DK2500261T3 - Linseformet luftskib og tilknyttede kontrolenheder - Google Patents
Linseformet luftskib og tilknyttede kontrolenheder Download PDFInfo
- Publication number
- DK2500261T3 DK2500261T3 DK12171556.9T DK12171556T DK2500261T3 DK 2500261 T3 DK2500261 T3 DK 2500261T3 DK 12171556 T DK12171556 T DK 12171556T DK 2500261 T3 DK2500261 T3 DK 2500261T3
- Authority
- DK
- Denmark
- Prior art keywords
- airship
- power source
- control
- thrust
- propulsion
- Prior art date
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/24—Arrangement of propulsion plant
- B64B1/30—Arrangement of propellers
- B64B1/34—Arrangement of propellers of lifting propellers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64B—LIGHTER-THAN AIR AIRCRAFT
- B64B1/00—Lighter-than-air aircraft
- B64B1/06—Rigid airships; Semi-rigid airships
- B64B1/36—Arrangement of jet reaction apparatus for propulsion or directional control
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/042—Initiating means actuated personally operated by hand
- B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Automation & Control Theory (AREA)
- Toys (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Mechanical Control Devices (AREA)
- Variable-Direction Aerials And Aerial Arrays (AREA)
Claims (15)
1. Linseformet luftskib, der omfatter et system til styring af giring, hvilket system omfatter: én eller flere vertikale styringsoverflader (350), der fortrinsvis omfatter et ror, forbundet med luftskibet; en første strømkilde (533) og en anden strømkilde (534), der hver er konfigureret til at tilvejebringe en uafhængigt variabel thrust forbundet med luftskibet; en giringsstyring (241), f.eks. en pedalaktuator (240, 242), konfigureret til at modtage et input, der indikerer en ønsket giringvinkel, kendetegnet ved, at en styreenhed (600) er kommunikationsmæssigt forbundet med giringsstyringen (241), den ene eller flere vertikale styringsoverflader (350) og den første og den anden strømkilde (533, 534), ved, at den første og anden strømkilde (533, 534) er uafhængigt drejbare for at variere retningen af den thrust, de frembringer, ved, at den første strømkilde (533) befinder sig i en position 120 grader fra næsen af luftskibet og den anden strømkilde (534) befinder sig i en negativ position på 120 grader fra næsen af luftskibet, og ved, at styreenheden er konfigureret til at modtage et udgangssignal fra giringsstyringen (241) svarende til den ønskede giringsvinkel og til at generere et styresignal konfigureret til at ændre en tilstand forbundet med den ene eller flere vertikale styringsoverflader (350), den første strømkilde (533) og den anden strømkilde (534), således at luftskibet i det væsentlige opnår den ønskede giringsvinkel.
2. Linseformet luftskib ifølge krav 1, hvor giringsstyringen omfatter to drejende pedalaktuatorer (240, 242), der er placeret i en position i en gondol (35), der er forbundet med luftskibet for således at kunne nås med en operatørs fødder.
3. Linseformet luftskib ifølge krav 1, hvor den ene eller flere styringsoverflader omfatter et ror (350), der er operativt koblet til et haleparti (25) forbundet med luftskibet.
4. Linseformet luftskib ifølge krav 3, hvor roret (350) er konfigureret til at dreje i en højre retning eller en venstre retning i forhold til en midterlinje af luftskibet.
5. Linseformet luftskib ifølge krav 4, hvor styresignalet er konfigureret til at bevirke, at roret drejer i den venstre retning eller den højre retning.
6. Linseformet luftskib ifølge krav 1, hvor styresignalet er konfigureret til at øge thrust fra den første strømkilde og reducere thrust fra den anden strømkilde eller til at øge thrust fra den anden strømkilde og reducere thrust fra den første strømkilde.
7. Linseformet luftskib ifølge krav 1, hvor styreenheden endvidere er konfigureret til at: modtage informationer, der indikerer aktuelle egenskaber relateret til luftskibets aktuelle flyvning; sammenligne de aktuelle egenskaber med et forhåndsbestemt sæt af foretrukne egenskaber og automatisk generere styresignalet baseret på sammenligningen.
