Assessment of Navy Heavy-Lift Aircraft Options
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Development of Modern Control Laws for the AH-64D in Hover/Low Speed Flight
Development of Modern Control Laws for the AH-64D in Hover/Low Speed Flight Jeffrey W. Harding 1 Scott J. Moody Geoffrey J. Jeram 2 Aviation Engineering Directorate U.S. Army Aviation and Missile Research, Development, and Engineering Center Redstone Arsenal, Alabama M. Hossein Mansur 3 Mark B. Tischler Aeroflightdynamics Directorate U.S. Army Aviation and Missile Research, Development, and Engineering Center Moffet Field, California ABSTRACT Modern control laws are developed for the AH-64D Longbow Apache to provide improved handling qualities for hover and low speed flight in a degraded visual environment. The control laws use a model following approach to generate commands for the existing partial authority stability augmentation system (SAS) to provide both attitude command attitude hold and translational rate command response types based on the requirements in ADS-33E. Integrated analysis tools are used to support the design process including system identification of aircraft and actuator dynamics and optimization of design parameters based on military handling qualities and control system specifications. The purpose is to demonstrate the potential for improving the low speed handling qualities of existing Army helicopters with partial authority SAS actuators through flight control law modifications as an alternative to a full authority, fly-by-wire, control system upgrade. NOTATION INTRODUCTION ACAH attitude command attitude hold The AH-64 Apache was designed in the late 70’s and went DH direction hold into service as the US Army’s most advanced day, night DVE degraded visual environment and adverse weather attack helicopter in 1986. The flight HH height hold control system was designed to meet the relevant handling HQ handling qualities qualities requirements based on MIL-F-8501 (Ref. -
National Advisory Committee for Aeronautics
NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS TECHNICAL NOTE 2154 AN ANALYSIS OF TIlE AUTOROTATIVE PERFORMANCE OF A BELICOPTER POWERED BY ROTOR-TIP JET UN[TS By Alfred Gessow Langley Aeronautical Laboratory Langley Air Force Base, Va. Washington July 1950 NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS TECHNICAL NOTE 2l AN ANALYSIS OF THE AUTOROTATIVE PERFORMANCE OF A HELICOPTER POWERED BY ROTOR-TIP JET UNITS By Alfred Gessow SUMMARY The autorotative performance of an assumed helicopter was studied to determine the effect of inoperative jet units located at the rotor- blade tip on the helicopter rate of descent. For a representative ram- jet design, the effect of the jet drag is to increase the minimum rate of descent of the helicopter from about l,OO feet per minute to 3,700 feet per minute when the rotor is operating at a tip speed of approximately 600 feet per second. The effect is less if the rotor operates at lower tip speeds, but the rotor kinetic energy and the stall margin available for the landing maneuver are then reduced. Power-off rates of descent of pulse-jet helicopters would be expected to be less than those of ram- jet.helicopters because pulse jets of current design appear to have greater ratios of net power-on thrust to power-off, drag than currently designed rain jets. Iii order to obtain greater accuracy in studies of autorotative per- forimance, calculations in'volving high power-off rates of descent should include the weight-supporting effect of the fuselage parasite-drag force and the fact that the rotor thrust does not equal the weight of the helicopter. -
Boeing's Mesa Site Is Humming with Apache Production—And That's Not
