GB455164A - Improvements connecfed with directional wireless apparatus for aircraft - Google Patents
Improvements connecfed with directional wireless apparatus for aircraftInfo
- Publication number
- GB455164A GB455164A GB2184335A GB2184335A GB455164A GB 455164 A GB455164 A GB 455164A GB 2184335 A GB2184335 A GB 2184335A GB 2184335 A GB2184335 A GB 2184335A GB 455164 A GB455164 A GB 455164A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aerial
- rochester
- yoke
- connecfed
- aircraft
- 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
- H01Q1/12—Supports; Mounting means
- H01Q1/1235—Collapsible supports; Means for erecting a rigid antenna
Landscapes
- Transceivers (AREA)
Abstract
455,164. Aerials. SHORT BROS. (ROCHESTER & BEDFORD), Ltd., and PARKS, A. G., Seaplane Works, Rochester, Kent. Aug. 1, 1935, No. 21843. [Class 40 (v)] A frame-aerial for an aeroplane is mounted so that it can be extended outside the fuselage of the craft when in operation, and retracted inside when out of use. As shown, the frame a is mounted on a rotatable shaft b and is supported by a yoke c sliding on guide-rods d, d<1>. The yoke is fixed in its uppermost position by pins d<4>. In the withdrawn position, shown in dotted lines, the pivoted lower end b3 of the shaft is bent to one side to save space. The slot f formed in the body of the machine, to allow the aerial to emerge, is closed by a coverplate f when the aerial is in use, and by a cover-plate f<2> fixed to the top of the aerial when the latter is retracted. The aerial can be rotated, when exposed, by a hand wheel g<2> which co-operates with a graduated scale g<4> and cursor g<5>.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2184335A GB455164A (en) | 1935-08-01 | 1935-08-01 | Improvements connecfed with directional wireless apparatus for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2184335A GB455164A (en) | 1935-08-01 | 1935-08-01 | Improvements connecfed with directional wireless apparatus for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB455164A true GB455164A (en) | 1936-10-15 |
Family
ID=10169735
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2184335A Expired GB455164A (en) | 1935-08-01 | 1935-08-01 | Improvements connecfed with directional wireless apparatus for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB455164A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4907007A (en) * | 1986-03-26 | 1990-03-06 | Siemens Aktiengesellschaft | Mount and magnetic field probe for navigating a motor vehicle |
-
1935
- 1935-08-01 GB GB2184335A patent/GB455164A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4907007A (en) * | 1986-03-26 | 1990-03-06 | Siemens Aktiengesellschaft | Mount and magnetic field probe for navigating a motor vehicle |
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