Jet Engines – The New Masters of Advanced Flight Control

References

1. Gal-Or, Benjamin. BEIJING, Invited Keynote Lecture; 3rd Int’l Conf. ISIAF, Chinese Academy of Sciences, Beijing, China, Sept. 2, 1996.Search in Google Scholar

2. Gal-Or, Benjamin. MOSCOW, Invited Plenary Lecture, “Civilizing Military Thrust Vectoring Flight Control to Maximize Civil Transport Safety”, 5th Int´l Symp. Aero Sci., Moscow Russia, Proceeding, TsAGI, 1999.Search in Google Scholar

3. Gal-Or, Benjamin. WARSAW, Invited opening Keynote Lecture, “Civilizing Military Thrust Vectoring Flight Control to Maximize Air Safety, 2nd Int’l Seminar on Aeronautics & Education, Poland, Nov. 25, 1996.Search in Google Scholar

4. UNITED STATES AIR FORCE & NATO, RTO-EN-12. 2000-2001 REVIEW published in Germany, U.S., UK and JAPAN: “Benjamin Gal-Or & Wolfgang Herbst have influenced the direction of fighter aircraft design.”Search in Google Scholar

5. “AVIATION WEEK & Space Technology”. (i) “When the Rubber Leaves the Road”, Jan. 12, 379, 1998; (ii) “(MILITARY) THRUST VECTOR CONTROL EYED FOR TRANSPORT”, Aug. 28, 1995.Search in Google Scholar

6. Gal-Or, Benjamin. Civilizing military thrust vectoring flight control. AEROSPACE AMERICA, April, 1996.Search in Google Scholar

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20. Gal-Or, Benjamin. Editorial: “Future Jet Technologies; Sensitive Thrust-Vectoring & Stealth Technology Transfers to South Korea and Japan Expose Lack of JES-Stealth-Drones R&D”. Int J Turbo Jet-Engines. 2014;31(4):277–85, 285–90, ISSN (Online) 2191-0332, ISSN 0334-0082, e-ISSSN 2191-0332; DOI:10.1515/tjj-2014-1001.Search in Google Scholar

21. Gal-Or, Benjamin. Editorial: “Global Needs for Jet-Engine-Steered (JES) Strike Drones vs. Lack of Updated Textbooks to Design 6th Generation UCLASS Due to UCAV Failure”. 2016;33(2):143–49.Search in Google Scholar

22. Gal-Or, Benjamin. Optimizing sub-critical-flow thrust-vectoring of converging-diverging nozzles. AIAA J Propulsion Power. 2000;16:202–06.10.2514/2.5584Search in Google Scholar

23. Gal-Or, Benjamin. “Upgraded, Completely Vectored F-22”, USAF-AFOSR-EOARD, CONTRACT F61708-92-W, Report Date: Feb. 28, 1993.Search in Google Scholar

24. Gal-Or, Benjamin. Vectored propulsion, supermaneuverability and Robot Aircraft. Springer Verlag, N.Y. and Heidelberg, ISBN 0387-97161-0, 3-540-87161-0, TL685.3.G23 1989, 629.I34ʹ353-de20, 89-21797. Copyrights Holder: Benjamin Gal-Or, This worldwide acclaimed book was defined “LANDMARK BOOK” in its FOREWORD by the UNITED STATES AIR FORCE CHIEF SCIENTIST. The book reviews 237 prior art references and 182 drawings that prove that state-protected, IPA-78402 [31] protects private top military secrets developed from 1968 to 1986 in total confidentiality as STEALTH JET-ENGINE STEERING (“JES”), or “Stealth 3D Thrust Vectoring” trade secrets that had neither been available nor invented in the USA prior to August 25, 1986, when, in response to US defense contractor Boeing’s June 24, 1986 invitation, were imported to BOEING, the USG and Boeing’s “third parties” PWA, Lockheed Martin and to a thousand of Boeing’s additional subcontractors during its 1986-1990 efforts to eventually win the $67 Billion F-22 Raptor Program under deferred payments for said IP importing under co-signed contract “Proprietary Information Agreement” (“PIA”) AND internationally protected by IPA 78402 [31].10.1007/978-1-4613-8961-3Search in Google Scholar

25. Gal-Or, Benjamin et al. UNITED STATES PATENT 5,782,431 “THRUST VECTORING/REVERSING”, 1998. The invention provides alternative flight control methods and structures which can prevent a crash of a passenger or a cargo aircraft under stall/spin and adverse flight conditions, failing Traditional Aerodynamic Flight Control, (“TAFC”), asymmetric icing, loss of one or more jet engines, pilot errors and strong side winds. That air-safety capability is provided by integrating roll-yaw-pitch engine-nozzle-nacelle 3D thrust vectoring flight control by retractable/rotatable vane-doors, collectively operated in individual JES-sectors, door-structures in one method or with novel retractable/rotatable TR vane-door sectorial structures. The methods and structures are intended for transport jets, except one configuration which is intended for turbo-prop transports. Another configuration replaces heavy and complex conventional TR doors and TR-nacelle-grids with an integrated, simpler and lighter JES/TR-systems.Search in Google Scholar

26. Gal-Or, Benjamin. Re-educating jet-engines-researchers to stay relevant. Int’l J Turbo Jet Engines. 2016;33(2):143–49.10.1515/tjj-2016-5001Search in Google Scholar

27. Gal-Or, Benjamin. Thrust vectoring: theory, laboratory, and flight tests. AIAA J Propulsion Power. 1993;9:51–58.10.2514/3.11484Search in Google Scholar

28. Gal-Or, Benjamin. Editorial: “Global Needs for Jet-Engine-Steered (JES) Strike Drones vs. Lack of Updated Textbooks to Design 6th Generation UCLASS Due to UCAV Failure”. Int’l J Turbo Jet Engines. 2016;33(2):143–49.Search in Google Scholar

29. Gal-Or, Benjamin. Optimizing sub-critical-flow thrust-vectoring of converging-diverging nozzles. AIAA J Propulsion Power. 2000;16:202–06.10.2514/2.5584Search in Google Scholar

30. ABRAHAM M. S. GOO. BOEING’s Military Airplanes Company’s president on June 24, 1986 extended a formally written invitation to import-contract state-protected JES-STEALTH PROTOTYPES defined by IPA 78402. The contract was signed on August 25, 1986 in Kansas, at Boeing’s Military Facilities. A Classified, 7-Page Import-Contract was immediately shared with The United States Government and Boeing’s Third Parties, Lockheed Martin and General Dynamics, Forth Worth, TX, Pratt and Whitney, FL. and with thousands of subcontractors for immediate adaptation of the so imported JES-STEALTH design trade secrets and flight testing trade secrets information also on computer programs, thus allowing Boeing and its Third Parties to win the $67 billion ATF program, later known as the F-22 Raptor program.Search in Google Scholar

31. Gal-Or, Benjamin. sole IP private owner of State Protected 1968–1986 confidential classified top trade secrets protected by a Collective Title: “Un-piloted aircraft or a stealth cruise missile”, IPA 78402, Filed on April 2, 1986 in Jerusalem Patent Office. State-ordered to be split into additional derivatives: Derivative-I Title: “Control system for jet-propelled air vehicles and spacecraft” IPA 80532; November 7, 1986, December 20, 1993, Derivative-II Title: “unmanned aircraft or cruise missile with minimal thermal signature” IPA106,145, June 25, 1993; December 20, 1993; Derivative-III Title: “Vectored air inlet for stealth drone or cruise missile” IPA106,165; June 29, 1993, December 20, 1993.Search in Google Scholar

32. Gal-Or, Benjamin. First ever, proof of concept flight testing [33] by First-Time Flight Testing in the History of Aviation of post-stall JES-STEALTH air vehicles – conducted at Megiddo Airfield, Israel. Flight tests performed with JES-STEALTH tail-less, first-ever in the deep post-stall domain (up to 170 Angle-of-Attack) via first YAW-PITCH-ROLL flight simulations of post-stall WVR-type Combat Maneuvers with and without resorting to TAFC.Search in Google Scholar

33. AVIATION WEEK. “Israelis Flight Test Jet-Powered RPV Fitted With Thrust Vectoring Nozzles”, May 18, p. 21, 1987; May 30, 1987. “ISRAEL FLIES VECTORING RPV”, FLIGHT INT’L, May 30, 1987; “Israel”, “RPVs”, JANE’S ALL THE WORLD’S AIRCRAFT. 1987.Search in Google Scholar

