| 词条 | Baldwin Mono Tiltrotor | |||||||
| 释义 |
The Baldwin Mono Tiltrotor project is a research effort into a tiltrotor aircraft that uses only one rotor. Like other tiltrotor configurations, the mono tiltrotor combines the vertical lift capability and structural efficiency of a helicopter with the speed and range of a fixed-wing aircraft. DevelopmentWork on the Mono Tiltrotor (MTR) was initiated in 2004. A concept study was performed under an Office of Naval Research contract and this study concluded that the MTR, if technically realizable, would be half the size and one-third the weight of legacy helicopter concepts for a {{convert|1000|nmi|km|adj=on}} mission.[1] In 2005 and 2006, design of the 9400 pound gross weight MTR Scaled Demonstrator (MTR-SD) was performed under a United States Army contract at the US Army Research Laboratories.[2][3][4][5][6][7] This work included the following tasks: engine selection; transmission design; hub, controls, and blade preliminary design; comprehensive performance and aeroelastic analysis; analysis of critical stress concentrations; conceptual design of the fixed wing and cargo pod; wind tunnel testing of wing deployment;[8] and longitudinal static stability analysis from hover through cruise. This work resulted in a definition of each component's and each subassembly's weight, moments of inertia, location on the aircraft, and aerodynamic drag. The predicted range and speed were derived from this aircraft design data. In 2007 and 2008, demonstrations and validations of the MTR-SD design were performed under an Army contract.[9][10][11][12] The three unprecedented hardware mechanisms of the MTR were demonstrated in small scale flight tests: 1) the aerodynamically deployed wing panels; 2) the pitch axis suspended cargo pod; and 3) the tilting centerline rotor. Furthermore, a {{convert|7|ft|m|adj=on}} diameter rotor remote control MTR Functional Demonstrator (MTR-FD) that integrates these three features was designed, built, and hover tested.[13] Bell Helicopter Textron used proprietary methods for advanced concept design and analysis to validate the {{convert|25|ft|m|adj=mid|-diameter}} rotor MTR-SD design. Bell Helicopter's assessment resulted in validations of the MTR-SD vertical lift capacity, engine power required and power available, cruise thrust and propulsive efficiency, aircraft weight, and airplane mode cruise lift. Bell Helicopter also generated and reported MTR-SD flight dynamics data. A computational fluid dynamics drag assessment was performed, and in combination with the Bell Helicopter assessment this validated MTR-SD projected drag and aircraft cruise range performance.[9] In early 2009, a Concept of Operations (CONOPS) video was produced showing the MTR-SD performing the missions specified in the United States Marine Corps - Cargo Unmanned Aircraft System - Universal Need Statement (USMC Cargo UAS UNS)[14] and in the Office of Naval Research – Cargo Unmanned Aircraft System – Request for Information (ONR Cargo UAS RFI).[15][16] In early 2010, under a multi-year contract with the Office of Naval Research (ONR),[17] the CONOPs and aircraft design were refined for Navy shipboard compatibility.[18] On October 2, 2010, the first full conversion between helicopter and airplane modes of flight was achieved using a revised Mono Tiltrotor - Functional Demonstrator (MTR-FD), 4 foot diameter, small-scale remote control model.[19] Specifications{{aircraft specs|ref= Baldwin Technology Company, LLC.[20] |prime units?=imp |crew= 0 |capacity= |length m= |length ft=24 |length in= |span m= |span ft=33 |span in= |width m= |width ft= |width in= |height m= |height ft=12.5 |height in= |wing area sqm= |wing area sqft= 165 |wing area note= |aspect ratio= |empty weight kg= |empty weight lb=4900 |gross weight kg= |gross weight lb=9400 |wing loading lb/sqft= |wing loading note= |payload lb=3000 |eng1 number=1 |eng1 name=LHTEC T800 |eng1 type= turboshaft engine |eng1 kn= |eng1 lbf= |eng1 kn-ab= |eng1 lbf-ab= |max speed kmh= |max speed mph= |cruise speed kmh= |cruise speed mph=230 |range km= |range miles= |endurance= |ceiling m= |ceiling ft= |climb rate ms= |climb rate ftmin= |armament1= |armament2= |armament3= |armament4= |armament5= |armament6= }} See also{{Aircontent|see also= |related= |similar aircraft=
