GB1459057A - Moored helicopter - Google Patents

Moored helicopter

Info

Publication number
GB1459057A
GB1459057A GB576475A GB576475A GB1459057A GB 1459057 A GB1459057 A GB 1459057A GB 576475 A GB576475 A GB 576475A GB 576475 A GB576475 A GB 576475A GB 1459057 A GB1459057 A GB 1459057A
Authority
GB
United Kingdom
Prior art keywords
landing
helicopter
tethered
drive unit
baseplate
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
GB576475A
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.)
Dornier GmbH
Original Assignee
Dornier GmbH
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 Dornier GmbH filed Critical Dornier GmbH
Publication of GB1459057A publication Critical patent/GB1459057A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U10/00Type of UAV
    • B64U10/60Tethered aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerials With Secondary Devices (AREA)

Abstract

1459057 Tethered helicopters DORNIER GmbH 11 Feb 1975 [20 March 1974] 5764/75 Headings B7G and B7W A tethered helicopter has a rigid baseplate 12 from which a payload 26, e.g. radar or sensors, is suspended, a drive uint 14, 16 mounted on the baseplate, and a partially-cylindrical, downwardly-flared, hollow landing cone 30 through which the mooring cable 42 extends. The drive unit is housed in a tapered shell 22. The landing cone is formed of glass-fibre-reinforced plastics and has a slotted landing ring 38 which may be provided with cushioning devices (not shown). A set-down switch 46 is provided to switch off the drive unit upon landing.
GB576475A 1974-03-20 1975-02-11 Moored helicopter Expired GB1459057A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE7409697 1974-03-20

Publications (1)

Publication Number Publication Date
GB1459057A true GB1459057A (en) 1976-12-22

Family

ID=6644261

Family Applications (1)

Application Number Title Priority Date Filing Date
GB576475A Expired GB1459057A (en) 1974-03-20 1975-02-11 Moored helicopter

Country Status (3)

Country Link
FR (1) FR2264714B3 (en)
GB (1) GB1459057A (en)
IT (1) IT1036882B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11772814B2 (en) 2016-12-02 2023-10-03 Elistair System including a drone, a wire, and a docking station, enabling autonomous landings of the drones in degraded conditions

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US11772814B2 (en) 2016-12-02 2023-10-03 Elistair System including a drone, a wire, and a docking station, enabling autonomous landings of the drones in degraded conditions

Also Published As

Publication number Publication date
FR2264714A3 (en) 1975-10-17
FR2264714B3 (en) 1978-07-21
IT1036882B (en) 1979-10-30

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee