GB804666A - Radio aerials for aircraft - Google Patents
Radio aerials for aircraftInfo
- Publication number
- GB804666A GB804666A GB460855A GB460855A GB804666A GB 804666 A GB804666 A GB 804666A GB 460855 A GB460855 A GB 460855A GB 460855 A GB460855 A GB 460855A GB 804666 A GB804666 A GB 804666A
- Authority
- GB
- United Kingdom
- Prior art keywords
- recess
- conductor
- aerial
- feeder
- coil
- 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
- H01Q1/287—Adaptation for use in or on aircraft, missiles, satellites, or balloons substantially flush mounted with the skin of the craft integrated in a wing or a stabiliser
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Astronomy & Astrophysics (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Physics & Mathematics (AREA)
- Remote Sensing (AREA)
- Details Of Aerials (AREA)
- Aerials With Secondary Devices (AREA)
Abstract
804,666. Aerials; aerial couplings. NATIONAL RESEARCH DEVELOPMENT CORPORATION. Feb. 15, 1956 [Feb. 16, 1955No. 4608/55. Addition to 704,659. Class 40 (7). An aircraft aerial system makes use of the metal skin of an aircraft member, such as a wing, as the aerial element and this is tuned and coupled to a transducer by means of a recess having a width equal or greater than its depth and conductive internal surfaces formed in a convex surface of the member. The recess contains means coupling it to a feeder and has a conductor or conductors arranged across its mouth and connecting a capacitor along the direction of flow of the radio-frequency currents. The dimensions of the recess and the value of the capacitor are chosen so as to tune the aerial system to frequencies within a required band. In one embodiment the recess 3 is formed in the leading edge of an aircraft wing 2 close to the fuselage 1. A coupling coil 4 is arranged in the recess and has a variable capacitor 7 connected across it for tuning purposes. The coaxial feeder has its inner conductor joined to the coil at an intermediate point 6 providing suitable matching and its outer conductor is earthed close to the point 30 at which the earthy side of the coil is connected to the side wall of the recess. A copper conductor 8 and capacitor 9 are connected across the mouth of the recess which may be protected by a non- conductive plastic sheet fairing 10. In a modification (Fig. 4) the tuned coil 4 is omitted and the inner conductor of the feeder led to a point 11 chosen so as to match the aerial to the feeder at a given operating frequency. In a more complex arrangement the feeder may be terminated at a switch on the side wall of the recess so arranged that the central conductor may be connected as required to any one of a number of extension wires connected to differing points 11 to provide proper matching at differing frequencies (Fig. 3, not shown). The capacitor 9 may be moved away from the recess and coupled to the side wall of the recess and the conductor 8 by a coaxial line; further, the conductor 8 may be made inductive by forming it as a coil. More than one recess may be provided to produce particular radiation patterns and the aerial may be formed from the tail fin or tail plane instead of a wing.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3249148A GB704659A (en) | 1955-02-16 | 1948-12-15 | Improvements in or relating to directly fed notched aerofoil aerials |
GB460855A GB804666A (en) | 1955-02-16 | 1955-02-16 | Radio aerials for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB460855A GB804666A (en) | 1955-02-16 | 1955-02-16 | Radio aerials for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB804666A true GB804666A (en) | 1958-11-19 |
Family
ID=9780369
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3249148A Expired GB704659A (en) | 1955-02-16 | 1948-12-15 | Improvements in or relating to directly fed notched aerofoil aerials |
GB460855A Expired GB804666A (en) | 1955-02-16 | 1955-02-16 | Radio aerials for aircraft |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3249148A Expired GB704659A (en) | 1955-02-16 | 1948-12-15 | Improvements in or relating to directly fed notched aerofoil aerials |
Country Status (1)
Country | Link |
---|---|
GB (2) | GB704659A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6175336B1 (en) | 1999-12-27 | 2001-01-16 | Northrop Grumman Corporation | Structural endcap antenna |
US6198445B1 (en) | 1999-12-29 | 2001-03-06 | Northrop Grumman Corporation | Conformal load bearing antenna structure |
CN110299602A (en) * | 2019-06-24 | 2019-10-01 | 陕西飞机工业(集团)有限公司 | A kind of mounting structure of hidden short-wave antenna |
US11258167B1 (en) | 2020-09-01 | 2022-02-22 | Rockwell Collins, Inc. | Embedded antennas in aerostructures and electrically short conformal antennas |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3618104A (en) * | 1968-02-26 | 1971-11-02 | Multronics Inc | Broadband cornucopia-type antenna system |
US3725941A (en) * | 1968-04-02 | 1973-04-03 | Lockheed Aircraft Corp | High-frequency notch-excited antenna |
-
1948
- 1948-12-15 GB GB3249148A patent/GB704659A/en not_active Expired
-
1955
- 1955-02-16 GB GB460855A patent/GB804666A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6175336B1 (en) | 1999-12-27 | 2001-01-16 | Northrop Grumman Corporation | Structural endcap antenna |
US6198445B1 (en) | 1999-12-29 | 2001-03-06 | Northrop Grumman Corporation | Conformal load bearing antenna structure |
CN110299602A (en) * | 2019-06-24 | 2019-10-01 | 陕西飞机工业(集团)有限公司 | A kind of mounting structure of hidden short-wave antenna |
CN110299602B (en) * | 2019-06-24 | 2022-03-15 | 陕西飞机工业(集团)有限公司 | Mounting structure of hidden short wave antenna |
US11258167B1 (en) | 2020-09-01 | 2022-02-22 | Rockwell Collins, Inc. | Embedded antennas in aerostructures and electrically short conformal antennas |
Also Published As
Publication number | Publication date |
---|---|
GB704659A (en) | 1954-02-24 |
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