WO2019088952A3 - An aerodynamic load test system - Google Patents

An aerodynamic load test system Download PDF

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Publication number
WO2019088952A3
WO2019088952A3 PCT/TR2018/050337 TR2018050337W WO2019088952A3 WO 2019088952 A3 WO2019088952 A3 WO 2019088952A3 TR 2018050337 W TR2018050337 W TR 2018050337W WO 2019088952 A3 WO2019088952 A3 WO 2019088952A3
Authority
WO
WIPO (PCT)
Prior art keywords
control component
movement
force
control
test system
Prior art date
Application number
PCT/TR2018/050337
Other languages
French (fr)
Other versions
WO2019088952A2 (en
Inventor
Ali AKCAY
Onur IMECE
Sabri SENTURK
Nihat Serkan AKCAY
Original Assignee
Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi
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 Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi filed Critical Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi
Publication of WO2019088952A2 publication Critical patent/WO2019088952A2/en
Publication of WO2019088952A3 publication Critical patent/WO2019088952A3/en

Links

Classifications

    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00—Simulators for teaching or training purposes
    • G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • G09B9/28—Simulation of stick forces or the like
    • 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

Abstract

The aerodynamic load test system developed by the present invention and suitable for use in testing the endurance of the control components (A), which guide the movement of the air by rotating, against the aerodynamic forces, comprising at least one control element (B) which simulates the first force applied by the assembly, enabling the movement of the control component (A), to the control component (A) and is suitable for connecting to the control component (A) so as to enable the movement of the control component (A) in a direction by rotating. The test system also comprises the surface loading system (7) which provides to apply a second force, being in the opposite direction of the first force, to the control component (A) and simulates this second force, wherein this surface loading system (7) comprises: the movement assembly (1) which forms rotational movement opposite to the movement direction of the control component (A) when the control component (A) is moved via the control element (B) so as to rotate in a direction; the counter force element (3) in connection with the control component (A) via the connecting component (4) at one side, and which connects to the movement assembly (1) at one side, which makes the control component (A) move in opposite direction of its movement, and by this way enables to apply the second force to the control component (A) in opposite direction of the first force; and the first transfer element (2) which enables the connection between the counter force element (3) and the movement assembly (1).
PCT/TR2018/050337 2017-07-03 2018-07-02 An aerodynamic load test system WO2019088952A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
TR2017/09721A TR201709721A2 (en) 2017-07-03 2017-07-03 An Aerodynamic Load Test System
TR2017/09721 2017-07-03

Publications (2)

Publication Number Publication Date
WO2019088952A2 WO2019088952A2 (en) 2019-05-09
WO2019088952A3 true WO2019088952A3 (en) 2019-07-25

Family

ID=66331458

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/TR2018/050337 WO2019088952A2 (en) 2017-07-03 2018-07-02 An aerodynamic load test system

Country Status (2)

Country Link
TR (1) TR201709721A2 (en)
WO (1) WO2019088952A2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115326350B (en) * 2022-10-14 2022-12-27 中国空气动力研究与发展中心高速空气动力研究所 Motor-driven wind tunnel jet test equivalent simulation device and application method thereof
CN117571249B (en) * 2024-01-15 2024-04-05 中国空气动力研究与发展中心高速空气动力研究所 Wind tunnel test angle limiting device convenient to adjust and application method thereof

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2937730A1 (en) * 2008-10-27 2010-04-30 Airbus France Movable element's e.g. aileron, rotation angle adjusting device for use during testing of aircraft model in wind tunnel, has actuator acting on element's axis moved with respect to fixed axis, and remote control unit arranged on gear motor
WO2013100767A1 (en) * 2011-12-28 2013-07-04 De Kroes Jan Louis Subsonic plane or flight simulator thereof, adjustable fuselage control surface, computer program product and method
CN204166725U (en) * 2014-10-10 2015-02-18 西京学院 A kind of analogue means of simple and easy aircraft drive system

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2808659A (en) 1954-07-22 1957-10-08 Dehmel Richard Carl Control loading simulating apparatus for flight trainers

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2937730A1 (en) * 2008-10-27 2010-04-30 Airbus France Movable element's e.g. aileron, rotation angle adjusting device for use during testing of aircraft model in wind tunnel, has actuator acting on element's axis moved with respect to fixed axis, and remote control unit arranged on gear motor
WO2013100767A1 (en) * 2011-12-28 2013-07-04 De Kroes Jan Louis Subsonic plane or flight simulator thereof, adjustable fuselage control surface, computer program product and method
CN204166725U (en) * 2014-10-10 2015-02-18 西京学院 A kind of analogue means of simple and easy aircraft drive system

Also Published As

Publication number Publication date
TR201709721A2 (en) 2019-01-21
WO2019088952A2 (en) 2019-05-09

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