|lists= }} References1. ^http://handle.dtic.mil/100.2/ADA428702 Leishman, J. G., Preator, R., Baldwin, G. D.,Conceptual Design Studies of a Mono Tiltrotor (MTR) Architecture, U.S. Navy Contract Number: N00014-03-C-0531, 2004. 2. ^http://www.baldwintechnology.com/MTR_AHS_Jan07.pdf {{Webarchive|url=https://web.archive.org/web/20081007162342/http://www.baldwintechnology.com/MTR_AHS_Jan07.pdf |date=2008-10-07 }} Baldwin, G. D., 'Preliminary Design Studies of a Mono Tiltrotor (MTR) with Demonstrations of Aerodynamic Wing Deployment', AHS International Specialists Meeting, Chandler, Arizona, January 23–25, 2007. 3. ^Mono Tiltrotor Design Underway 4. ^Baldwin, G. D., Mono Tiltrotor (MTR) Concept Evaluation, U. S. Army Contract Number: W911W6-04-D-0004-0001, RDECOM TR 06-D-40, DTIC Accession Number ADB324612, 2006. 5. ^The Mono-Tiltrotor Final Project Report, U.S. Army Research Laboratory: Vehicle Technology Directorate, June 16, 2006. 6. ^MTR FY 2005 Development Final Comprehensive Report, Eagle Aviation Technologies Incorporated, May 18, 2006. 7. ^“Cargo Mono Tiltrotor is Fine Tuned”. Flight International, June 3, 2007. 8. ^“Folding Tiltrotor in Tunnel Test”. Flight International, Nov. 4, 2006. 9. ^1 http://www.baldwintechnology.com/MTR_AHS_08.pdf Baldwin, G. D., 'Mono Tiltrotor (MTR) Validation Activities', Proceedings of the 64th Annual National Forum of the American Helicopter Society, Montreal, Canada, April 29 - May 1, 2008. 10. ^Baldwin, G. D., Mono Tiltrotor Validation Activities, U. S. Army Contract Number: W911W6-04-D-0004-0002, RDECOM TR 08-D-0069, July 2008. 11. ^Assessment of the Mono Tiltrotor Scaled Demonstrator, Contract No: BTC001, Bell Helicopter Textron Incorporated, January 23, 2008. 12. ^Mavriplis, D. J., Computational Drag Study for the Mono Tiltrotor Scaled Demonstrator (MTR-SD), March 2008. 13. ^http://www.aviationweek.com/aw/blogs/defense/index.jsp?plckController=Blog&plckScript=blogScript&plckElementId=blogDest&plckBlogPage=BlogViewPost&plckPostId=Blog%3A27ec4a53-dcc8-42d0-bd3a-01329aef79a7Post%3A5d1e6791-b57b-43ff-8b59-15f04ec92ea9 “Mono Tiltrotor makes progress, on a small scale”, Aviation Week Defense Technology Blog, May 12, 2008. 14. ^Universal Need Statement for The Cargo Unmanned Aircraft System (Cargo UAS), HQ USMC, August 27, 2008. 15. ^http://www.aviationweek.com/aw/blogs/defense/index.jsp?plckController=Blog&plckScript=blogScript&plckElementId=blogDest&plckBlogPage=BlogViewPost&plckPostId=Blog%3A27ec4a53-dcc8-42d0-bd3a-01329aef79a7Post%3A834278bd-47ba-48a2-ac28-3ce27639dd64 “VIDEO: Mono Tiltrotor as Cargo UAS”, Aviation Week Defense Technology, March 12, 2009. 16. ^http://news.cnet.com/8301-13639_3-10201662-42.html “Robot tiltrotor boxcar may fly Navy supply missions”, CNET News, March 21, 2009. 17. ^http://www.aviationweek.com/aw/generic/story_channel.jsp?channel=defense&id=news/BALDWIN.xml "Persistence Pays Off For Mono Tiltrotor Inventor", Aviation Week 171.16, October 26, 2009, page 64 18. ^http://www.baldwintechnology.com/MTR_AHS_10.pdf Baldwin, G. D., 'A Cargo UAS Design and CONOPs', Proceedings of the 66th Annual National Forum of the American Helicopter Society, Phoenix, Arizona, May 11–13, 2010. 19. ^http://www.baldwintechnology.com/deepdive.html, Full Conversion Flight Demo (2 minutes) 20. ^http://www.baldwintechnology.com/current-design/54-specifications.html Further reading
External links
3 : Tiltrotor aircraft|Abandoned civil aircraft projects of the United States|Aircraft with contra-rotating propellers |
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