GB2369809A - Aircraft landing system utlising electromagnetic field - Google Patents

Aircraft landing system utlising electromagnetic field Download PDF

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Publication number
GB2369809A
GB2369809A GB0030113A GB0030113A GB2369809A GB 2369809 A GB2369809 A GB 2369809A GB 0030113 A GB0030113 A GB 0030113A GB 0030113 A GB0030113 A GB 0030113A GB 2369809 A GB2369809 A GB 2369809A
Authority
GB
United Kingdom
Prior art keywords
aircraft
landing
wheels
platform
helicopter
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.)
Granted
Application number
GB0030113A
Other versions
GB0030113D0 (en
GB2369809B (en
Inventor
Francis Wright
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB0030113A priority Critical patent/GB2369809B/en
Publication of GB0030113D0 publication Critical patent/GB0030113D0/en
Publication of GB2369809A publication Critical patent/GB2369809A/en
Application granted granted Critical
Publication of GB2369809B publication Critical patent/GB2369809B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/42Arrangement or adaptation of brakes
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/32Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/52Skis or runners
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND 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
    • B64F1/00Ground or aircraft-carrier-deck installations
    • B64F1/12Ground or aircraft-carrier-deck installations for anchoring aircraft
    • B64F1/125Mooring or ground handling devices for helicopters

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Braking Arrangements (AREA)

Abstract

A runway, oil rig landing platform, or landing strip on an aircraft carrier, is provided with means for generating an electromagnetic field. An aircraft or helicopter undercarriage is provided with a metallic fixture, such as a ski or plate 5, which may be lowered or raised by means of a hydraulic cylinder 3, the fixture interacting with the electromagnetic field on landing of the aircraft/helicopter to brake the aircraft's motion and hold the aircraft/helicopter down.

Description

<Desc/Clms Page number 1>
Landing platform for helicopters and helicopters without wheels.
The helicopter must be fitted with its own metallic fitting set in the bottom fixture in order for it to be attracted to the electromagnetic field of the platform.
The electromagnetic field has to be spaced out across the platform in small strips. When the helicopter comes down to land it has to be activated to hold the helicopter down and, if necessary, secure with brackets.
Fig. 3 The platform has to have the electromagnetic field embedded flat with the top and must be activated before a helicopter lands.
1. Electromagnetic fields on the platform 2. Fixture on the helicopter 3. Metallic fitting on fixture 4. Fitted on helicopter
<Desc/Clms Page number 2>
Landing gear and platform for helicopter and planes Fig. 1
An electromagnetic platform for safe landing on oil rigs, flat roofed houses, warships, aircraft carriers and airfields, with the fixture or frame to keep the helicopter on the ground. The fixture must have a metallic fitting to attract it to the electromagnetic field on the platform.
Helicopters with wheels must have fixtures fastened on to the axis or struts which have to have a hydraulically controlled pressure mechanism to enable the pilot to move the fixture up and down. As the tyres compress by touching the platform or landing strip the pilot must adjust, if
necessary, and activate the sliding skis through the hydraulic pressure. They must also be of a metallic material to be attracted to the electromagnetic field on the platform or landing strip on aircraft carrier.
The aircraft can be stopped it there is enough power in the electromagnet and so preventing it from overshooting the aircraft carrier or airfieìd, The electromagnetic fields must be of various strengths to match the size of the different
helicopters and planes. especially in stormy weather. The hydraulic cylinder must be able to move up and down as well as pivot because planes come down to land at an angle. The helicopter takes off and lands in more of a vertical direction, but there is stiR a pivotal movement necessary.
The pilot has to control the hydraulic brake mechanism as the trailing ski will touch the platform first and give the pilot a warning light This informs the pilot that the skis must go down to brake the aircraft and prevent overshooting the aircraft carrier or the air field The electromagnetic fields must be embedded flat into the platform, runway and deck on aircraft carriers and oil ngs,
<Desc/Clms Page number 3>
Fig. 1 1. wheels on planes and helicopters 2. axis. and for pivoting the hydraulic cylinder 3. Hydraulic cylinder to move the braking skis up and down 4. struts or support frame or fixture 5. skis or flat metallic plates 6. pipe for hydraulic fluid to the breaking cylinder with warning light for pilot 7. supporting plate with skis 8. landing platform for the helicopter with electromagnetic fields on oil rigs and ships.
9. Runways for planes on aircraft carriers and civilian airfields with electromagnetic fields 10. the electromagnetic fields have to be embedded into the platform or runway 11. sensor-to cockpit when landing Fig. 2 wheels with braking cylinder Fig. 3 landing platform for helicopter on oil rigs
Fig. 4 landing strip on aircraft carrier Fig. 5 Runway on airfields

Claims (11)