34. Gal-Or, Benjamin. “Novel, Post-Stall, Thrust-Vectored F-15 RPVs: Laboratory and Flight Tests” Funded by the US Air Force, 1990, 188 pages, (Canarded and Canard-less F-15 1/7-scaled prototypes were tested to refute TAFC- opposition in the USAF, DOD, USN, NASA, DARPA and, during the next 30 years, in Russia, China, Japan, Israel and India, while the EU is still canard-arrested.).Search in Google Scholar

35. Gal-Or, Benjamin. “Tailless Vectored Fighters: Theory, Laboratory and Flight Tests”, USAF, 196 pages, July 15, 1991.Search in Google Scholar

36. Gal-Or, Benjamin. “Vectorable Inlets/Nozzles and Tailless Flying Models vs. Pilot’s Tolerances Affecting Maximum Post-Stall Vectoring Agility”, USAF, 238 pages.Search in Google Scholar

37. Gal-Or, Benjamin. “Tailless Vectored Fighters: Theory, Laboratory and Flight Tests”, USAF, WPAFB, Ohio, USA, AFOSR FY 1456-8905052, 196 pages, July 15, 1991.Search in Google Scholar

38. Gal-Or, Benjamin. “Dynamic Scaling, Pilot v. G-Loads under post-stall Maneuvers with vectored fighters”, Funded series of projects by U.S. AIR FORCE; E. g., (i) San Antonio, BAFB, 1990, USAF Colonel J. Tedor team; (ii) “Dynamic Scaling of Prototypes Using Radius of Gyration Method: Theory, Laboratory and Flight Tests”, REPORT #I to USAF Capt. J. Wigle (Sep. 30, 1991); (iii) REPORT #II to USAF Dr. D. W. Repperger, AL/WPAFB (Sep. 30, 1991); (iv) Report to USAF Col. J. Tedor, Deputy Director, Human Systems Division, BAFB, TX; USAF Special Project, SPC-91-4003, AF/AFOSR/EOARD, 141 pages; Classified Reports to Lockheed-Martin/General Dynamics, Ft Worth, TX, via Spence E. Peters, Tel. 817-935-1588, Main: 817-777-2000, E-Mail: Spence.e.pters@LMCO.com and Dorsett, both had maintained mutual visits during the longest cooperation programs in which all imports to SACOM/JES/STVS imported technologies were inter alia provided to Lockheed Martin/GD up to about 1997.Search in Google Scholar

39. Gal-Or, Benjamin. Classified Reports to PWA, Manager, Component Technology, R. E. (Bob) Davis, 1987–1994.Search in Google Scholar

40. Gal-Or, Benjamin. Classified Reports to General Electric, Aircraft Engines to Don Dunbar, Ed Rogala and GE VP Krebs. 1987–1988.Search in Google Scholar

41. Gal-Or, Benjamin. Agility Benefits of Integrated Aerodynamic & Thrust Vectoring Control, GD/Lockheed-Martin RFP Ref. TECH-RRJ-JK-0001, TIIT-TRDF 160–779, 1993–1995, Progress Report No. 2, Feb. 10, 1995.Search in Google Scholar

42. THE UNITED STATES Government Accounting Office (“GAO”). October 25, 2016: Commonality exists between B-21’s PWA Engine and F-35/F-135 engine; 145 B-21 units are needed to complete this $80 billion program. GAO-16-389R, March 24, 2016; GAO: RQ-180 design influences B-21 (LRS-B) and associated advanced air-launched cruise missile, strike missiles. [RQ-180 is only nominally replacing the LM RQ-170 captured by Iran. GAO-15-374: Air-defense: DOD debates UCLASS high-profile design under the original mission vs. a low-profile proposal by the outgoing Government, a debate that has delayed UCLASS development by 3 years, from 2014 to 2017. US Secretary of Defense at an earlier time, Robert Gates, stated the need for pilotless next-generation bomber option. GAO, August 2005: DOD awarded GE & Rolls-Royce $2.4 billion contract to develop the F136 engine as alternative for the F-35/PWA Engine. LM Conceptual designs of a new JES STVS FB-22 Bomber includes adaptation of GE F136 or PWA F135 jet engines. Multi Axis No Tail (JES-Stealth) X-44 MANTA influences the new designs. Cf. Figures 1 to 7.Search in Google Scholar