Boeing’s Mesa site is humming with Apache production—and that’s not all By Eric Fetters-Walp and photos by Bob Ferguson PHOTO: Boeing and U.S. Army aviators put two AH-64D Apache Longbow attack helicopters through their paces over the Arizona desert. NOVEMBER 2011 BOEING FRONTIERS / COVER STORY 21 byMesa the numbers 1 ranking of Boeing Mesa’s business among all Arizona manufacturers 382 acres (155 hectares) comprising the Mesa site 576 number of Boeing suppliers or vendors in Arizona 1982 year Mesa site was established by Hughes Helicopters 4,500 approximate number of employees 8,300 hours volunteered by employees in 2010 he hot desert air above Mesa, making a growing array of components Ariz., frequently pulses with the for multiple Boeing aircraft. 1,900,000 T sound of Apache attack helicop- “We’ve gone from producing Block II ters as the intimidating machines are put Apaches two years ago to having three dollars given by Boeing Mesa and through their paces after emerging from and soon four production lines here today,” employees in charitable contributions the Boeing production line. first of the next-generation Apache Block III said Dave Koopersmith, Boeing Military during 2010 It’s a sound that’s become familiar over production models this fall. The U.S. Army Aircraft’s vice president of Attack Helicopter the nearly 30 years that the Mesa site has plans to order nearly 700 newly built or Programs and Mesa senior site executive, built Apaches for the U.S. Army and a remanufactured Block III helicopters, which referring to the two Apache production 2,000,000 growing number of international customers. -
Over Thirty Years After the Wright Brothers
ver thirty years after the Wright Brothers absolutely right in terms of a so-called “pure” helicop- attained powered, heavier-than-air, fixed-wing ter. However, the quest for speed in rotary-wing flight Oflight in the United States, Germany astounded drove designers to consider another option: the com- the world in 1936 with demonstrations of the vertical pound helicopter. flight capabilities of the side-by-side rotor Focke Fw 61, The definition of a “compound helicopter” is open to which eclipsed all previous attempts at controlled verti- debate (see sidebar). Although many contend that aug- cal flight. However, even its overall performance was mented forward propulsion is all that is necessary to modest, particularly with regards to forward speed. Even place a helicopter in the “compound” category, others after Igor Sikorsky perfected the now-classic configura- insist that it need only possess some form of augment- tion of a large single main rotor and a smaller anti- ed lift, or that it must have both. Focusing on what torque tail rotor a few years later, speed was still limited could be called “propulsive compounds,” the following in comparison to that of the helicopter’s fixed-wing pages provide a broad overview of the different helicop- brethren. Although Sikorsky’s basic design withstood ters that have been flown over the years with some sort the test of time and became the dominant helicopter of auxiliary propulsion unit: one or more propellers or configuration worldwide (approximately 95% today), jet engines. This survey also gives a brief look at the all helicopters currently in service suffer from one pri- ways in which different manufacturers have chosen to mary limitation: the inability to achieve forward speeds approach the problem of increased forward speed while much greater than 200 kt (230 mph). -
Naval Postgraduate School Thesis
NAVAL POSTGRADUATE SCHOOL MONTEREY, CALIFORNIA THESIS A STUDY OF THE RUSSIAN ACQUISITION OF THE FRENCH MISTRAL AMPHIBIOUS ASSAULT WARSHIPS by Patrick Thomas Baker June 2011 Thesis Advisor: Mikhail Tsypkin Second Reader: Douglas Porch Approved for public release; distribution is unlimited THIS PAGE INTENTIONALLY LEFT BLANK REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instruction, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302, and to the Office of Management and Budget, Paperwork Reduction Project (0704-0188) Washington DC 20503. 1. AGENCY USE ONLY (Leave blank) 2. REPORT DATE 3. REPORT TYPE AND DATES COVERED June 2011 Master‘s Thesis 4. TITLE AND SUBTITLE 5. FUNDING NUMBERS A Study of the Russian Acquisition of the French Mistral Amphibious Assault Warships 6. AUTHOR(S) Patrick Thomas Baker 7. PERFORMING ORGANIZATION NAME(S) AND ADDRESS(ES) 8. PERFORMING ORGANIZATION Naval Postgraduate School REPORT NUMBER Monterey, CA 93943-5000 9. SPONSORING /MONITORING AGENCY NAME(S) AND ADDRESS(ES) 10. SPONSORING/MONITORING N/A AGENCY REPORT NUMBER 11. SUPPLEMENTARY NOTES The views expressed in this thesis are those of the author and do not reflect the official policy or position of the Department of Defense or the U.S. -
