GB1492109A - Aircraft flight monitoring apparatus - Google Patents

Aircraft flight monitoring apparatus

Info

Publication number
GB1492109A
GB1492109A GB26781/75A GB2678175A GB1492109A GB 1492109 A GB1492109 A GB 1492109A GB 26781/75 A GB26781/75 A GB 26781/75A GB 2678175 A GB2678175 A GB 2678175A GB 1492109 A GB1492109 A GB 1492109A
Authority
GB
United Kingdom
Prior art keywords
aircraft
angle
june
monitoring apparatus
aircraft flight
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
Application number
GB26781/75A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Bodenseewerk Geratetechnik GmbH
Original Assignee
Bodenseewerk Geratetechnik GmbH
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 Bodenseewerk Geratetechnik GmbH filed Critical Bodenseewerk Geratetechnik GmbH
Publication of GB1492109A publication Critical patent/GB1492109A/en
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/06—Measuring arrangements specially adapted for aerodynamic testing
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING OR COUNTING
    • G06G—ANALOGUE COMPUTERS
    • G06G7/00—Devices in which the computing operation is performed by varying electric or magnetic quantities
    • G06G7/48—Analogue computers for specific processes, systems or devices, e.g. simulators
    • G06G7/70—Analogue computers for specific processes, systems or devices, e.g. simulators for vehicles, e.g. to determine permissible loading of ships, centre of gravity, necessary fuel

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • Theoretical Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • Mathematical Physics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Measuring Arrangements Characterized By The Use Of Fluids (AREA)
  • Measuring Fluid Pressure (AREA)

Abstract

1492109 Determining uplift of aircraft BODENSEEWERK GERATETECHNIK GmbH 24 June 1975 [27 June 1974] 26781/75 Heading G1N The lift coefficient of an aircraft is derived from measurements of the pressure head, the surface pressure of a lifting surface and the angle of the control flaps, which measurement signals are combined in a computer network in accordance with empirically derived formulae. Further equations and corresponding computer sections produce signals representing the angle of incidence of the aircraft and its weight. The equations used are modified when the aircraft is not in straight-line flight to take into account the bank angle and vertical acceleration.
GB26781/75A 1974-06-27 1975-06-24 Aircraft flight monitoring apparatus Expired GB1492109A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2430805A DE2430805C3 (en) 1974-06-27 1974-06-27 Device for determining the aerodynamic flow condition of an aircraft equipped with wings

Publications (1)

Publication Number Publication Date
GB1492109A true GB1492109A (en) 1977-11-16

Family

ID=5919057

Family Applications (1)

Application Number Title Priority Date Filing Date
GB26781/75A Expired GB1492109A (en) 1974-06-27 1975-06-24 Aircraft flight monitoring apparatus

Country Status (3)

Country Link
DE (1) DE2430805C3 (en)
FR (1) FR2276573A1 (en)
GB (1) GB1492109A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3930854A1 (en) * 1989-09-15 1991-03-28 Cestmir Sebesta Stalling speed danger warning appts. for pilot - has electronic unit evaluating dynamic air pressures picked-up from two positions on aircraft
CN112693626A (en) * 2021-03-23 2021-04-23 中国空气动力研究与发展中心低速空气动力研究所 Control surface angle sheet applied to wind tunnel test model and installation method

Also Published As

Publication number Publication date
FR2276573B1 (en) 1980-08-14
DE2430805C3 (en) 1982-03-18
DE2430805A1 (en) 1976-01-15
FR2276573A1 (en) 1976-01-23
DE2430805B2 (en) 1981-07-02

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee