GB973384A - Improvements in or relating to a device for measuring angle of attack of aircraft wings - Google Patents
Improvements in or relating to a device for measuring angle of attack of aircraft wingsInfo
- Publication number
- GB973384A GB973384A GB16814/63A GB1681463A GB973384A GB 973384 A GB973384 A GB 973384A GB 16814/63 A GB16814/63 A GB 16814/63A GB 1681463 A GB1681463 A GB 1681463A GB 973384 A GB973384 A GB 973384A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wing
- vane
- attack
- axis
- angle
- 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
- 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
- B64D43/02—Arrangements or adaptations of instruments for indicating aircraft speed or stalling conditions
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Length Measuring Devices With Unspecified Measuring Means (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US191899A US3190115A (en) | 1962-05-02 | 1962-05-02 | Angle of attack measuring device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB973384A true GB973384A (en) | 1964-10-28 |
Family
ID=22707365
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB16814/63A Expired GB973384A (en) | 1962-05-02 | 1963-04-29 | Improvements in or relating to a device for measuring angle of attack of aircraft wings |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3190115A (enExample) |
| JP (1) | JPS527240B1 (enExample) |
| GB (1) | GB973384A (enExample) |
Families Citing this family (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3604259A (en) * | 1969-05-02 | 1971-09-14 | Rosemount Eng Co Ltd | Angle of attack measuring device with adjustable airfoil |
| JPS5617090U (enExample) * | 1979-07-16 | 1981-02-14 | ||
| JPS5617091U (enExample) * | 1979-07-16 | 1981-02-14 | ||
| JPS6067799U (ja) * | 1983-10-14 | 1985-05-14 | 行司 泉 | 伸縮ポ−ル |
| US5583289A (en) * | 1994-08-19 | 1996-12-10 | Airguide Instrument Company | Marine velocity detection device with channel to wash out debris |
| US5544076A (en) * | 1994-08-19 | 1996-08-06 | Airguide Instrument Company | Marine speedometer |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2337753A (en) * | 1941-02-24 | 1943-12-28 | Ralph D Lacoe | Airplane stall and high-speed indicating apparatus |
| US2478967A (en) * | 1944-05-12 | 1949-08-16 | Greene Leonard | Stall warning device for airplanes |
| GB707167A (en) * | 1951-07-16 | 1954-04-14 | Nat Res Dev | Improvements relating to stall indicating or like devices for aircraft |
| US2818730A (en) * | 1955-08-05 | 1958-01-07 | G M Giannini & Co Inc | Retractable aircraft instrument |
-
1962
- 1962-05-02 US US191899A patent/US3190115A/en not_active Expired - Lifetime
-
1963
- 1963-04-29 GB GB16814/63A patent/GB973384A/en not_active Expired
- 1963-05-02 JP JP38022466A patent/JPS527240B1/ja active Pending
Also Published As
| Publication number | Publication date |
|---|---|
| US3190115A (en) | 1965-06-22 |
| JPS527240B1 (enExample) | 1977-03-01 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB973384A (en) | Improvements in or relating to a device for measuring angle of attack of aircraft wings | |
| US3604259A (en) | Angle of attack measuring device with adjustable airfoil | |
| GB1100970A (en) | Linear air-speed sensor | |
| US3045353A (en) | Direct reading computer | |
| GB660854A (en) | Improvements in stall warning device for airplanes | |
| GB1045554A (en) | Rotary wing aircraft | |
| GB1191720A (en) | Aerodynamic Obturator Device for a Variable Geometry Aircraft | |
| GB748797A (en) | Method of and apparatus for determining and adjusting the aerodynamic pitching moment of a full-sized rotary aerodynamic member | |
| GB680565A (en) | Improvements in or relating to instruments for indicating measuring or recording themach number of an airstream | |
| GB702289A (en) | Improved means for detecting aircraft stall conditions | |
| US3670569A (en) | Flight measuring apparatus | |
| GB937024A (en) | Arrangement for preventing icing at air intakes or like apertures in aircraft | |
| JORDAN | Exact solution for lifting surfaces(Development of numerical analysis techniques for determining lifting surface characteristics of circular wings and parabolic wing tips) | |
| GB596608A (en) | Improvements relating to air speed measuring and indicating arrangements | |
| GB825446A (en) | Improvements in rotary wing aircraft | |
| Klein et al. | A proposal for a self-contained instrumentation system for flight research on stability and control | |
| GB785633A (en) | Improvements in aircraft having a variable wing area | |
| GB1276956A (en) | Apparatus for indicating the liquid level in a container | |
| GB675087A (en) | Airspeed indicator | |
| GB1069086A (en) | Improvements relating to airflow direction indicators | |
| TAKASAWA | On the pitch damping moment in hovering of a rigid helicopter rotor(Analysis of pitch damping moment for hovering helicopter rotary wing and development of formula for calculating pitch damping derivative) | |
| GB707167A (en) | Improvements relating to stall indicating or like devices for aircraft | |
| GB1019673A (en) | Improvements in or relating to helicopter rotors | |
| MELICK | Analysis of inlet flow distortion and turbulence effects on compressor stability(Effect of steady state circumferential total pressure distortion on loss in compressor stall pressure ratio) | |
| GB701844A (en) | Improved means for detecting disturbed flow over aircraft surfaces or for stall warning |