CA2525089A1 - Method and apparatus for assisting a propelled flying object during landing and takeoff - Google Patents
Method and apparatus for assisting a propelled flying object during landing and takeoff Download PDFInfo
- Publication number
- CA2525089A1 CA2525089A1 CA002525089A CA2525089A CA2525089A1 CA 2525089 A1 CA2525089 A1 CA 2525089A1 CA 002525089 A CA002525089 A CA 002525089A CA 2525089 A CA2525089 A CA 2525089A CA 2525089 A1 CA2525089 A1 CA 2525089A1
- Authority
- CA
- Canada
- Prior art keywords
- fluid current
- flying object
- landing
- takeoff
- fluid
- 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
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
- B64F1/36—Other airport installations
Abstract
The invention relates to a method for assisting a propelled flying object during landing and/or takeoff of. For assistance a, related to a landing and/or a takeoff area 10, stationary-generated fluid current is provided in order to introduce energy into the flying object.
The invention likewise relates to an apparatus, which has a fluid current generator 11 for generating the fluid current.
The invention likewise relates to an apparatus, which has a fluid current generator 11 for generating the fluid current.
Claims (23)
1. Method for assisting the landing and/or takeoff of a propelled flying object, said method comprising the provision of a, relative to a landing and/or takeoff area (10), stationary-generated fluid current, in order to introduce energy into the flying object, characterized in that the density of the fluid current is adjusted depending on the situation.
2. Method according to Claim 1, characterized in that the direction of the fluid current is adjusted depending on the situation.
3. Method according to Claim 1, characterized in that the value of at least one further physical parameter of the fluid current is adjusted depending on the situation.
4. Method according to Claim 3, characterized in that the at least one physical parameter comprises at least one of the following parameters: temperature of the fluid current, velocity of the fluid current, homogeneity of the fluid current and laminarity rate of the fluid current.
5. Method according to Claim 1, characterized in that the fluid current provided has a certain specific density and if necessary is enriched by at least one substance of higher specific density.
6. Method according to Claim 1, characterized in that a fire-extinguishing agent is introduced into the fluid current provided.
7. Method according to Claim 1, characterized in that the fluid current provided is a wind generated artificially from the existing atmosphere. a matter stream or a mass flow.
8. Method according to Claim 1, characterized in that to assist the landing of a flying object firstly a fluid current is provided, which is capable of decelerating the flying object, and then a fluid current is provided, which is capable of lowering the flying object from a hovering position onto the landing area (10).
9. Method according to Claim 1, characterized in that to assist the takeoff of a flying object firstly a fluid current is provided, which is capable of lifting the flying object from the takeoff area (10) to a hovering position and then a fluid current is provided, which is capable of accelerating the flying object in a desired direction.
10. Apparatus for assisting the landing and/or takeoff of a propelled flying object, comprising at least one, related to a landing and/or a takeoff area (10), stationary fluid current generator (11), which is designed to provide a fluid current in order to introduce energy into a flying object, characterized in that the fluid current generator is further designed to vary the density of the fluid current provided.
11. Apparatus according to Claim 10, characterized in that the fluid current provided by the fluid current generator (11) can be adjusted.
12. Apparatus according to Claim 10, characterized in that the fluid current generator is designed so as to vary the value of at least one further physical parameter of the fluid current provided.
13. Apparatus according to Claim 10, characterized by a heating element (12) for heating up the fluid current provided.
14. Apparatus according to Claim 10, characterized by a cooling element (12) for cooling down the fluid current provided.
15. Apparatus according to Claim 10, characterized by a substance supply unit (13) for introducing an additional substance into a fluid current provided, wherein the additional substance has a higher specific density than the fluid current provided.
16. Apparatus according to Claim 10, characterized by a fire-extinguishing agent supply unit (13) for introducing a fire-extinguishing agent into the fluid current provide.
17. Apparatus according to Claim 10. characterized in that the at least one fluid current generator comprises at least one blower (11).
18. Apparatus according to Claim 16, characterized in that the at least one blower comprises at least one turbofan (11).
19. Apparatus according to Claim 10, characterized in that the at least one fluid current generator (11) is designed so as to provide as fluid current a wind artificially generated from the existing atmosphere, a matter stream or a mass flow.
20. Apparatus according to Claim 10, characterized by a control device (14) for determining the optimum value of at least one parameter of the fluid current being provided by the at least one fluid current generator and for adjusting this at least one parameter value.
21. Apparatus according to Claim 19, characterized in that the at least one parameter comprises at least one of the following parameters: direction of the fluid current, temperature of the fluid current, density of the fluid current, velocity of the fluid current, homogeneity of the fluid current and laminarity rate of the fluid current.
22. Method for assisting the landing and/or takeoff of a propelled flying object, said method comprising the provision of a, relative to a landing and/or takeoff area (10), stationary-generated fluid current, in order to introduce energy into the flying object, characterized in that the fluid current provided is adjusted such that the flight object takes off in analogy to a low launching of a glider.
23. Apparatus for assisting the landing and/or takeoff of a propelled flying object.
comprising at least one, related to a landing and/or a takeoff area (10), stationary fluid current generator (11), which is designed to provide a fluid current in order to introduce energy into a flying object, characterized in that the fluid current generator is designed to adjust the fluid current such that the flight object takes off in analogy to a tow launching of a glider.
comprising at least one, related to a landing and/or a takeoff area (10), stationary fluid current generator (11), which is designed to provide a fluid current in order to introduce energy into a flying object, characterized in that the fluid current generator is designed to adjust the fluid current such that the flight object takes off in analogy to a tow launching of a glider.
Applications Claiming Priority (7)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE10326144 | 2003-06-06 | ||
| DE10326144.3 | 2003-06-06 | ||
| DE10327743 | 2003-06-18 | ||
| DE10327743.9 | 2003-06-18 | ||
| DE10328292 | 2003-06-23 | ||
| DE10328292.0 | 2003-06-23 | ||
| PCT/EP2004/005642 WO2004108530A1 (en) | 2003-06-06 | 2004-05-26 | Method for supporting a propelled flying object during take-off and/or landing |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2525089A1 true CA2525089A1 (en) | 2004-12-16 |
| CA2525089C CA2525089C (en) | 2012-07-31 |
Family
ID=33514365
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA2525089A Expired - Fee Related CA2525089C (en) | 2003-06-06 | 2004-05-26 | Method and apparatus for assisting a propelled flying object during landing and takeoff |
Country Status (7)
| Country | Link |
|---|---|
| US (1) | US20070029442A1 (en) |
| EP (1) | EP1631494B1 (en) |
| JP (1) | JP4787151B2 (en) |
| AT (1) | ATE375294T1 (en) |
| CA (1) | CA2525089C (en) |
| DE (1) | DE502004005215D1 (en) |
| WO (1) | WO2004108530A1 (en) |
Families Citing this family (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20090236475A1 (en) * | 2008-03-20 | 2009-09-24 | Vonnie Leibow | Lift chamber |
| DE102008054107B3 (en) * | 2008-10-31 | 2010-06-17 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | A method and apparatus for alleviating circulation in the wake after a take-off or landing aircraft |
| US20110004388A1 (en) * | 2009-07-01 | 2011-01-06 | United Technologies Corporation | Turbofan temperature control with variable area nozzle |
| ES2332400B2 (en) | 2009-08-05 | 2011-06-07 | Universidad Politecnica De Madrid | SYSTEM AND METHOD FOR ASSISTING THE EARTHLESS WITHOUT TRACK OF CONVENTIONAL AIRCRAFT OF ALA FIJA. |
| CN102152855B (en) * | 2011-04-29 | 2013-10-16 | 徐州工程学院 | Device special for airplane launch |
| CN102826232B (en) * | 2011-06-17 | 2015-04-22 | 航天信息股份有限公司 | Airplane short-distance sliding take-off and landing system based on RFID (Radio Frequency Identification) technology |
| DE102019205849B4 (en) * | 2019-04-24 | 2021-02-04 | Volkswagen Aktiengesellschaft | Method for carrying out a starting process of an aviation automobile, as well as a system for operating a corresponding aviation automobile |
| DE102020119847B4 (en) | 2020-07-28 | 2022-03-31 | Dr. Ing. H.C. F. Porsche Aktiengesellschaft | Landing platform for an aircraft |
| DE102021000102B8 (en) | 2021-01-10 | 2022-10-27 | Frank Obrist | Autogyro and suitable take-off and landing site for the same |
| US11939082B1 (en) * | 2023-03-22 | 2024-03-26 | United Arab Emirates University | Acoustically enhanced landing pad for ground-effect noise suppression |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US1709058A (en) * | 1926-07-17 | 1929-04-16 | Brunner Frederick | Landing method for aircraft |
| GB343763A (en) * | 1929-03-02 | 1931-02-26 | Roger Beaucaire | A new or improved method of facilitating the starting and landing of aeroplanes and apparatus therefor |
| US1796693A (en) * | 1929-05-31 | 1931-03-17 | D John Schimmel | Means for landing and launching airplanes and the like |
| US2355948A (en) * | 1939-04-14 | 1944-08-15 | Bonstow Thomas Lacey | Method and means for assisting the take-off of landplanes |
| US2383559A (en) * | 1942-01-17 | 1945-08-28 | Henry C Parker | Airplane launching device and carrier |
| US2988308A (en) * | 1958-02-05 | 1961-06-13 | Avro Aircraft Ltd | Vertical propulsion of aircraft |
| US3196822A (en) * | 1962-05-24 | 1965-07-27 | Bertin & Cie | Device for permitting deck landings on an aircraft-carrier in misty or foggy weather |
| US3544044A (en) * | 1968-07-03 | 1970-12-01 | Bernhardt Stahmer | Airport with manufactured surface winds |
| US3771747A (en) * | 1971-07-01 | 1973-11-13 | L Mednikow | Aircraft-landing strip device |
| US4700912A (en) * | 1986-04-24 | 1987-10-20 | Grumman Aerospace Corporation | Laser illumination system for aircraft launch and landing system |
| US5407149A (en) * | 1991-05-30 | 1995-04-18 | Singhai; Tara C. | Devices and means to engage in indoor flight of radio controlled model aircrafts |
| GB9215105D0 (en) * | 1992-07-16 | 1992-08-26 | British Aerospace | Landing of aircraft |
| US6139439A (en) * | 1994-05-11 | 2000-10-31 | Nicholas M. Kavouklis | Means for linearizing an open air flow |
| US5592159A (en) * | 1995-06-30 | 1997-01-07 | Tsai; Yeong-Shyeong | Control system for a flight vehicle |
| US5850988A (en) * | 1996-08-20 | 1998-12-22 | Visidyne, Inc. | Radiosonde balloon launching system |
| GB9824220D0 (en) * | 1998-11-05 | 1999-11-10 | British Aerospace | Aircraft carriers and methods of operation thereof |
| WO2004026687A2 (en) * | 2002-08-20 | 2004-04-01 | Aero Systems Engineering Inc. | Free fall simulator |
-
2004
- 2004-05-26 JP JP2006508204A patent/JP4787151B2/en not_active Expired - Fee Related
- 2004-05-26 CA CA2525089A patent/CA2525089C/en not_active Expired - Fee Related
- 2004-05-26 US US10/559,655 patent/US20070029442A1/en not_active Abandoned
- 2004-05-26 AT AT04734818T patent/ATE375294T1/en not_active IP Right Cessation
- 2004-05-26 WO PCT/EP2004/005642 patent/WO2004108530A1/en active IP Right Grant
- 2004-05-26 DE DE502004005215T patent/DE502004005215D1/en active Active
- 2004-05-26 EP EP04734818A patent/EP1631494B1/en not_active Not-in-force
Also Published As
| Publication number | Publication date |
|---|---|
| EP1631494A1 (en) | 2006-03-08 |
| US20070029442A1 (en) | 2007-02-08 |
| ATE375294T1 (en) | 2007-10-15 |
| CA2525089C (en) | 2012-07-31 |
| DE502004005215D1 (en) | 2007-11-22 |
| EP1631494B1 (en) | 2007-10-10 |
| WO2004108530A1 (en) | 2004-12-16 |
| JP4787151B2 (en) | 2011-10-05 |
| JP2006527117A (en) | 2006-11-30 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed |
Effective date: 20150526 |