SU14574A1 - Device for take-off of an aircraft, with the use of an aircraft temporarily carrying an aircraft, a mast of suspension and delay cables - Google Patents

Device for take-off of an aircraft, with the use of an aircraft temporarily carrying an aircraft, a mast of suspension and delay cables

Info

Publication number
SU14574A1
SU14574A1 SU23903A SU23903A SU14574A1 SU 14574 A1 SU14574 A1 SU 14574A1 SU 23903 A SU23903 A SU 23903A SU 23903 A SU23903 A SU 23903A SU 14574 A1 SU14574 A1 SU 14574A1
Authority
SU
USSR - Soviet Union
Prior art keywords
aircraft
mast
take
suspension
cables
Prior art date
Application number
SU23903A
Other languages
Russian (ru)
Inventor
А.Г. Нигай
Original Assignee
А.Г. Нигай
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 А.Г. Нигай filed Critical А.Г. Нигай
Priority to SU23903A priority Critical patent/SU14574A1/en
Application granted granted Critical
Publication of SU14574A1 publication Critical patent/SU14574A1/en

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Description

Известны устройста дл  взлета самолетов с малых площадок, в которых применены временно несущи самолет органы, мачты, подвесные и задерживающие тросы. В предлагаемом устройстве,- с целью облегчени  взлета и предохранени  от падени , указанные временно несущие самолет органы снабжаютс  .поддерживающими поверхност ми и хвостовым пропеллером , вращаемым посредством эле . ктромоторов.Aircraft take-off devices are known from small sites in which aircraft organs, masts, suspension and delay cables are temporarily carried. In the proposed device, in order to facilitate take-off and protection from falling, said temporary aircraft-carrying organs are provided with supporting surfaces and a tail propeller rotated by means of an ale. ktromotorov.

На чертеже схематически изображено предлагаемое устройство.The drawing schematically shows the proposed device.

На ллощадке А, с которой предполагаетс  подъем самолетов, устанавливаетс  приводимый в действие от мотора л лебедочный аппарат л, один трос г которого , огиба  блок к, укрепленный на мачте а, установленной на той же площадке , крепитс  к поддерживающим поверхност м ti, временно несущего самолет органа о, а другой трос д крепитс  к хвосту того же органа. Упом нутый несущий самолет орган снабжен дл  передвижени  колесами s, электрическими замками ж дл  укреплени  на нем самолета и приводимым во вращение электрическим мотором пропеллером е, служащим дл  удержани  в воздухе несущего самолет органа после вылета из него самолета в.On the platform A, from which the aircraft is supposed to be lifted, a winch device, powered by a motor, is installed, one cable g of which, a skirting block, mounted on the mast, installed on the same platform, is attached to supporting surfaces ti, temporarily bearing the plane of the body is about, and the other cable is attached to the tail of the same body. The aircraft carrying body is equipped with wheels s, electric locks to secure the aircraft on it and a propeller e driven by an electric motor, which serves to hold the aircraft carrying unit in the air after the aircraft leaves it.

Перед вылетом самолет устанавливаетс  на временно несущий орган, укрепл етс  к нему электрическими замками ж и приводитс  в указанное пунктиром на чертеже положение, близкое к мачте а. После этого пускаетс  в ход авио-и электромоторы , которые постепенно увеличивают свою скорость, а в это врем  самолет вместе с несущим органом, помощью тросов гид, удерживаетс  в уаом нутом положении до тех пор, пока моторы не разовьют достаточной дл  подъема и взлета скорости, по достижении каковой тросы сматываютс  с барабана лебедки л и система начинает двигатьс  сначала в горизонтальном положени, а затем, под действием троса «, начнет забирать вверх. Когда самолет, пролет  определенную дистанцию вместе с несущим органом, приобрел способность держатьс  в воздухе , выключаютс  замки ж, и самолет срываетс  с несущего органа и продолжает свой путь, а последний, удерживаемый от полета тросами г, д от действи  пропеллера е, остаетс  подвешенным в воздухе до тех пор, пока лебедка л не вернет его на площадку Л. В этот момент останавливаетс  мотор, вращающий пропеллер е, и несущий самолет орган устайавливаетс  в.новое, исходное положение дл  подъема следующего самолета или ждет в этом положении улетевшего-дл  нового его подъема.Before departure, the aircraft is mounted on a temporarily bearing body, is fixed to it with electric locks and is driven to the position indicated by the dotted line in the drawing, close to the mast a. After that, the air and electric motors, which gradually increase their speed, are floated, and at this time the aircraft, together with the supporting body, using the guide cables, is kept in this position until the motors have developed sufficient speed for lifting and taking off, on reaching which the cables are reeled off the drum of the winch and the system begins to move first in a horizontal position, and then, under the action of the cable, will begin to pick up. When the plane, flying a certain distance together with the main body, acquired the ability to hold air, the locks are turned off, and the plane breaks off the main body and continues its journey, and the latter, kept from flight by cables g, d from the propeller e, remains suspended in until the winch returns it to platform L. At this point, the motor, which rotates the propeller e, stops and the body carrying the aircraft is installed in the new, initial position for raising the next aircraft or waiting in this position flown away, for his new lift.

Предмет патента. Устройство дл  взлета самолета, с применением временно несущего самолеторгана , мачты, подвесных и задерживающих тросов, характеризующеес  тем, что временно несущий самолет орган, в цел х облегчени  взлета, снабжаетс  поддерживающими поверхност ми и хвостовым пропеллером, вращаемым посредством элетромоторов.The subject of the patent. A device for take-off of an aircraft using a temporary aircraft carrier, a mast, suspended and delaying cables, characterized in that the temporary aircraft-carrying organ, in order to facilitate take-off, is provided with supporting surfaces and a tail propeller rotated by electromotors.

ЛL

SU23903A 1927-12-21 1927-12-21 Device for take-off of an aircraft, with the use of an aircraft temporarily carrying an aircraft, a mast of suspension and delay cables SU14574A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU23903A SU14574A1 (en) 1927-12-21 1927-12-21 Device for take-off of an aircraft, with the use of an aircraft temporarily carrying an aircraft, a mast of suspension and delay cables

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU23903A SU14574A1 (en) 1927-12-21 1927-12-21 Device for take-off of an aircraft, with the use of an aircraft temporarily carrying an aircraft, a mast of suspension and delay cables

Publications (1)

Publication Number Publication Date
SU14574A1 true SU14574A1 (en) 1930-03-31

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Family Applications (1)

Application Number Title Priority Date Filing Date
SU23903A SU14574A1 (en) 1927-12-21 1927-12-21 Device for take-off of an aircraft, with the use of an aircraft temporarily carrying an aircraft, a mast of suspension and delay cables

Country Status (1)

Country Link
SU (1) SU14574A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2454355C1 (en) * 2010-11-25 2012-06-27 Александр Афанасьевич Нарижный Method of launching spaceships by reusable system and system for multiple launching of spaceships
RU2537079C2 (en) * 2013-12-20 2014-12-27 Валерий Васильевич Редников Aircraft gravity launcher

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2454355C1 (en) * 2010-11-25 2012-06-27 Александр Афанасьевич Нарижный Method of launching spaceships by reusable system and system for multiple launching of spaceships
RU2537079C2 (en) * 2013-12-20 2014-12-27 Валерий Васильевич Редников Aircraft gravity launcher

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