 60 degrees each.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US819727XA | 1955-08-02 | 1955-08-02 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB819727A true GB819727A (en) | 1959-09-09 |
Family
ID=22167573
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB33764/55A Expired GB819727A (en) | 1955-08-02 | 1955-11-24 | Improvements in or relating to aircraft warning system |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB819727A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8573820B2 (en) | 2011-10-26 | 2013-11-05 | Honeywell International Inc. | Modular LED based aircraft rear position light |
-
1955
- 1955-11-24 GB GB33764/55A patent/GB819727A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8573820B2 (en) | 2011-10-26 | 2013-11-05 | Honeywell International Inc. | Modular LED based aircraft rear position light |
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