FIELD: aviation.
SUBSTANCE: invention relates to antenna-feeder devices, mostly to antenna spinners of navigation systems of a helicopter and other low-speed aircrafts. A radio-transparent spinner of a navigation antenna of a helicopter system differs in that a spinner wall with a thickness of 1.0-2.5 mm is made of two prepreg layers based on quartz fabric with dielectric permeability of ε = 2.0-4.0, between which a glass mesh is placed, a thread thickness of which is equal to 0.5-1.5 mm, and a cell size is normalized to half a wavelength of an antenna operating range, and glass honeycomb is connected to an inner surface of the wall in a direction from a base to a top of the spinner, a thickness and a height of which are selected taking into account provision of optimal radio engineering characteristics and rigidity of the spinner.
EFFECT: provision of the minimal distortion of a directional diagram of an antenna device within obtainment of the maximal passage coefficient and the minimal level of side DD petals, as well as requirements for strength and rigidity.
1 cl, 3 dwg
Title | Year | Author | Number |
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RADIO TRANSPARENT RADOME OF NAVIGATION ANTENNA SYSTEM | 2023 |
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Authors
Dates
2023-02-06—Published
2021-12-24—Filed