SE8106271L - Flygplan med arrangemang for montering av en sond - Google Patents
Flygplan med arrangemang for montering av en sondInfo
- Publication number
- SE8106271L SE8106271L SE8106271A SE8106271A SE8106271L SE 8106271 L SE8106271 L SE 8106271L SE 8106271 A SE8106271 A SE 8106271A SE 8106271 A SE8106271 A SE 8106271A SE 8106271 L SE8106271 L SE 8106271L
- Authority
- SE
- Sweden
- Prior art keywords
- probe
- control member
- aircraft
- airplane
- arrangements
- Prior art date
Links
- 239000000523 sample Substances 0.000 abstract 4
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
- B64D39/00—Refuelling during flight
- B64D39/04—Adaptations of hose construction
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C5/00—Stabilising surfaces
- B64C5/10—Stabilising surfaces adjustable
- B64C5/16—Stabilising surfaces adjustable about spanwise axes
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Arrangements For Transmission Of Measured Signals (AREA)
- Length Measuring Devices With Unspecified Measuring Means (AREA)
- Details Of Aerials (AREA)
- Steering Controls (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8034415 | 1980-10-24 |
Publications (2)
Publication Number | Publication Date |
---|---|
SE8106271L true SE8106271L (sv) | 1982-04-25 |
SE443965B SE443965B (sv) | 1986-03-17 |
Family
ID=10516880
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8106271A SE443965B (sv) | 1980-10-24 | 1981-10-23 | Flygplan med arrangemang for montering av en sond |
Country Status (4)
Country | Link |
---|---|
US (1) | US4428549A (sv) |
DE (1) | DE3142135A1 (sv) |
FR (1) | FR2496595A1 (sv) |
SE (1) | SE443965B (sv) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5299455A (en) * | 1992-03-27 | 1994-04-05 | Mangalam Siva M | Method and instrumentation system for measuring airspeed and flow angle |
US5616861A (en) * | 1995-06-07 | 1997-04-01 | Rosemount Aerospace Inc. | Three pressure pseudo -Δ-P sensor for use with three pressure air data probe |
US5753505A (en) * | 1995-07-06 | 1998-05-19 | Emory University | Neuronal progenitor cells and uses thereof |
AU2001239948A1 (en) * | 2000-03-09 | 2001-09-17 | Rosemount Aerospace Inc. | Integrated probe and sensor system |
US6609421B2 (en) * | 2001-05-08 | 2003-08-26 | Rosemount Aerospace Inc. | Sideslip correction for a multi-function three probe air data system |
ES2394558B1 (es) * | 2010-01-18 | 2013-12-12 | Eads Construcciones Aeronáuticas, S.A. | Dispositivo de soporte para sonda. |
CN105620774B (zh) * | 2014-10-28 | 2017-09-26 | 哈尔滨飞机工业集团有限责任公司 | 一种机翼外端探杆的角度调节机构 |
US11765494B2 (en) * | 2019-12-31 | 2023-09-19 | Zipline International Inc. | Acoustic probe array for aircraft |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB676430A (en) * | 1949-04-01 | 1952-07-30 | Flight Refueling Ltd | Improvements in apparatus for towing and refuelling aircraft in flight |
GB874845A (en) * | 1957-03-07 | 1961-08-10 | Hispano Aviacion S A | Means for controlling the stability of an aircraft |
US3585859A (en) * | 1969-05-26 | 1971-06-22 | Rosemount Eng Co Ltd | Aerodynamically compensated static pressure tube |
DE2831185C2 (de) * | 1978-07-15 | 1983-03-03 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Leitwerksflächen eines Luftfahrzeuges |
-
1981
- 1981-10-23 FR FR8119960A patent/FR2496595A1/fr active Granted
- 1981-10-23 SE SE8106271A patent/SE443965B/sv not_active IP Right Cessation
- 1981-10-23 US US06/314,416 patent/US4428549A/en not_active Expired - Fee Related
- 1981-10-23 DE DE19813142135 patent/DE3142135A1/de not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
DE3142135A1 (de) | 1982-06-09 |
FR2496595A1 (fr) | 1982-06-25 |
US4428549A (en) | 1984-01-31 |
FR2496595B1 (sv) | 1985-05-10 |
SE443965B (sv) | 1986-03-17 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE69228762D1 (de) | Mit einem blockierbaren freiflügel ausgerüstetes flugzeug | |
DE3762027D1 (de) | Fluegelklappensteuersystem eines flugzeuges. | |
DE3576318D1 (de) | Ultraleichtflugzeug mit freilaufendem starrfluegel. | |
IT1098083B (it) | Dispositivo di carenatura atto alla riduzione della resistenza aerodinamica in veicoli articolati o simili | |
IL86840A (en) | Flutter exciter for testing of aircraft wings | |
SE8106271L (sv) | Flygplan med arrangemang for montering av en sond | |
NO803025L (no) | Styremekanisme for halerotorens stigningsforstillingsanordning ved et helikopter med foldbar halerotorpylon | |
SE7807995L (sv) | Navigationssystem for ett flygplan, som er utrustat med en autopilot | |
DE3775190D1 (de) | Flugzeug. | |
GR890100336A (el) | Ταχυπλοον σκαφος. | |
RU1828444C (ru) | Дирижабль | |
WOLOWICZ | Free wing assembly for an aircraft[Patent] | |
GB987792A (en) | Improvements in and relating to aircraft wings | |
IT7921057A0 (it) | Timone per la generazione aerodinamica di momenti su aeroplani. | |
SU582629A2 (ru) | Механизм отклонения аэродинамической поверхности крыла летательного аппарата | |
Gravelle | Active flutter control in transonic conditions | |
SE7901512L (sv) | Ringformig vinge | |
BOLDING et al. | The design, analysis and testing of a low budget wind tunnel flutter model with active aerodynamic controls, volume 2[Final Report, 1 Dec. 1970- 30 Nov. 1975] | |
MAITA et al. | Powered lift aerodynamics of USB STOL aircraft(Upper Surface Blowing) | |
BETZINA | Force and moment data from a wind-tunnel test of a tilt-nacelle V/STOL propulsion system with an attitude control vane(conducted in Ames 40 by 80 foot wind tunnel) | |
SU845350A1 (ru) | Летательный аппарат артемова о.а. | |
SANDLIN | Wind tunnel tests of a free-wing/free-trimmer model[Final Report] | |
WOLOWICZ et al. | Longitudinal aerodynamic characteristics of light, twin-engine, propeller-driven airplanes(Analytical procedures and design data for predicting stability and control characteristics of light, propeller-driven aircraft) | |
GB1534483A (en) | Overhead device for propelling a boat | |
DESTUYNDER | Wing buffeting active control testing on a transport aircraft configuration in a large sonic windtunnel |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |
Ref document number: 8106271-3 Effective date: 19880627 Format of ref document f/p: F |