Aircraft Collection
A, AIR & SPA ID SE CE MU REP SEU INT M AIRCRAFT COLLECTION From the Avenger torpedo bomber, a stalwart from Intrepid’s World War II service, to the A-12, the spy plane from the Cold War, this collection reflects some of the GREATEST ACHIEVEMENTS IN MILITARY AVIATION. Photo: Liam Marshall TABLE OF CONTENTS Bombers / Attack Fighters Multirole Helicopters Reconnaissance / Surveillance Trainers OV-101 Enterprise Concorde Aircraft Restoration Hangar Photo: Liam Marshall BOMBERS/ATTACK The basic mission of the aircraft carrier is to project the U.S. Navy’s military strength far beyond our shores. These warships are primarily deployed to deter aggression and protect American strategic interests. Should deterrence fail, the carrier’s bombers and attack aircraft engage in vital operations to support other forces. The collection includes the 1940-designed Grumman TBM Avenger of World War II. Also on display is the Douglas A-1 Skyraider, a true workhorse of the 1950s and ‘60s, as well as the Douglas A-4 Skyhawk and Grumman A-6 Intruder, stalwarts of the Vietnam War. Photo: Collection of the Intrepid Sea, Air & Space Museum GRUMMAN / EASTERNGRUMMAN AIRCRAFT AVENGER TBM-3E GRUMMAN/EASTERN AIRCRAFT TBM-3E AVENGER TORPEDO BOMBER First flown in 1941 and introduced operationally in June 1942, the Avenger became the U.S. Navy’s standard torpedo bomber throughout World War II, with more than 9,836 constructed. Originally built as the TBF by Grumman Aircraft Engineering Corporation, they were affectionately nicknamed “Turkeys” for their somewhat ungainly appearance. Bomber Torpedo In 1943 Grumman was tasked to build the F6F Hellcat fighter for the Navy. -
E. E. W.M. PE Velocity Animproved Fight Control Method Is Utilized With
US00572.7754A United States Patent (19) 11 Patent Number: 5,727,754 Carter, Jr. 45) Date of Patent: Mar. 17, 1998 (54 GYROPLANE 4,928,907 5/1990 Zuck, 5,301,900 4/1994 Groen et al. ......................... 244,1725 75) Inventor: Jay W. Carter, Jr. Burkburnett, Tex. 5,462,409 10/1995 Frengley et al. ........................ 416/144 Primary Examiner-Galen L. Barefoot 73) Assignee: CarterCopters, L.L.C.. Wichita Falls, Attorney, Agent, or Fi Felsman, Bradley, Gunter & Tex. Dillon, LLP (21) Appl. No.: 521,690 57 ABSTRACT 22 Filed: Aug. 31, 1995 An improved gyroplane having an improved rotor blade (51) int. Clar. inchwith anper edgewise pound of stiffness aircraft gross(E) ofweight at least and 80,000 blade weightspounds (52) 244/8: 244/75 R; 24.4/17.11 of sufficient size to store a minimum of 100 foot pounds of 58) Field of Search .............................. 244/4 R., 6, 7 R. rotational kinetic energy per pound of gross weight of the 244/17.118 gyroplane while the rotor blade pitch is set to minimum lift during blade prerotation. Then a clutch driving the rotor is 56) References Cited disengaged and the rotor blade pitch is changed to a lift U.S. PATENT DOCUMENTS condition to enable the gyroplane to climb to an altitude of at least fifty feet. The speed and thrust of a propeller is D. 172,712 7/1954 Gebhard ................................. D2/335 increased to achieve an increasing a horizontal velocity to D. 178,598 8/1956 Fletcher. P22 maintain altitude, first with the rotor blade providing most of D. -
(12) United States Patent (10) Patent No.: US 8,991,744 B1 Khan (45) Date of Patent: Mar
