[go: up one dir, main page]

Greene, 1979 - Google Patents

A wind shear/downdraft drift angle warning system

Greene, 1979

Document ID
12154271731520135053
Author
Greene R
Publication year
Publication venue
Society of Experimental Test Pilots, Technical Review

External Links

Continue reading at scholar.google.com (other versions)

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/006—Safety devices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically
    • B64C29/0008—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded
    • B64C29/0016—Aircraft capable of landing or taking-off vertically having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2700/00—** to be decided **
    • B64D2700/62—** to be decided **
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for

Similar Documents

Publication Publication Date Title
SE8403095D0 (en) WARNING SYSTEM FOR EXTREMELY HIGH SUN SPEED OF AIRPLANE WITH ROTATING WINGS
Greene A wind shear/downdraft drift angle warning system
COLLIN et al. Air navigation in the 1980 s- Proposal of an integrated system
Kranenburg et al. Operational application of the STALINS method for measuring take-off and landing trajectories
PETERS et al. Design considerations for an escape module retrorocket impact attenuation system
HOWELLS Subjective assessment of a helicopter approach system for IFR conditions
Bangen et al. Implementation of flight control in an integrated guidance and control system
SUDDERTH et al. Development of longitudinal handling qualities criteria for large advanced supersonic aircraft[Final Report]
BARANOV et al. Aviation meteorology(Russian book)
HUSICK Technological advancements in general aviation avionics
BERGMAN et al. Control authority with a flight performance controller(development of aircraft system for pilot control of aircraft bank angle and vertical speed)
KIRK et al. An investigation of airborne displays and controls for Search And Rescue(SAR). Volume 9: Project Sea Scanner avionics and sensor system[Final Report, Oct. 1972- Jul. 1973]
CARNEGIS Engine sensory requirements for energy management
Williams Boom probe position error corrections for Sea King Mk 50 flight tests
LEHMAN et al. Simulation and analysis of wind shear hazard(for aircraft landing and takeoff)[Final Report, Jun. 1976- Oct. 1977]
MCCUSKER Cockpit information requirements- Common elements
WUENNENBERG VSTOL aircraft stability and control experienced from methods and results of Do 31 flight tests(Command and control of stability of Do-31 aircraft by landing and hovering)
YANKIN Meteorological safety of aircraft flights(Analysis of meteorological parameters affecting safety of civil aviation and instructions for increased flight safety)
DOETSCH The flight investigation and analysis of longitudinal handling qualities of STOL aircraft on landing approach[Final Report, Jul. 1972- May 1974]
STAATS In flight escape systems for helicopters should be developed to prevent fatalities(Analysis of escape systems for helicopter flight crews and passengers)[Report to the Congress by the Comptroller General of the United States]
SKINNER et al. Airworthiness and flight characteristics evaluation: YAH-1 S improved Cobra agility and maneuverability helicopter[Final Report, 17 Mar.- 17 Apr. 1975]
Wilhelm et al. In-flight investigation of the effects of time delay in control system on flying qualities in landing approach
SHEPARD The variable stability airplane- New tool for flight development and training(Air transport total in-flight simulator/AT/TIFS/ equipped with six degree of freedom variable stability system for aircraft development and pilot training)
Williams et al. Stability and control status for current fighters
GRISARD Automatic approach of helicopters and STOL aircraft