8. Fremgangsmåde til styring af giring forbundet med et linseformet luftskib, der indbefatter en første strømkilde (533), en anden strømkilde (534) og en vertikal styringsoverflade (350), hvilken fremgangsmåde omfatter: modtagelse, fra en giringsstyring, af et signal, der indikerer en ønsket giringvinkel for luftskibet, kendetegnet ved, at den første strømkilde (533) befinder sig i en position 120 grader fra næsen af luftskibet og den anden strømkilde (534) befinder sig i en negativ position på 120 grader fra næsen af luftskibet, og ved, at fremgangsmåden indbefatter bestemmelse af en driftstilstand forbundet med den første strømkilde (533) og den anden strømkilde (534) og den vertikale styringsoverflade (350) og ændring af den driftstilstand, der er forbundet med den første strømkilde, den anden strømkilde og den vertikale styringsoverflade for at få luftskibet til at opnå den ønskede giringsvinkel.
9. Fremgangsmåde ifølge krav 8, der endvidere omfatter aktivering af én eller flere pedaler (240, 242) forbundet med giringsstyringen for at indikere den ønskede giringsvinkel.
10. Fremgangsmåde ifølge krav 8, hvor ændringen omfatter tilvejebringelse af et styresignal baseret på den driftstilstand, der er forbundet med den første strømkilde (533), den anden strømkilde (534) og den vertikale styringsoverflade (350), og den ønskede giringsvinkel.
11. Fremgangsmåde ifølge krav 10, hvor ændring af den driftstilstand, der er forbundet med den vertikale styringsoverflade (350), omfatter drejning af et ror, fortrinsvis i forhold til et haleparti forbundet med luftskibet.
12. Fremgangsmåde ifølge krav 11, hvor drejningen udføres i en højre retning eller en venstre retning i forhold til en midterlinje af luftskibet, baseret på den ønskede giringsvinkel.
13. Fremgangsmåde ifølge krav 12, hvor styresignalet er konfigureret til at få roret til at dreje i den venstre retning eller i den højre retning.
14. Fremgangsmåde ifølge krav 8, hvor ændringen endvidere omfatter ændring af thrust forbundet med den første strømkilde (533) og ændring af thrust forbundet med den anden strømkilde (534), for eksempel Øgning af thrust fra den første strømkilde og reduktion af thrust fra den anden strømkilde eller øgning af thrust fra den anden strømkilde og reduktion af thrust fra den første strømkilde.
15. Fremgangsmåde ifølge krav 8, der endvidere omfatter modtagelse af informationer, der indikerer en aktuel egenskab forbundet med en aktuel flyvning for luftskibet; sammenligning af de aktuelle egenskaber med et forhåndsbestemt sæt af foretrukne egenskaber og automatisk generering af et styresignal baseret på sammenligningen.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US93538307P | 2007-08-09 | 2007-08-09 | |
EP08827387.5A EP2173613B1 (en) | 2007-08-09 | 2008-08-07 | Lenticular airship and associated controls |
Publications (1)
Publication Number | Publication Date |
---|---|
DK2500261T3 true DK2500261T3 (da) | 2017-07-17 |
Family
ID=40208729
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DK12171556.9T DK2500261T3 (da) | 2007-08-09 | 2008-08-07 | Linseformet luftskib og tilknyttede kontrolenheder |
DK12171557.7T DK2511173T3 (da) | 2007-08-09 | 2008-08-07 | Linseformet luftskib og tilknyttede kontrolenheder |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DK12171557.7T DK2511173T3 (da) | 2007-08-09 | 2008-08-07 | Linseformet luftskib og tilknyttede kontrolenheder |
Country Status (17)
Country | Link |
---|---|
US (4) | US8297550B2 (da) |
EP (4) | EP2500262A1 (da) |
CN (4) | CN102774498B (da) |
AU (1) | AU2008287518B2 (da) |
CA (3) | CA3062083A1 (da) |
CY (1) | CY1119307T1 (da) |
DK (2) | DK2500261T3 (da) |
EA (2) | EA024007B1 (da) |
ES (3) | ES2465622T3 (da) |
HK (1) | HK1140988A1 (da) |
HR (1) | HRP20170914T1 (da) |
HU (1) | HUE034865T2 (da) |
LT (1) | LT2500261T (da) |
PL (1) | PL2500261T3 (da) |
PT (1) | PT2500261T (da) |
SI (1) | SI2500261T1 (da) |
WO (1) | WO2009023114A2 (da) |
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US9139287B2 (en) * | 2012-06-26 | 2015-09-22 | Hamilton Sundstrand Corporation | Propeller blade with carbon foam spar core |
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