GB544684A - Improvements in or relating to reel mechanism particularly for aircraft antennas - Google Patents

Improvements in or relating to reel mechanism particularly for aircraft antennas

Info

Publication number
GB544684A
GB544684A GB16757/40A GB1675740A GB544684A GB 544684 A GB544684 A GB 544684A GB 16757/40 A GB16757/40 A GB 16757/40A GB 1675740 A GB1675740 A GB 1675740A GB 544684 A GB544684 A GB 544684A
Authority
GB
United Kingdom
Prior art keywords
motor
cable
worm
spring
reel
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
GB16757/40A
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.)
LEAR AVIA Inc
Original Assignee
LEAR AVIA Inc
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 LEAR AVIA Inc filed Critical LEAR AVIA Inc
Publication of GB544684A publication Critical patent/GB544684A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/27Adaptation for use in or on movable bodies
    • H01Q1/28Adaptation for use in or on aircraft, missiles, satellites, or balloons
    • H01Q1/30Means for trailing antennas

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Astronomy & Astrophysics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Remote Sensing (AREA)
  • Transmission Devices (AREA)
  • Details Of Aerials (AREA)

Abstract

544,684. Winches. LEAR AVIA, Inc. Nov. 21, 1940, No. 16757. Convention date, Dec. 15, 1939. [Class 78 (v)] A reel-mechanism, particularly for aircraft antennae, comprises a cable &c. reel 32 mounted on a shaft 19 driven through worm gearing 7 and spur gearing 14, 15 by an electric motor 2. The worm 7 is carried slidably but non-rotatably by a spindle 5, on which are mounted, also slidably, two switch-button operating cams, 9,10 positioned respectively by a weak spring, 13 and a strong spring 12. When a manual switch is operated to start the motor 2 in the paying-out direction, the pull on the cable due to its attached weight or drag-sock tends to keep the worm 7 up against the cam 9 which is supported by the spring 13. When the cable is fully unwound the pull of its swivel terminal connection to the reel tends to reverse the direction of rotation of the latter and to force the worm 7 up against a bearing sleeve 6. This allows the spring 13 to push along the cam 9 to follow up and so operate the button of switch 20 to deenergise the motor 2. Should the cable snarl or foul the fairlead during unwinding the forward pull on the shaft 19 would similarly cease and the cam 9 be moved to stop the motor. If the manual switch be moved to the motor-reverse position, the cable will be wound in till the sock or ponder weight jerks it to a standstill at the end of the wind, and this will join the worm wheel and force the worm 7 toward the cams 9, 10, pushing these under the drive of the motor till the cam 10 presses in the button of switch 8 and stops the motor. The outward pressure of spring 12 on the worm 7 maintains tension in the wound-up cable. The reel 32 has a central aluminium core 31 keyed to the shaft 19, and is held in place by a snap slide assembly 30 engaging a groove in the shaft end. The flanges 29 have inturned lips to guide the cable 56 on to the middle of the reel rim. A warning light may be switched on during the time the cable is partly or wholly payed out, and a resistance may be included in one of the motor fields to equalise the motor speeds in both directions. The cams 9, 10 may switch in the non-operative field when the motor is stopped to produce a braking E.M.F. In a modification the sliding cams are replaced by spring-controlled discs.
GB16757/40A 1939-12-15 1940-11-21 Improvements in or relating to reel mechanism particularly for aircraft antennas Expired GB544684A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US309411A US2204579A (en) 1939-12-15 1939-12-15 Antenna reel mechanism

Publications (1)

Publication Number Publication Date
GB544684A true GB544684A (en) 1942-04-23

Family

ID=23198121

Family Applications (1)

Application Number Title Priority Date Filing Date
GB16757/40A Expired GB544684A (en) 1939-12-15 1940-11-21 Improvements in or relating to reel mechanism particularly for aircraft antennas

Country Status (2)

Country Link
US (1) US2204579A (en)
GB (1) GB544684A (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2472904A (en) * 1943-12-24 1949-06-14 Firm Autophon Ag Transmitting antenna with automatic tuning, particularly for aircraft wireless
DE1029432B (en) * 1957-01-25 1958-05-08 Hirschmann Radiotechnik Telescopic antenna that can be extended and retracted from inside the vehicle
DE1079133B (en) * 1957-05-18 1960-04-07 Hirschmann Radiotechnik Drive device for electrically extendable and retractable telescopic antennas from inside the vehicle
US3202378A (en) * 1963-03-08 1965-08-24 Roger L Williamson Motor driven reel for kites
US3247944A (en) * 1963-04-30 1966-04-26 Burroughs Corp Line find mechanism
US4153825A (en) * 1978-04-26 1979-05-08 General Motors Corporation Electric switch and actuator for an antenna drive system
US7140571B2 (en) * 2003-06-11 2006-11-28 Autoliv, Asp, Inc. Electric seat belt retractor system
CN112594347A (en) * 2020-12-11 2021-04-02 洛阳理工学院 Interval constant force device capable of realizing stepless regulation

Also Published As

Publication number Publication date
US2204579A (en) 1940-06-18

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