AIRCRAFT FLIGHT CHARACTERISTIC MEASUREMENT

• US 20160091362A1
• Filed: 09/29/2014
• Published: 03/31/2016
• Est. Priority Date: 09/29/2014
• Status: Abandoned Application

• Current Assignee: Aeroacoustic Method, LLC
• Original Assignee: Aeroacoustic Method, LLC
• Inventors: Schmitz, Fredric H., Koushik, N. Sudarshana, Sickenberger, Richard D., Eckert, William T.
• Application Number:
  US14/500,681
• Publication Number:
  US 20160091362A1
• Time in Patent Office: Days
• US Class Current: 1/1
• CPC Class Codes: G01H 3/00 Measuring characteristics of vibrations by using a detector in a fluid G01H7/00, G01H9/00, G01H11/00 take precedence
• CPC Class Codes: G01M 17/00 Testing of vehicles testing fluid tightness G01M3/00; testing elastic properties of bodies or chassis, e.g. torsion-testing, G01M5/00; testing alignment of vehicle headlight devices G01M11/06; testing of engines G01M15/00

Abstract

A method and device of measuring external flight characteristics of aircraft, including fixed-wing, rotorcraft, and Unmanned Aerial Vehicles, utilizes one or more floating platforms, each supporting one or more measuring instruments. The floating platform may be a hot air balloon, dirigible or other quasi-neutrally-buoyant airship, untethered to avoid interference between the aircraft being measured and any tether. Measurement of rotorcraft acoustic characteristics is particularly enhanced by permitting measurements that account for directionality of noise sources and are not affected by wind or reflected noise.

Claims

1. A method for measuring aircraft external flight characteristics, comprising the steps of:

a. supporting a measuring instrument by a platform floating in air,

b. flying an aircraft in proximity to said instrument, and

c. using said instrument to measure flight characteristics of said aircraft.

2. A method according to claim 1, wherein said measuring instrument comprises a sound measuring device for measuring sound waves.

3. A method according to claim 1, wherein said platform comprises an untethered hot air balloon.

4. A method according to claim 1, wherein said platform comprises an untethered dirigible.

5. A method according to claim 1, further comprising:

d. determining relative positions of said platform and said aircraft and

e. analyzing effect of said relative positions on measured flight characteristics.

6. A method according to claim 5, wherein relative positions of said platform and said aircraft are determined by using digital global positioning system.

7. A method according to claim 1, further comprising a plurality of measuring instruments supported by said platform.

8. A method according to claim 1, further comprising a plurality of floating platforms, each supporting at least one measuring instrument.

9. A method according to claim 1, in which measurement of flight characteristics is not affected by wind.

10. A device for measuring aircraft external flight characteristics of an aircraft, comprising:

a. measuring instrument for measuring flight characteristics of ah aircraft,

b. platform floating in air, and

c. support means for supporting said measuring instrument by said platform.

11. A device for measuring aircraft external flight characteristics according to claim 10, wherein said measuring instrument comprises a sound measuring device for measuring sound waves.

12. A device for measuring aircraft external flight characteristics according to claim 10, wherein said platform comprises an untethered hot air balloon.

13. A device for measuring aircraft external flight characteristics according to claim 10, wherein said platform comprises an untethered dirigible.

14. A device for measuring aircraft external flight characteristics according to claim 10, further comprising:

d. means for determining relative positions of said platform and said aircraft and

e. means for analyzing effect of said relative positions on measured flight characteristics.

15. A device for measuring aircraft external flight characteristics according to claim 10, further comprising global positioning system inertial navigation unit supported by said platform.

16. A device for measuring aircraft external flight characteristics according to claim 10, further comprising a plurality of measuring instruments supported by said platform.

17. A device for measuring aircraft external flight characteristics according to claim 10, further comprising a plurality of floating platforms, each supporting at least one measuring instrument.

18. A device for measuring aircraft external flight characteristics according to claim 10, in which measurement of flight characteristics is not affected by wind.