WO2023156817A1 - Autonomous jet platform for takeoff and landing of flying vehicles with no landing gear - Google Patents
Autonomous jet platform for takeoff and landing of flying vehicles with no landing gear Download PDFInfo
- Publication number
- WO2023156817A1 WO2023156817A1 PCT/IB2022/051371 IB2022051371W WO2023156817A1 WO 2023156817 A1 WO2023156817 A1 WO 2023156817A1 IB 2022051371 W IB2022051371 W IB 2022051371W WO 2023156817 A1 WO2023156817 A1 WO 2023156817A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- landing
- engines
- takeoff
- platform
- jet
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/14—Space shuttles
Definitions
- the invention relates to rocket and space technology. Reusable space systems.
- spacecraft This is a special kind of aircraft designed to fly into space, while it takes off and lands like an airplane.
- For takeoff and landing, such a device needs a landing gear.
- the spacecraft landing gear mechanism is an important structural element, but it is used only during takeoff and landing, and nevertheless, included in the spacecraft design, it is also launched into space. This is extra weight.
- the present invention aims to overcome this disadvantage. It is a structure in the form of a double frame, inside which there are fuel tanks and a control system. On the sides are jet engines. The control of the structure is achieved by deflecting the engines themselves, or by deflecting the thrust vector if the engines are fixed motionless.
- ARP autonomous jet platform
- ARP autonomous rocket platform
- Landing using ARP looks like this.
- the spacecraft spacecraft enters the atmosphere, slows down (slows down) to a certain speed.
- the ARP rises to the required height and moves to the meeting point. Docking occurs, the ARP connects to the spacecraft from below and delivers it to the landing site.
Abstract
An autonomous jet platform (AJP) is designed for the takeoff and landing of flying vehicles that do not have landing gear. It is a structure consisting of a rigid double frame with jet engines arranged along the sides thereof. Within the frame are fuel tanks and a control system. The control system is based on deflection of the jet thrust of the engines, or of the engines themselves, using a thrust vector. The number of engines depends on the size and weight of the vehicle to be lifted and the payload capacity of the platform and can vary (from 4 or more). For takeoff, the AJP is positioned beneath a spacecraft and lifts the latter to the required height using the thrust of its own engines, at the same time (if necessary) accelerating the vehicle to the required speed. The platform then disconnects and returns to the desired location. In the case of landing, the AJP performs airborne docking (recovery) with a vehicle having no landing gear, whereupon the structure executes a landing.
Description
Автономная реактивная платформа для взлета и посадки воздушных аппаратов без шасси Autonomous jet platform for takeoff and landing of aircraft without landing gear
Изобретение относится к ракетно космической технике. Многоразовые космические системы .В настоящее время существует множество проектов орбитального самолета (космолета ) . Это особого рода самолет предназначенный для полетов в космос , при этом он взлетает и садится по самолетному типу. Для взлета и посадки подобному аппарату необходимо шасси . Механизм шасси космолета важный элемент конструкции ,но используется только при взлете и посадке , и тем не менее включенный в конструкцию космолета он так же выводится в космос .Это лишний вес . Данное изобретение призвано устранить этот недостаток . Представляет собой конструкцию в виде двойной рамы , внутри которой находятся топливные баки и система управления .По сторонам — реактивные двигатели .Управление конструкцией достигается отклонением самих двигателей , либо отклонением вектора тяги , если двигатели закреплены неподвижно . The invention relates to rocket and space technology. Reusable space systems. Currently, there are many projects for an orbital aircraft (spacecraft). This is a special kind of aircraft designed to fly into space, while it takes off and lands like an airplane. For takeoff and landing, such a device needs a landing gear. The spacecraft landing gear mechanism is an important structural element, but it is used only during takeoff and landing, and nevertheless, included in the spacecraft design, it is also launched into space. This is extra weight. The present invention aims to overcome this disadvantage. It is a structure in the form of a double frame, inside which there are fuel tanks and a control system. On the sides are jet engines. The control of the structure is achieved by deflecting the engines themselves, or by deflecting the thrust vector if the engines are fixed motionless.
Если использовать автономную реактивную платформу (АРП ) не только в качестве заменителя шасси ( только помогая взлету и посадке любого аппарата ) ,но и для разгона какого либо аппарата — то можно дополнительно придать конструкции аэродинамическую форму . If you use an autonomous jet platform (ARP) not only as a chassis substitute (only helping to take off and land any device), but also to accelerate any device, then you can additionally give the structure an aerodynamic shape.
Взлет с АРП ( автономная реактивная платформа ) выглядит так : АРП располагается снизу космолета и работой своих двигателей поднимает его в воздух на необходимую высоту .После чего отсоединяется и возвращается к месту взлета . Takeoff from the ARP (autonomous rocket platform) looks like this: ARP is located below the spacecraft and the operation of its engines lifts it into the air to the required height. After that, it disconnects and returns to the take-off site.
Посадка с использованием АРП выглядит так .Космический аппарат ( космолет ) входит в атмосферу , сбрасывает скорость ( тормозит ) до определенной скорости .В это время АРП поднимается на необходимую высоту и перемещается в место встречи .Происходит стыковка , АРП снизу соединяется с космолетом и доставляет его в место посадки . Landing using ARP looks like this. The spacecraft (spacecraft) enters the atmosphere, slows down (slows down) to a certain speed. At this time, the ARP rises to the required height and moves to the meeting point. Docking occurs, the ARP connects to the spacecraft from below and delivers it to the landing site.
Преимущества данной схемы перед традиционными ( с использованием шасси закрепленном на аппарате ) .Отсутствие шасси существенно облегчает конструкцию космолета .Позволяет уменьшить запас топлива . Позволяет использовать любое место для взлета и посадки .Не требуется взлетно посадочная полоса .Может использоваться как на суше так и на море .
The advantages of this scheme over traditional ones (using a chassis mounted on the spacecraft). The lack of a chassis greatly facilitates the spacecraft design. Allows you to use any place for takeoff and landing. No runway required. Can be used both on land and at sea.
Claims
2 2
ФОРМУЛА ИЗОБРЕТЕНИЯ CLAIM
Конструкция в виде прямоугольной рамы имеющая по сторонам реактивные двигатели .Предназначена для взлета (подъема ) и посадки воздушного аппарата не имеющего шасси .Управляется отклонением направления реактивной тяги .
Design in the form of a rectangular frame with jet engines on the sides. Designed for takeoff (lifting) and landing of an aircraft without a landing gear. Controlled by jet thrust direction deviation.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/IB2022/051371 WO2023156817A1 (en) | 2022-02-16 | 2022-02-16 | Autonomous jet platform for takeoff and landing of flying vehicles with no landing gear |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/IB2022/051371 WO2023156817A1 (en) | 2022-02-16 | 2022-02-16 | Autonomous jet platform for takeoff and landing of flying vehicles with no landing gear |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2023156817A1 true WO2023156817A1 (en) | 2023-08-24 |
Family
ID=87577656
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/IB2022/051371 WO2023156817A1 (en) | 2022-02-16 | 2022-02-16 | Autonomous jet platform for takeoff and landing of flying vehicles with no landing gear |
Country Status (1)
Country | Link |
---|---|
WO (1) | WO2023156817A1 (en) |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5667167A (en) * | 1994-09-02 | 1997-09-16 | Kistler Aerospace Corporation | Methods and apparatus for reusable launch platform and reusable spacecraft |
RU2355600C1 (en) * | 2007-10-12 | 2009-05-20 | Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") | Water-jet propeller |
US8498756B1 (en) * | 2011-08-18 | 2013-07-30 | The United States of America as Represented by the Adminstrator of the National Aeronautics & Space Administration (NASA) | Movable ground based recovery system for reuseable space flight hardware |
CN108860638A (en) * | 2018-05-08 | 2018-11-23 | 赵凤银 | It is slided with efficient short distance or the platform-type jet runway of VTOL aircraft device |
RU199914U1 (en) * | 2020-02-19 | 2020-09-28 | Общество с ограниченной ответственностью "БЕСПИЛОТНЫЕ СИСТЕМЫ" | Takeoff and landing platform for unmanned aerial vehicles |
-
2022
- 2022-02-16 WO PCT/IB2022/051371 patent/WO2023156817A1/en unknown
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5667167A (en) * | 1994-09-02 | 1997-09-16 | Kistler Aerospace Corporation | Methods and apparatus for reusable launch platform and reusable spacecraft |
RU2355600C1 (en) * | 2007-10-12 | 2009-05-20 | Федеральное государственное унитарное предприятие "Московское машиностроительное производственное предприятие "САЛЮТ" (ФГУП "ММПП "САЛЮТ") | Water-jet propeller |
US8498756B1 (en) * | 2011-08-18 | 2013-07-30 | The United States of America as Represented by the Adminstrator of the National Aeronautics & Space Administration (NASA) | Movable ground based recovery system for reuseable space flight hardware |
CN108860638A (en) * | 2018-05-08 | 2018-11-23 | 赵凤银 | It is slided with efficient short distance or the platform-type jet runway of VTOL aircraft device |
RU199914U1 (en) * | 2020-02-19 | 2020-09-28 | Общество с ограниченной ответственностью "БЕСПИЛОТНЫЕ СИСТЕМЫ" | Takeoff and landing platform for unmanned aerial vehicles |
Non-Patent Citations (1)
Title |
---|
ANONYMOUS: "AUTONOMOUS SPACEPORT DRONE SHIP", WWW.HISOUR.COM, 23 April 2020 (2020-04-23), pages 1 - 8, XP093087596, Retrieved from the Internet <URL:http://web.archive.org/web/20200423180708/https://www.hisour.com/autonomous-spaceport-drone-ship-43244> [retrieved on 20231002] * |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US10124890B2 (en) | Modular nacelles to provide vertical takeoff and landing (VTOL) capabilities to fixed wing aerial vehicles, and associated systems and methods | |
US8528853B2 (en) | In-line staged horizontal takeoff and landing space plane | |
US8403254B2 (en) | Aero-assisted pre-stage for ballistic rockets and aero-assisted flight vehicles | |
US8498756B1 (en) | Movable ground based recovery system for reuseable space flight hardware | |
EA037795B1 (en) | Aircraft with vertical takeoff and landing and method of operating same | |
AU3443589A (en) | Rocket-powered, air-deployed, lift-assisted booster vehicle for orbital, supraorbital and suborbital flight | |
CN103097246A (en) | Salvaging and braking device for objects flying freely in space | |
US20070215751A1 (en) | Asymmetrical VTOL UAV | |
CN106288980A (en) | A kind of three grades of vehicles and usings method thereof of based on RBCC power | |
US8168929B2 (en) | Non-powered, aero-assisted pre-stage for ballistic rockets and aero-assisted flight vehicles | |
US3302908A (en) | Unmanned flying machine | |
US3114520A (en) | Stabilization and control system for pilotless, vertical take-off and landing aircraft | |
CN202439843U (en) | Flying disk aircraft | |
WO2023156817A1 (en) | Autonomous jet platform for takeoff and landing of flying vehicles with no landing gear | |
CN111959824A (en) | Heavy reusable aerospace vehicle system with space-based launching | |
CN114194387B (en) | Coaxial anti-oar double-rotor type sky removes runway | |
CN103253372A (en) | Flying saucer spacecraft | |
CN109018341A (en) | It is a kind of can launch mission load land and water landing unmanned plane | |
CN103832582A (en) | Multifunctional helicopter | |
RU2309087C2 (en) | Missile carrier "vityaz" for horizontal takeoff without takeoff run at low-temperature gliding in atmosphere and soft landing | |
DE102014019398A1 (en) | Returning launching device for a space rocket and the launching process | |
RU2730300C9 (en) | Device for mass delivery of tourists to stratosphere and subsequent return to ground | |
RU2731518C1 (en) | Device for accelerated delivery of passengers to intercontinental distances | |
RU2715816C1 (en) | Accelerating carrier aircraft (versions) | |
RU2342288C1 (en) | Method of servicing cosmic articles and shuttle aerospace system for its implementation |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 22926926 Country of ref document: EP Kind code of ref document: A1 |