USD616805S1 - Co-flow jet aircraft - Google Patents

Co-flow jet aircraft Download PDF

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Publication number
USD616805S1
USD616805S1 US29320424 US32042408F USD616805S US D616805 S1 USD616805 S1 US D616805S1 US 29320424 US29320424 US 29320424 US 32042408 F US32042408 F US 32042408F US D616805 S USD616805 S US D616805S
Authority
US
Grant status
Grant
Patent type
Design
Prior art keywords
fig
view
jet
flow
aircraft
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.)
Active
Application number
US29320424
Inventor
Gecheng Zha
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.)
University of Miami
Original Assignee
University of Miami
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
Grant date

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Description

FIG. 1 is a front perspective view of a co-flow jet aircraft, showing my new design;

FIG. 2 is a top view thereof;

FIG. 3 is a bottom view thereof;

FIG. 4 is a first side view thereof;

FIG. 5 is a second side view thereof;

FIG. 6 is a front view thereof; and,

FIG. 7 is a rear view thereof.

The broken lines show the unclaimed portions of the jet that form no part of the claimed design.

Claims (1)

  1. The ornamental design for a co-flow jet aircraft, as shown and described.
US29320424 2004-08-20 2008-06-26 Co-flow jet aircraft Active USD616805S1 (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US6405305 true 2005-02-23 2005-02-23
PCT/US2007/010122 WO2008054518A3 (en) 2006-04-28 2007-04-24 Emissionless silent and ultra-efficient airplane using cfj airfoil
US12119193 US8262031B2 (en) 2004-08-20 2008-05-12 Co-flow jet aircraft
US29320424 USD616805S1 (en) 2005-02-23 2008-06-26 Co-flow jet aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29320424 USD616805S1 (en) 2005-02-23 2008-06-26 Co-flow jet aircraft

Publications (1)

Publication Number Publication Date
USD616805S1 true USD616805S1 (en) 2010-06-01

Family

ID=42200562

Family Applications (1)

Application Number Title Priority Date Filing Date
US29320424 Active USD616805S1 (en) 2004-08-20 2008-06-26 Co-flow jet aircraft

Country Status (1)

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US (1) USD616805S1 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100270424A1 (en) * 2009-04-24 2010-10-28 Delaurier James D Hybrid airship
USD738438S1 (en) * 2014-04-29 2015-09-08 Kma Concepts Limited Swept wing airplane projectile
USD807809S1 (en) * 2015-07-07 2018-01-16 Kabushiki Kaisha Bellsion Aircraft
USD807966S1 (en) * 2016-05-03 2018-01-16 Flavio Manzoni Toy space ship
USD813143S1 (en) * 2016-11-04 2018-03-20 Aerovironment, Inc. Vertical take-off and landing (VTOL) winged air vehicle with complementary angled rotors
USD813956S1 (en) * 2016-10-27 2018-03-27 Horizon Hobby, LLC Flying wing

Non-Patent Citations (22)

* Cited by examiner, † Cited by third party
Title
Anders, S., et al., "Active Flow Control Activities at NASA Langley", AIAA 2004-2623, Jun. 2004.
Bradley, L.C., "An Experimental Investigation of a Sting-Mounted Finite Circulation Control Wing", M.S. Thesis, Air Force Institute of Technology, Dec. 1995.
Brown, G., et al., "On Density Effects and Large Scale Structure in Turbulent Mixing Layers", Journal of Fluid Mechanics, vol. 64, Part 4, pp. 775-816, 1974.
Englar, R., et al., "Test Techniques for High Lift, Two-Dimensional Airfoils with Boundary Layer and Circulation Control for Application to Rotary Wing Aircraft", Canadian Aeronautics and Space Journal, vol. 19, No. 3, pp. 93-108, Mar. 1973.
Englar, R.J., "Circulation Control for High Lift and Drag Generation on Stol Aircraft", Journal of Aircraft, vol. 12,No. 5, pp. 457-463, May 1975.
Englar, R.J., "Circulation Control Pneumatic Aerodynamics: Blown Force and Moment Augmentation and Modifications; Past, Present and Future", AIAA 2000-2541, Jun. 2000.
Englar, R.J., et al., "Application of Circulation Control to Advanced Subsonic Transport Aircraft, Part I: Airfoil Development", Journal of Aircraft, vol. 31, No. 5, pp. 1160-1168, Oct. 1994.
Englar, R.J., et al., "Application of Circulation Control to Advanced Subsonic Transport Aircraft, Part II: Transport Application", Journal of Aircraft, vol. 31, No. 5, pp. 1169-1177, Oct. 1994.
Englar, R.J., et al., "STOL Potential of the Circulation Control Wing for 'High-Performance Aircraft," Journal of Aircraft, vol. 14, No. 3, pp. 175-181, Mar. 1978.
International Search Report dated Oct. 3, 2009 for International Application No. PCT/US07/10122.
Johari, H., et al., "Visualization of Pulsed Vortex Generator Jets for Active Control of Bounday Layer Separation", AIAA 97-2021, 1997.
Kibens, V., et al., "An Overview of Active Flow control Applications at the Boeing Company", AIAA 2004-2624, Jun. 2004.
Liu, Y, et al., "Computational Evaluation of the Steady and Pulsed Jet Effects on the Performance of a Circulation Control Wing Section", AIAA 2004-56, 2004.
McManus, K., et al., "Airfoil Performance Enhancement Using Pulsed Jet Separation Control", AIAA 97-1971, 1997.
McManus, K., et al., "Separation Control in Incompressible and Compressible Flows Using Pulsed Jets", AIAA 96-1948, 1996.
Miller, D., et al., "Aerodynammic Flowfield Control Technologies for Highly Integrated Airframe Propulsion Flowpaths", AIAA 2004-2625, Jun. 2004.
Strykowski, P., et al., "The Effect of Counterflow on the Development of Compressible Shear Layers", Journal of Fluid Mechanics, vol. 308, pp. 63-69, 1996.
Tilmann, C.P., et al., "Flow Control Research and Applications at the AFRL's Air Vehicles Directorate", AIAA 2004-2622, Jun. 2004.
Wood, N., et al., "Circulation Control Airfoils Past, Present, Future", AIAA 85/0204, 1985.
Wood, N., et al., "Control of Asymmetric Vorticial Flows over Delta Wings at High Angle of Attack", Journal of Aircraft, vol. 27, No. 5, pp. 429-435, May 1990.
Wood, N., et al., "Control of Vortical Lift on Delta Wings by Tangential Leading-Edge Blowing", Journal of Aircraft, vol. 25, No. 3, pp. 236-243, Mar. 1988.
Wygnanski, I., "The Variables Affecting the Control Separation by Periodic Excitation", AIAA 2004-2505, Jun. 2004.

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20100270424A1 (en) * 2009-04-24 2010-10-28 Delaurier James D Hybrid airship
USD738438S1 (en) * 2014-04-29 2015-09-08 Kma Concepts Limited Swept wing airplane projectile
USD807809S1 (en) * 2015-07-07 2018-01-16 Kabushiki Kaisha Bellsion Aircraft
USD807966S1 (en) * 2016-05-03 2018-01-16 Flavio Manzoni Toy space ship
USD813956S1 (en) * 2016-10-27 2018-03-27 Horizon Hobby, LLC Flying wing
USD813143S1 (en) * 2016-11-04 2018-03-20 Aerovironment, Inc. Vertical take-off and landing (VTOL) winged air vehicle with complementary angled rotors

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