GB1286419A - Radar antenna support and drive assembly - Google Patents

Radar antenna support and drive assembly

Info

Publication number
GB1286419A
GB1286419A GB07522/71A GB1752271A GB1286419A GB 1286419 A GB1286419 A GB 1286419A GB 07522/71 A GB07522/71 A GB 07522/71A GB 1752271 A GB1752271 A GB 1752271A GB 1286419 A GB1286419 A GB 1286419A
Authority
GB
United Kingdom
Prior art keywords
pedestal part
secured
gear
flange
nuts
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
Application number
GB07522/71A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of GB1286419A publication Critical patent/GB1286419A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q25/00Antennas or antenna systems providing at least two radiating patterns
    • H01Q25/04Multimode antennas
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
    • H01Q3/04Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying one co-ordinate of the orientation

Landscapes

  • Aerials With Secondary Devices (AREA)
  • Details Of Aerials (AREA)
  • Support Of Aerials (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

1286419 Aerials WESTINGHOUSE ELECTRIC CORP 27 May 1971 [30 June 1970] 17522/71 Heading H4A A radar aerial support and drive assembly comprises a fixed pedestal part 13 which is adapted to be mounted atop a tower 35, a main-support ball bearing removably mounted on the top of the said fixed pedestal part, a bull-gear 16 mounted on said ball-bearing, a rotary pedestal part 5 having a removable central top cover member 6 removably secured to said bull gear, and a mounting frame 1, for a feed horn 2 and a reflector 3, which is secured to the rotary pedestal part so that removal of the cover 6 is not impeded. The assembly also comprises a pair of drive means, removably secured to the fixed pedestal, and including pinions engaging diametrically opposite points of the bull gear, and means for supporting and locking the rotary pedestal part during removal of its top cover member 6. The mounting frame 1 includes side members 8 spaced apart on opposite sides of the part 5, and attached by means allowing the attitude of the frame to be adjusted relative to the azimuthal axis 4, for determining the elevation angle of the beam (Fig. 1, not shown). A waveguide feed 10 for the horn 2 is disposed along the axis 4, and is provided with a rotary joint 26. The top cover member 6 of the rotary pedestal part 5 is secured by screws 7, and the bull gear 16, which also constitutes the outer race of the main support ball bearing, is secured to the said cover member by screws 23. The inner race 17 of the ball-bearing fits over a cylindrical surface 14 to an annular shoulder 12, which are provided in the fixed pedestal part 13, and it is secured by screws 20. Pinions 40 mesh with the gear 16 and are driven by electric motors 41 through speed reducing mechanisms 42 and self-aligning assemblies 46, which include universal joints 43, 44. An annular well is provided so that the gear 16 and the pinions 40 can be immersed in lubricating oil 62. The fixed pedestal part 13 has mounting brackets 32 by means of which it is bolted to the top of the tower 35. Studs 34, carrying nuts 36, 39, engage in threaded holes in the brackets 32 and are normally screwed down so that they clear the flange 31 of the rotary pedestal part 5. When it is desired to lock the part 5, holes 37 in the flange 31 are aligned with the studs 34, the nuts 36 are removed, the studs 34 are screwed up and through the flange 31, the nuts 36 are replaced and they, and the nuts 39, are tightened against the said flange.
GB07522/71A 1970-06-30 1971-05-27 Radar antenna support and drive assembly Expired GB1286419A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US5109870A 1970-06-30 1970-06-30

Publications (1)

Publication Number Publication Date
GB1286419A true GB1286419A (en) 1972-08-23

Family

ID=21969332

Family Applications (1)

Application Number Title Priority Date Filing Date
GB07522/71A Expired GB1286419A (en) 1970-06-30 1971-05-27 Radar antenna support and drive assembly

Country Status (6)

Country Link
US (1) US3624656A (en)
JP (1) JPS5443344B1 (en)
BE (1) BE769253A (en)
DE (1) DE2131641A1 (en)
FR (1) FR2096601B1 (en)
GB (1) GB1286419A (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH622129A5 (en) * 1977-09-30 1981-03-13 Bbc Brown Boveri & Cie
US4858490A (en) * 1987-10-13 1989-08-22 Hughes Aircraft Company Two motor redundant drive mechanism
JP3475872B2 (en) * 1999-09-30 2003-12-10 日本電気株式会社 Antenna AZ wide-angle driving device and driving method
US6398444B1 (en) * 1999-11-19 2002-06-04 Raytheon Company Coupling for airport surveillance antennas and other rotating structures
US6608596B2 (en) * 2001-10-12 2003-08-19 The Boeing Company Microwave reflector antenna
US10720714B1 (en) * 2013-03-04 2020-07-21 Ethertronics, Inc. Beam shaping techniques for wideband antenna
CN110018444A (en) * 2019-03-14 2019-07-16 安徽天兵电子科技股份有限公司 A kind of reciprocation type rotation rotating radar
CN115289380B (en) * 2022-06-29 2024-02-09 安徽恒诺机电科技有限公司 Pitching electric cylinder for single motor double cylinders

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3040318A (en) * 1950-08-09 1962-06-19 United Aircraft Corp Radar antenna azimuth control and search system
US2719921A (en) * 1951-11-23 1955-10-04 Bendix Aviat Corp Tiltable search antenna pedestal
US3315543A (en) * 1964-06-24 1967-04-25 Falk Corp Housing for multiple-pinion gear drives
US3324474A (en) * 1964-09-18 1967-06-06 Gen Dynamics Corp Rotatable horn antenna with feed moveable out of horn to form omnidirectional antenna

Also Published As

Publication number Publication date
JPS5443344B1 (en) 1979-12-19
FR2096601A1 (en) 1972-02-18
FR2096601B1 (en) 1976-05-28
US3624656A (en) 1971-11-30
DE2131641A1 (en) 1972-01-13
BE769253A (en) 1971-12-29

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees