GB1063652A - Ground handling equipment for vertical take off and landing aircraft - Google Patents
Ground handling equipment for vertical take off and landing aircraftInfo
- Publication number
- GB1063652A GB1063652A GB4332664A GB4332664A GB1063652A GB 1063652 A GB1063652 A GB 1063652A GB 4332664 A GB4332664 A GB 4332664A GB 4332664 A GB4332664 A GB 4332664A GB 1063652 A GB1063652 A GB 1063652A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- trackway
- handling equipment
- cable
- platform
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/12—Anchoring
- B64F1/125—Mooring or ground handling devices for helicopters
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
Abstract
1,063,652. Aircraft landing places. MINISTER OF AVIATION LONDON. Oct. 22, 1965 [Oct. 23, 1964], No. 43326/64. Heading B7G. Handling equipment to facilitate the landing of a VTOL aircraft, e.g. a helicopter, on a movable platform such as a ship's deck, comprises a cable guide 13, through which a cable lowered from the aircraft may be led to a winch 15 on the platform, movably mounted on a trackway 18 (Fig. 4, not shown) so that as the aircraft moves relative to the platform, the guide tends to remain underneath the aircraft. The trackway is arcuate, and as seen in end elevation (Fig. 1, not shown) is centred on the centre of roll of the ship. The trackway may also be arcuate as seen in plan, and the curvature in both planes is achieved by its lying in a plane inclined at 45 degrees to the horizontal. The point of attachment of the cable to the winch lies on the polar axis of the trackway.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB4332664A GB1063652A (en) | 1964-10-23 | 1964-10-23 | Ground handling equipment for vertical take off and landing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB4332664A GB1063652A (en) | 1964-10-23 | 1964-10-23 | Ground handling equipment for vertical take off and landing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1063652A true GB1063652A (en) | 1967-03-30 |
Family
ID=10428283
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB4332664A Expired GB1063652A (en) | 1964-10-23 | 1964-10-23 | Ground handling equipment for vertical take off and landing aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB1063652A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014102437A1 (en) * | 2012-12-31 | 2014-07-03 | Universidad Pablo De Olavide | System for controlling rotary-wing unmanned aircraft for vertical landing on moving surfaces by feeding forward forces in the control system |
| DE102014016914A1 (en) * | 2014-11-17 | 2016-05-19 | Thyssenkrupp Ag | System and method for obtaining an unmanned aerial vehicle |
| CN113335544A (en) * | 2021-06-30 | 2021-09-03 | 燕山大学 | Transmission system of landing assisting device of ship-based helicopter |
| US11548657B2 (en) | 2018-03-22 | 2023-01-10 | Israel Aerospace Industries Ltd. | Aerial vehicle securing system and method |
-
1964
- 1964-10-23 GB GB4332664A patent/GB1063652A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014102437A1 (en) * | 2012-12-31 | 2014-07-03 | Universidad Pablo De Olavide | System for controlling rotary-wing unmanned aircraft for vertical landing on moving surfaces by feeding forward forces in the control system |
| DE102014016914A1 (en) * | 2014-11-17 | 2016-05-19 | Thyssenkrupp Ag | System and method for obtaining an unmanned aerial vehicle |
| US11548657B2 (en) | 2018-03-22 | 2023-01-10 | Israel Aerospace Industries Ltd. | Aerial vehicle securing system and method |
| CN113335544A (en) * | 2021-06-30 | 2021-09-03 | 燕山大学 | Transmission system of landing assisting device of ship-based helicopter |
| CN113335544B (en) * | 2021-06-30 | 2022-08-30 | 燕山大学 | Transmission system of ship-based helicopter landing assisting device |
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