GB486084A - Improvements in aerials for aircraft radio compasses - Google Patents
Improvements in aerials for aircraft radio compassesInfo
- Publication number
- GB486084A GB486084A GB3231536A GB3231536A GB486084A GB 486084 A GB486084 A GB 486084A GB 3231536 A GB3231536 A GB 3231536A GB 3231536 A GB3231536 A GB 3231536A GB 486084 A GB486084 A GB 486084A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aerial
- cabin
- windows
- dielectric
- aerials
- 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
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01Q—ANTENNAS, i.e. RADIO AERIALS
- H01Q1/00—Details of, or arrangements associated with, antennas
- H01Q1/27—Adaptation for use in or on movable bodies
- H01Q1/28—Adaptation for use in or on aircraft, missiles, satellites, or balloons
- H01Q1/286—Adaptation for use in or on aircraft, missiles, satellites, or balloons substantially flush mounted with the skin of the craft
Abstract
486,084. Wireless signalling. BASHENOFF, V. I. Nov. 25, 1936, No. 32315. [Class 40 (v)] A loop aerial for an all-metal aeroplane is mounted inside the cabin which has glass or celluloid windows. It is mounted so as not to obscure the view through the windows, the vertical limbs being spaced away from the walls, whilst the horizontal limbs may be placed close to the metal framework. It may follow the contour of the dielectric as shown at A in Fig. 1 where the nose of the cabin is fitted with a window, and at A in Fig. 2 where it is fitted around the transparent windscreen. The aerial may also be located outside the machine in a position where it closely follows the contours of a dielectric surface. The arrangement prevents frictional drag, reduces ice-formation, and minimizes the effect of rain-static. The aerial may be adjusted relatively to the plane of symmetry of the craft to compensate for wind " drift," or one end of the coil windings may be loaded relatively to the other end for the same purpose. Specification 473,866 is referred to.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3231536A GB486084A (en) | 1936-11-25 | 1936-11-25 | Improvements in aerials for aircraft radio compasses |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB3231536A GB486084A (en) | 1936-11-25 | 1936-11-25 | Improvements in aerials for aircraft radio compasses |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB486084A true GB486084A (en) | 1938-05-25 |
Family
ID=10336690
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB3231536A Expired GB486084A (en) | 1936-11-25 | 1936-11-25 | Improvements in aerials for aircraft radio compasses |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB486084A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2490330A (en) * | 1944-06-26 | 1949-12-06 | Curtiss Wright Corp | Aircraft antenna system |
| DE757212C (en) * | 1939-02-07 | 1953-03-23 | Blaupunkt Werke Gmbh | Rod antenna made of telescopic extendable and retractable members for vehicles |
-
1936
- 1936-11-25 GB GB3231536A patent/GB486084A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE757212C (en) * | 1939-02-07 | 1953-03-23 | Blaupunkt Werke Gmbh | Rod antenna made of telescopic extendable and retractable members for vehicles |
| US2490330A (en) * | 1944-06-26 | 1949-12-06 | Curtiss Wright Corp | Aircraft antenna system |
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