GB1169880A - Aircraft having Means to Counteract Displacement of the Aerodynamic Centre - Google Patents
Aircraft having Means to Counteract Displacement of the Aerodynamic CentreInfo
- Publication number
- GB1169880A GB1169880A GB49503/66A GB4950366A GB1169880A GB 1169880 A GB1169880 A GB 1169880A GB 49503/66 A GB49503/66 A GB 49503/66A GB 4950366 A GB4950366 A GB 4950366A GB 1169880 A GB1169880 A GB 1169880A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- aircraft
- wings
- parts
- immovable
- 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
- 238000006073 displacement reaction Methods 0.000 title abstract 2
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C17/00—Aircraft stabilisation not otherwise provided for
-
- 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
- B64C1/0009—Aerodynamic aspects
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
- B64C5/12—Stabilising surfaces adjustable for retraction against or within fuselage or nacelle
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/34—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members
- B64C9/36—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members the members being fuselages or nacelles
-
- 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
-
- 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
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Toys (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
1,169,880. Controlling supersonic aircraft. HAMBERGER FLUGZEUGBAU G.m.b.H. 4 Nov., 1966 [4 Nov., 1965], No. 49503/66. Headings B7G and B7W. An aircraft with immovable swept wings 2 has means for counteracting displacement of the aerodynamic centre on flying through the speed of sound or on altering the supersonic speed of flight, the means comprising front wing parts 3 mounted at the leading edges of the immovable wings, the parts 3 being displaceable in the plane of the wing or rotatable about a transverse axis 12, in which latter case the front wing parts are incorporated in a pivotable nose 11. Each part 3 when movable in the plane of the wing may be either bodily translatable parallel to the leading edge of the wing 2 or pivotable about a vertical axis 6 at the trailing end or at the leading end of the part 3. Various configurations of flaps 3 and wings 2 are shown.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEH0057592 | 1965-11-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1169880A true GB1169880A (en) | 1969-11-05 |
Family
ID=7159812
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB49503/66A Expired GB1169880A (en) | 1965-11-04 | 1966-11-04 | Aircraft having Means to Counteract Displacement of the Aerodynamic Centre |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE1456048A1 (en) |
FR (1) | FR1500579A (en) |
GB (1) | GB1169880A (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH537833A (en) * | 1971-09-17 | 1973-06-15 | U Farner Hans | Method for controlling fixed-wing aircraft |
DE2656692C2 (en) * | 1976-12-15 | 1982-07-29 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Duck plane |
-
1965
- 1965-11-04 DE DE19651456048 patent/DE1456048A1/en active Pending
-
1966
- 1966-11-04 FR FR82584A patent/FR1500579A/en not_active Expired
- 1966-11-04 GB GB49503/66A patent/GB1169880A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
FR1500579A (en) | 1967-11-03 |
DE1456048A1 (en) | 1968-11-14 |
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