GB903137A - Improvements in or relating to aircraft aerials - Google Patents
Improvements in or relating to aircraft aerialsInfo
- Publication number
- GB903137A GB903137A GB1464460A GB1464460A GB903137A GB 903137 A GB903137 A GB 903137A GB 1464460 A GB1464460 A GB 1464460A GB 1464460 A GB1464460 A GB 1464460A GB 903137 A GB903137 A GB 903137A
- Authority
- GB
- United Kingdom
- Prior art keywords
- link
- section
- tension
- aerial
- sections
- 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
- 239000012212 insulator Substances 0.000 abstract 1
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
- H01Q1/285—Aircraft wire antennas
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Astronomy & Astrophysics (AREA)
- General Physics & Mathematics (AREA)
- Elimination Of Static Electricity (AREA)
Abstract
903,137. Aerials. CHELTON (ELECTROSTATICS) Ltd., SANDERSON, W. T., and SMITH, H. R. April 25, 1961 [April 26, 1960], No. 14644/60. Class 40 (7). A link unit of an aircraft stretched wire aerial comprises two sections relatively movable in the direction of applied tension with coacting stop means on the sections limiting the extent of the movement, a first weak link holding the sections with the stop means apart, and a second weak link securing one section to the aerial, or to a third section, it being so arranged that the first link fractures under a smaller stress than the second. Excessive tension causes the first link to fracture, the resulting extension tending to reduce the tension. In the event of the tension still increasing, the second link fractures leaving the aerial free. A spring tension unit may be provided between one section and a support, e.g. the tailplane. A pull to the left on shaft 20 causes link 23 to shear and the stop member 31 to engage the shoulder 32 of an insulator 21. The second link section, between this section and the end of the aerial, is not shown.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1464460A GB903137A (en) | 1960-04-26 | 1960-04-26 | Improvements in or relating to aircraft aerials |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1464460A GB903137A (en) | 1960-04-26 | 1960-04-26 | Improvements in or relating to aircraft aerials |
Publications (1)
Publication Number | Publication Date |
---|---|
GB903137A true GB903137A (en) | 1962-08-09 |
Family
ID=10044974
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1464460A Expired GB903137A (en) | 1960-04-26 | 1960-04-26 | Improvements in or relating to aircraft aerials |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB903137A (en) |
-
1960
- 1960-04-26 GB GB1464460A patent/GB903137A/en not_active Expired
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