  1. Claim Fig. 1 1. wheels on planes and helicopters
  2. 2. axis, and for pivoting the hydraulic cylinder
  3. 3. Hydraulic cylinder to move the braking skis up and down
  4. 4. struts or support frame or fixture
  5. 5. skis or flat metallic plates
  6. 6. pipe for hydraulic fluid to the breaking cylinder with warning light for pilot
  7. 7. supporting plate with skis
  8. 8. landing platform for the helicopter with electromagnetic fields on oil rigs and ships.
  9. 9. Runways for planes on aircraft carriers and civilian airfields with electromagnetic fields
  10. 10. the electromagnetic fields have to be embedded into the platform or runway
  11. 11. sensor-to cockpit when landing Fig. 2 wheels with braking cylinder Fig. 3 landing platform for helicopter on oil rigs Fig. 4 landing strip on aircraft carrier Fig. 5 Runway on airfields
    <Desc/Clms Page number 5>
    Amended claims have been filed as follows CLAIMS 1. An aircraft landing system comprising a landing surface for receiving and supporting a landing aircraft, said surface comprising electromagnetic means embedded therein for generating an electromagnetic field, said aircraft landing system further comprising an aircraft having an undercarriage provided with a plurality of wheels, a plurality of elongate metallic plates movably mounted on said aircraft, a plurality of hydraulic cylinders each connected and arranged so as to be capable of moving a respective one of said plates relative to a respective one of said wheels between a first position, in which said respective one of said wheels projects beneath said respective one of said plates, relative to the aircraft, and a second position, in which said respective one of said plates can contact said landing surface upon landing of said aircraft on said surface, a warning light for the pilot of said aircraft, and means for actuating the warning light as a plate touches said landing surface, said electromagnetic means, being capable of being activated to produce a magnetic field of sufficient strength to attract said elongate metallic plates to said surface whereby to hold said aircraft on said surface.
GB0030113A 2000-12-11 2000-12-11 Electromagnetic landing system for aircraft Expired - Fee Related GB2369809B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0030113A GB2369809B (en) 2000-12-11 2000-12-11 Electromagnetic landing system for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0030113A GB2369809B (en) 2000-12-11 2000-12-11 Electromagnetic landing system for aircraft

Publications (3)

Publication Number Publication Date
GB0030113D0 GB0030113D0 (en) 2001-01-24
GB2369809A true GB2369809A (en) 2002-06-12
GB2369809B GB2369809B (en) 2002-10-23

Family

ID=9904802

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0030113A Expired - Fee Related GB2369809B (en) 2000-12-11 2000-12-11 Electromagnetic landing system for aircraft

Country Status (1)

Country Link
GB (1) GB2369809B (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013079583A1 (en) * 2011-12-02 2013-06-06 Datanion Gmbh Method for landing an airship on a landing device placed on the ground
CN103332295A (en) * 2013-06-27 2013-10-02 厦门天圣能源科技有限公司 Novel helicopter carrier landing system
WO2016175648A1 (en) * 2015-04-30 2016-11-03 Poh Chung Kiak Intelligent docking system with automated stowage for uavs
RU2631093C1 (en) * 2016-10-06 2017-09-18 Федеральное государственное бюджетное образовательное учреждение высшего образования "Петербургский государственный университет путей сообщения Императора Александра I" Device for landing aircraft on ship

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6056096A (en) * 1983-09-08 1985-04-01 Yukio Okura Anodic oxidation of titanium or titanium alloy
US5222689A (en) * 1991-04-22 1993-06-29 Leonid Simuni Aircraft having magnetic suspension systems
US5253825A (en) * 1992-07-30 1993-10-19 Christian Melvyn R Aircraft ski

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0656096A (en) * 1992-08-05 1994-03-01 Fujita Corp Take off gear for airplane

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6056096A (en) * 1983-09-08 1985-04-01 Yukio Okura Anodic oxidation of titanium or titanium alloy
US5222689A (en) * 1991-04-22 1993-06-29 Leonid Simuni Aircraft having magnetic suspension systems
US5253825A (en) * 1992-07-30 1993-10-19 Christian Melvyn R Aircraft ski

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
PAJ Abstract and JP050016897 A *
WPI Abstract Accesion No. 1994-254025 [31] and RU2005672 *

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013079583A1 (en) * 2011-12-02 2013-06-06 Datanion Gmbh Method for landing an airship on a landing device placed on the ground
US9321541B2 (en) 2011-12-02 2016-04-26 Datanion Gmbh Method for landing an airship on a landing device placed on the ground
CN103332295A (en) * 2013-06-27 2013-10-02 厦门天圣能源科技有限公司 Novel helicopter carrier landing system
WO2016175648A1 (en) * 2015-04-30 2016-11-03 Poh Chung Kiak Intelligent docking system with automated stowage for uavs
RU2631093C1 (en) * 2016-10-06 2017-09-18 Федеральное государственное бюджетное образовательное учреждение высшего образования "Петербургский государственный университет путей сообщения Императора Александра I" Device for landing aircraft on ship

Also Published As

Publication number Publication date
GB0030113D0 (en) 2001-01-24
GB2369809B (en) 2002-10-23

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20051211