SE8106271L - Flygplan med arrangemang for montering av en sond - Google Patents

Flygplan med arrangemang for montering av en sond

Info

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
Application number
SE8106271A
Other languages
Unknown language ( )
English (en)
Other versions
SE443965B (sv
Inventor
D P Halliday
J F Riley
B Sharrock
Original Assignee
British Aerospace
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by British Aerospace filed Critical British Aerospace
Publication of SE8106271L publication Critical patent/SE8106271L/sv
Publication of SE443965B publication Critical patent/SE443965B/sv

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D39/00Refuelling during flight
    • B64D39/04Adaptations of hose construction
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C5/00Stabilising surfaces
    • B64C5/10Stabilising surfaces adjustable
    • B64C5/16Stabilising 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)
SE8106271A 1980-10-24 1981-10-23 Flygplan med arrangemang for montering av en sond SE443965B (sv)

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)

* Cited by examiner, † Cited by third party
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)

* Cited by examiner, † Cited by third party
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

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