GB1044922A - Flying device with double fuselage arrangement - Google Patents
Flying device with double fuselage arrangementInfo
- Publication number
- GB1044922A GB1044922A GB522/64A GB52264A GB1044922A GB 1044922 A GB1044922 A GB 1044922A GB 522/64 A GB522/64 A GB 522/64A GB 52264 A GB52264 A GB 52264A GB 1044922 A GB1044922 A GB 1044922A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuselages
- wing
- jan
- flying device
- hinges
- 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.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
- B64C31/028—Hang-glider-type aircraft; Microlight-type aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/62—Systems for re-entry into the earth's atmosphere; Retarding or landing devices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0018—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only
- B64C2001/0036—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only arranged side by side at the same level
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0045—Fuselages characterised by special shapes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Mechanical Engineering (AREA)
- Tires In General (AREA)
Abstract
1,044,922. Aircraft; space vehicles. JUNKERS FLUGZEUG - UND MOTORENWERKE A.G. Jan. 6, 1964 [Jan. 29, 1963; Jan. 30, 19631, No. 522/64. Heading B7W. A flying device for use in the atmosphere and in space, comprises two fuselages 1 and 2 (Fig. 2), and between them a wing 6 connected to the fuselages. As shown in Fig. 2, the wing 6 is flexible. The fuselages 1<SP>1</SP> and 2<SP>1</SP> (Fig. 4) are hinged to a cabin 5<SP>1</SP> by means of pins 6. Servomotors 7a, 7b and pinions 8a, 8b cause bearing elements 9a, 9b to rotate with hinges 10a, 10b, thus causing the fuselages 1<SP>1</SP>, 2<SP>1</SP> to rotate in opposite directions. Spreading of the fuselages is effected by a telescopic hydraulic booster 11. The booster 11 is connected to the fuselages by way of hinges 12a, 12b and axles 13a, 13b which are rotatably connected to the fuselages. In an embodiment, Figs. 8 to 12 (not shown), the wing is foldable and substantially inflexible and hinged to the fuselages tangentially relative to the fuselage walls.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEJ23067A DE1217791B (en) | 1963-01-29 | 1963-01-29 | Aircraft with a flexible wing area between two carriers |
DEJ23083A DE1228146B (en) | 1963-01-30 | 1963-01-30 | Aircraft with two fuselages that converge like arrows in the direction of flight |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1044922A true GB1044922A (en) | 1966-10-05 |
Family
ID=25982417
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB522/64A Expired GB1044922A (en) | 1963-01-29 | 1964-01-06 | Flying device with double fuselage arrangement |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1044922A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2136514A1 (en) * | 1996-09-06 | 1999-11-16 | Munoz Saiz Manuel | Aircraft and high speed vehicles |
US6957792B2 (en) | 1996-09-06 | 2005-10-25 | Manuel Munoz Saiz | Lifting arrangement for aircraft fuselages |
EP3098162A1 (en) * | 2015-05-26 | 2016-11-30 | Airbus Group SAS | Aircraft with lifting body fuselage |
-
1964
- 1964-01-06 GB GB522/64A patent/GB1044922A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2136514A1 (en) * | 1996-09-06 | 1999-11-16 | Munoz Saiz Manuel | Aircraft and high speed vehicles |
US6957792B2 (en) | 1996-09-06 | 2005-10-25 | Manuel Munoz Saiz | Lifting arrangement for aircraft fuselages |
EP3098162A1 (en) * | 2015-05-26 | 2016-11-30 | Airbus Group SAS | Aircraft with lifting body fuselage |
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