USOO899.174.4B1 (12) United States Patent (10) Patent No.: US 8,991,744 B1 Khan (45) Date of Patent: Mar. 31, 2015 (54) ROTOR-MAST-TILTINGAPPARATUS AND 4,099,671 A 7, 1978 Leibach METHOD FOR OPTIMIZED CROSSING OF 35856 A : 3. Wi NATURAL FREQUENCIES 5,850,6154. W-1 A 12/1998 OSderSO ea. 6,099.254. A * 8/2000 Blaas et al. ................... 416,114 (75) Inventor: Jehan Zeb Khan, Savoy, IL (US) 6,231,005 B1* 5/2001 Costes ....................... 244f1725 6,280,141 B1 8/2001 Rampal et al. (73) Assignee: Groen Brothers Aviation, Inc., Salt 6,352,220 B1 3/2002 Banks et al. Lake City, UT (US) 6,885,917 B2 4/2005 Osder et al. s 7,137,591 B2 11/2006 Carter et al. (*) Notice: Subject to any disclaimer, the term of this 16. R 1239 sign patent is extended or adjusted under 35 2004/0232280 A1* 11/2004 Carter et al. ............... 244f1725 U.S.C. 154(b) by 494 days. OTHER PUBLICATIONS (21) Appl. No.: 13/373,412 John Ballard etal. An Investigation of a Stoppable Helicopter Rotor (22) Filed: Nov. 14, 2011 with Circulation Control NASA, Aug. 1980. Related U.S. Application Data (Continued) (60) Provisional application No. 61/575,196, filed on Aug. hR". application No. 61/575,204, Primary Examiner — Joseph W. Sanderson • Y-s (74) Attorney, Agent, or Firm — Pate Baird, PLLC (51) Int. Cl. B64C 27/52 (2006.01) B64C 27/02 (2006.01) (57) ABSTRACT ;Sp 1% 3:08: A method and apparatus for optimized crossing of natural (52) U.S. -
Propulsion System Based on Compressed Air Due to Rotor Blade Rotation
International Journal of Smart Grid and Clean Energy Propulsion system based on compressed air due to rotor blade rotation Aiman Elmahmodia*, Nikola Davidovicb, Ramadan A. Al-Madanic a Aeronautical Eng., Faculty of engineering-University of Tripoli, Tripoli - Libya b EDePro Jet Propulsion Laboratory, Begrade, Serbia cEngineering Faculty, Al-Jabel Algharbi University, Tripoli – Libya Abstract The theoretical and experimental investigation of the potential of jet propulsion system to drive rotor of (VTOL) Vertical Takeoff and Landing aircraft has been presented. The analysis of tip jet propulsion system is based on compressed air due to rotor blade rotation. The system performances were compared in the case of the rotor with rocket, and pressure-jet engine. Rocket engine had practical application in middle of 20th century, while the present work tip jet pressure propulsion system is based on turbojet thermodynamic cycle. Comparison has been performed according to available and required power, and to flight duration. Performances of the present propulsion system were also analyzed with introduction of typical rotor geometry. Analysis shows possible application of such propulsion as unmanned or low-weight helicopters and Vertical Take-Off and Landing (VTOL) vehicles. Keywords: Helicopter rotor, tip jet, flying vehicle, unmanned helicopters, pressure jet. Nomenclature ma Air inlet mass flow rate (kg/sec) n number of rotor blades mf Fuel mass flow rate (kg/sec) M payload (Kg) me exit mass flow rate (kg/sec) f fuel – air mixture ratio cpa Specific heat (J/kg.K) P Power (w) Ta Ambient temperature (K) PROT Rotor useful power (w) Csp specific fuel consumption (kg/Nh) Pdrag drag power (w) γ Specific heat ratio F Thrust (N) πr pressure ratio of the rotor blade. -
Model Predictive Control (Mpc) Algorithm for Tip- Jet Reaction Drive
MODEL PREDICTIVE CONTROL (MPC) ALGORITHM FOR TIP- JET REACTION DRIVE SYSTEMS A Thesis Presented to The Academic Faculty by Brian Kestner In Partial Fulfillment of the Requirements for the Degree Doctor of Philosophy in the School of Aerospace Engineering Georgia Institute of Technology December 2009 MODEL PREDICTIVE CONTROL (MPC) ALGORITHM FOR TIP- JET REACTION DRIVE SYSTEMS Approved by: Prof. Dimitri N. Mavris, Advisor Dr. Jimmy Tai School of Aerospace Engineering School of Aerospace Engineering Georgia Institute of Technology Georgia Institute of Technology Dr. Tim Healy Mr. Randy Rosson Gas Turbine Combustion Engineering Gas Turbine Performance Methods General Electric Energy General Electric Energy Prof. Brian German School of Aerospace Engineering Georgia Institute of Technology Date Approved: November 13, 2009 ACKNOWLEDGEMENTS I would like to thank my advisor, Professor Dimitri Mavris, for giving me the opportunity to join the ASDL and pursue my PhD. In addition to providing me with this opportunity, his philosophy towards research was most inspiring. I would like to especially thank Dr. Jimmy Tai for all the support, advice, and help over the last five years. The formulation of this dissertation came out of our weekly meetings. I could not have completed this dissertation without his help. I would like to thank Dr. Tim Healy and Mr. Randy Rosson. The feedback and help provided was always most enlightening, even though it usually took me awhile to realize it. I would to thank Professor Brian German for always keeping an eye on me. To the love of my life, Gina Martell, thank you for being there through all the good and the bad. -
