RU94025329A - Device for take-off and landing of flying vehicles - Google Patents

Device for take-off and landing of flying vehicles

Info

Publication number
RU94025329A
RU94025329A RU94025329/11A RU94025329A RU94025329A RU 94025329 A RU94025329 A RU 94025329A RU 94025329/11 A RU94025329/11 A RU 94025329/11A RU 94025329 A RU94025329 A RU 94025329A RU 94025329 A RU94025329 A RU 94025329A
Authority
RU
Russia
Prior art keywords
ship
landing
platform
deck
aircraft
Prior art date
Application number
RU94025329/11A
Other languages
Russian (ru)
Other versions
RU2090459C1 (en
Inventor
М.А.-Х. Шариф
А.В. Егоршев
В.А. Комаров
М.Ю. Араби
Original Assignee
М.А.-Х. Шариф
А.В. Егоршев
В.А. Комаров
М.Ю. Араби
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 М.А.-Х. Шариф, А.В. Егоршев, В.А. Комаров, М.Ю. Араби filed Critical М.А.-Х. Шариф
Priority to RU94025329A priority Critical patent/RU2090459C1/en
Publication of RU94025329A publication Critical patent/RU94025329A/en
Application granted granted Critical
Publication of RU2090459C1 publication Critical patent/RU2090459C1/en

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Landscapes

  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Tires In General (AREA)

Abstract

FIELD: aircraft manufacture; auxiliary equipment used for take-off and landing of vertical take-off and landing aeroplanes and helicopters on shipboard platforms not equipped with standard take-off and landing equipment. SUBSTANCE: device has perforated plate mounted above surface of ground or ship's deck. Plate is made in form of platform. Device is also provided with mechanism for mounting and moving the platform and drive. End side of perforated plate is secured by means of hinges at level of ship's deck and is provided with guides secured on lower surface of plate. Connected to cantilever end of plate are N double-member breaker struts. End of each strut is articulated to ship's side. Double-member breaker strut is articulated to rod of drive at break point. Housing of drive is articulated in ship's recess. Tip of rod of telescopic drive is provided with rollers which are engageable with guide of platform in raising and lowering it. EFFECT: enhanced efficiency due to avoidance of negative effects arising due to action of gas jet from engines on flying vehicle and on ship's deck. 3 dwg

Claims (1)

Изобретение относится к области самолетостроения, а именно к вспомогательному оборудованию, обеспечивающему взлет и посадку самолетов вертикального взлета и посадки (СВВП) и вертолетов на необорудованные штатными взлетно-посадочными площадками корабли. Цель изобретения - похищение эффективности эксплуатации летательных аппаратов за счет исключения отрицательных эффектов, возникающих от воздействия газовой струи от двигателей на летательный аппарат и палубу корабля. Указанная цель достигается тем, что в устройстве для обеспечения взлета и посадки летательных аппаратов, содержащем перфорированную пластину, установленную над поверхностью земли или палубы корабля, выполненную в виде площадки, механизм ее установки и перемещения и привод, перфорированная площадка торцевой стороной шарнирно закрепляется на уровне палубы корабля, снабжена направляющими, закрепленными на нижней поверхности пластины, а к консольному концу последней присоединено N двузвенных ломающихся подкосов, каждый из которых другим своим концом закреплен шарнирно на борту корабля, при этом двузвенный ломающийся подкос в точке излома шарнирно соединен с штоком привода, выполненного телескопическим, корпус которого закреплен шарнирно в нише корпуса корабля, причем на законцовке штока телескопического привода установлены ролики, контактирующие при подъеме и опускании площадки с направляющими последней.The invention relates to the field of aircraft construction, and in particular to auxiliary equipment providing takeoff and landing of vertical take-off and landing aircraft (VTOL) and helicopters on ships not equipped with regular take-off and landing sites. The purpose of the invention is the theft of the operational efficiency of aircraft by eliminating the negative effects arising from the effects of a gas stream from the engines on the aircraft and the deck of the ship. This goal is achieved by the fact that in the device for providing takeoff and landing of aircraft, containing a perforated plate mounted above the surface of the earth or the deck of the ship, made in the form of a platform, the mechanism for its installation and movement and the drive, the perforated platform with the end side is pivotally fixed at deck level the ship, is equipped with guides mounted on the bottom surface of the plate, and N two-link breaking braces attached to the cantilever end of the latter, each of which is different its end is pivotally mounted on board the ship, while the two-link breaking strut at the break point is pivotally connected to the telescopic drive rod, the body of which is pivotally mounted in the ship’s hull, and rollers are mounted on the tip of the telescopic drive rod, which contact when raising and lowering the platform with guides last.
RU94025329A 1994-07-06 1994-07-06 Flying vehicle alighting gear RU2090459C1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU94025329A RU2090459C1 (en) 1994-07-06 1994-07-06 Flying vehicle alighting gear

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU94025329A RU2090459C1 (en) 1994-07-06 1994-07-06 Flying vehicle alighting gear

Publications (2)

Publication Number Publication Date
RU94025329A true RU94025329A (en) 1996-12-20
RU2090459C1 RU2090459C1 (en) 1997-09-20

Family

ID=20158142

Family Applications (1)

Application Number Title Priority Date Filing Date
RU94025329A RU2090459C1 (en) 1994-07-06 1994-07-06 Flying vehicle alighting gear

Country Status (1)

Country Link
RU (1) RU2090459C1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104975571A (en) * 2015-07-08 2015-10-14 何春旺 Parking device for air vehicle
CN105019367A (en) * 2015-07-08 2015-11-04 何春旺 Parking device for aircraft, and control method of parking device

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2943990B1 (en) * 2009-04-03 2011-04-01 Dcns ANCHORING HARPO, IN PARTICULAR AN AIRCRAFT AND ANCHORING SYSTEM COMPRISING SUCH A HARPOON.
IL219836A (en) * 2012-05-16 2017-02-28 Meir Yoffe Point take-off and landing of unmanned flying objects
CN108945286A (en) * 2018-07-04 2018-12-07 中国船舶工业集团公司第七0八研究所 Active extendible helicopter platform device

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104975571A (en) * 2015-07-08 2015-10-14 何春旺 Parking device for air vehicle
CN105019367A (en) * 2015-07-08 2015-11-04 何春旺 Parking device for aircraft, and control method of parking device
CN105019367B (en) * 2015-07-08 2017-07-18 珠海磐磊智能科技有限公司 Aircraft stop device and its control method
CN104975571B (en) * 2015-07-08 2018-12-04 珠海磐磊智能科技有限公司 Aircraft stop device

Also Published As

Publication number Publication date
RU2090459C1 (en) 1997-09-20

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