Helicopters in Combat: Methods for Helicopter Use in Special Operations
Review of the Air Force Academy No.1 (36)/2018 HELICOPTERS IN COMBAT: METHODS FOR HELICOPTER USE IN SPECIAL OPERATIONS Ioan MISCHIE Air Force Headquarters, Bucharest, Romania ([email protected]) DOI: 10.19062/1842-9238.2018.16.1.1 Abstract: The world is now marked by conventional and unconventional military actions, from classical armed confrontations, counterinsurgency, counter-terrorism to counter-act trafficking in human beings and drugs. In this wide range of actions, special operations play a particularly important role, solving sensitive issues in order to facilitate the achievement of political goals. These operations always begin with the action of introducing troops into the action area to carry out their missions. Helicopters are, by their characteristics, the means of transportation commonly preferred by commanders who plan and conduct such operations for the purpose of introducing, re-supplying, and extracting troops from the area of action. Keywords: special operations, helicopters, combat methods, high-value targets 1. INTRODUCTION Following World War II, lessons were learned, according to which the support of a classical war would have been costly, both economically and in terms of the loss of human lives, to resolve misunderstandings or confrontations between states, more emphasis has been put on the use of armed forces in atypical ways to carry out the armed struggle. In this way, it was intended to influence the opponent in order to impose its own goals, avoiding an open confrontation between states. In this new type of war, unconventional actions, meant to discredit and isolate the enemy on the international arena, have become increasingly important. -
Northwest District Fire and Aviation Aviation Plan
2019 BLM National Aviation Plan And Colorado State Aviation Plan And Northwest Colorado Fire and Aviation Management Unit Aviation Plan Prepared by: _James Michels________________ Date: __5/22/2019___ James Michels Unit AFMO/Unit Aviation Manager Reviewed by: ___ _____________ Date:_____________ Clark Hammond State Aviation Manager Reviewed by: ________________________________Date:______________ William Colt Mortenson Unit Fire Management Officer Approved by: _________________________________Date:______________ Andrew Archuleta BLM-Northwest District Manager The State Aviation plan, which was distributed via IM that was signed by the Associate State Director. The NWCFAMU will follow the Colorado State Aviation Plan and the National Aviation Plan as it is printed. Any areas that are more specific to NWCFAMU will be noted in red text inserted within the document. This plan was reviewed by the State Aviation Manager and noted that it is not less restrictive than the CO State Aviation Plan and there is no need for the plan to be signed as it is covered under the IM for. The Northwest Colorado Fire and Aviation Management Unit 455 Emerson Street Craig, CO 81625 The Table of Organization for Aviation within NWCFAMU: Unit Fire Management Officer o William Colt Mortenson : . w-(970) 826-5036 . c-(970) 367-6233 . [email protected] Unit Assistant Fire Management Officer/Unit Aviation Manager o James Michels . Meeker w-(970) 878-3821 . Craig w-(970) 826-5012 . c-(970) 749-7399 . [email protected] Cache Manager / SEAT Manager Trainee o Martin Martinez . w-(970) 826-5041 . c-(970) 761-3497 Craig Interagency Dispatch Center o (970) 826-5037 o [email protected] o Aviation Dispatcher Desk .