The Sikorsky X2 is an experimental high-speed compound helicopter with coaxial rotors, developed by Sikorsky Aircraft, that made its first flight in 2008 and was officially retired in 2011.
X2 | |
---|---|
Sikorsky X2 Demonstrator | |
Role | Experimental compound helicopter |
Manufacturer | Sikorsky Aircraft / Schweizer Aircraft |
First flight | 27 August 2008[1] |
Retired | 14 July 2011 |
Status | Retired |
Number built | 1 |
Design and development
editSikorsky developed the X2 helicopter on a $50 million budget. The design includes expertise gathered from several earlier design projects. The S-69/XH-59A Advancing Blade Concept Demonstrator had shown that high speed was possible with a coaxial helicopter with auxiliary propulsion supplied using two jet engines, but that vibration and fuel consumption was excessive;[2][3][4] the Cypher UAV expanded the company's knowledge of the unique aspects of coaxial flight control laws with a fly-by-wire aircraft; and the RAH-66 Comanche developed expertise in composite rotors and advanced transmission design.[5][6]
Other features include slowed[7] "de-swirling"[8] rigid rotors two feet apart, active force counter-vibration inspired by the Black Hawk,[9] and using most of the power in forward flight for the pusher propeller rather than the rotor.[2] Unusually for helicopters, the power required for high speed is more than the hover power. The pilot controls the independent propeller power with a thumb wheel on the collective.[10]
Test flights and flight simulations were combined to improve test procedure.[11][12] The fly-by-wire system is provided by Honeywell, the rotor by Eagle Aviation Technologies, anti-vibration technology from Moog Inc, and propeller by Aero Composites.[13] The rotor hub can have 10-20 times the drag of the blade.[14] Sikorsky intended to test hub fairings to reduce drag by 40%,[15] and test flew fairings on the hubs themselves but not the central hub fairing ("aero sail") in between the hubs.[16] Sikorsky has since patented a "Standpipe" (fixed tube between rotating rotor axes) suitable for a central hub fairing.[17]
On 4 May 2009, Sikorsky unveiled a mockup of a Light Tactical Helicopter derivative of the X2,[18] and unveiled a prototype in October 2014.[19][20][21]
In June 2014, Sikorsky/Boeing submitted the SB-1 Defiant helicopter design for the Future Vertical Lift program based on the X2 principle,[22][23] which was approved by the Army in October.[24]
Operational history
editThe X2 first flew on 27 August 2008 from Schweizer Aircraft, a division of Sikorsky Aircraft Corporation's facility at Horseheads, New York. The flight lasted 30 minutes.[1] This began a four-phase flight test program, to culminate with reaching a planned 250-knot top speed.[25] The X2 completed flights with its propeller fully engaged in July 2009.[26] Sikorsky completed phase three of the testing with the X2 reaching 181 knots in test flight in late May 2010.[27]
On 26 July 2010, Sikorsky announced that the X2 exceeded 225 knots (259 mph; 417 km/h) during flight testing in West Palm Beach Florida, unofficially surpassing the current FAI rotorcraft world speed record of 216 knots (249 mph; 400 km/h) set by a modified Westland Lynx in 1986.[28][29]
On 15 September 2010, test pilot Kevin Bredenbeck achieved Sikorsky's design goal for the X2 when he flew it at a speed of 250 knots (290 mph; 460 km/h) in level flight,[30][31] an unofficial speed record for a helicopter.[2][32] The demonstrator then reached a new record speed of 260 knots (300 mph; 480 km/h) in a shallow 2˚ to 3˚ dive,[33] which was just short of the 303 mph achieved by the Sikorsky S-69 technology demonstrator helicopter.[34] Sikorsky states that the X2 has the same noise level at 200 knots that a regular helicopter has at 100 knots. Above 200 knots, the rotor speed is reduced from 446 to 360 RPM[35][36] to keep tip speed below Mach 0.9, the rotor disc is slightly nose-up, and the lift-to-drag ratio is about twice that of a conventional helicopter. Hands-off flying was also successfully performed during flight tests.[37]
On 14 July 2011, the X2 completed its final flight and was officially retired after accumulating 22 hours over 23 test flights.[38][39] With the end of development, the X2 will be followed by its first application, the S-97 Raider high-speed scout and attack helicopter.[40] It was donated to the National Air and Space Museum in October 2016 and is on display in the Steven F. Udvar-Hazy Center in Chantilly, Virginia.[41][42]
Awards
editThe Sikorsky Aircraft Corporation and the X2 Technology Demonstrator Team was awarded the 2010 Robert J. Collier Trophy by the National Aeronautic Association[43][44] "...For demonstrating a revolutionary 250 knot helicopter, which marks a proven departure point for the future development of helicopters by greatly increasing their speed, maneuverability and utility." For 2011, the X2 team received the Howard Hughes Award (American Helicopter Society).[45]
Specifications
editData from Flug-Revue[13] NOTE: No other specifications have been released by Sikorsky.
General characteristics
- Crew: Two
- Aspect ratio: 9.5
- Empty weight: 5,300 lb (2,404 kg) [41]
- Gross weight: 6,000 lb (2,722 kg) [46][47][48]
- Max takeoff weight: 5,300 lb (2,404 kg) [36][49]–6,000 lb (2,700 kg)[citation needed]
- Powerplant: 1 × LHTEC T800-LHT-801 turboshaft, 1,800 shp (1,300 kW)
- Main rotor diameter: 2 × 26 ft 5 in (8.05 m)
- Main rotor area: 548 sq ft (50.9 m2) contra-rotating four-bladed coaxial.[36][50]
- Propellers: 6-bladed pusher
Performance
- Maximum speed: 290 mph (460 km/h, 250 kn) [51]
- Range: 35 mi (56 km, 30 nmi)
- Wing loading: 0.44 lb/sq ft (2.1 kg/m2)
- Power/mass: 3.66 hp/lb[36]
See also
editRelated development
Aircraft of comparable role, configuration, and era
Related lists
References
edit- ^ a b Trimble, Stephen. "Sikorsky's X2 speedster completes first flight". Flightglobal.com, 27 August 2008.
- ^ a b c Goodier, Rob (September 20, 2010). "Inside Sikorsky's Speed-Record-Breaking Helicopter Technology". Popular Mechanics. Retrieved 22 September 2010.
- ^ Thomas Lawrence; David Jenney (31 Aug 2010). "The Fastest Helicopter on Earth". IEEE Spectrum. Archived from the original on 30 January 2017. Retrieved 1 August 2017.
the helicopter vibrated so much at these higher speeds that its pilots struggled to control it .. The heavy and fuel-hungry jets pushed the aircraft to high speed
- ^ XH-59A / X2 comparison IEEE
- ^ Sikorsky to Build and Test X2 Technology Demonstrator Helicopter Archived July 14, 2008, at the Wayback Machine. Sikorsky
- ^ Trimble, Stephen (26 July 2010). "Sikorsky X2 sets unofficial helicopter speed record". FlightGlobal. Reed Business Information. Retrieved 29 July 2010.
- ^ First Flight Of Sikorsky X2 Demonstrator, Archived March 7, 2012, at the Wayback Machine Aviation Week & Space Technology, 27 August 2008. Accessed: 9 March 2012. Archived on 7 March 2012.
- ^ Chandler, Jay. "Advanced rotor designs break conventional helicopter speed restrictions (page 1) Archived July 18, 2013, at the Wayback Machine" Page 2 Archived July 18, 2013, at the Wayback Machine Page 3 Archived 2013-07-18 at the Wayback Machine. ProPilotMag, September 2012. Accessed: 10 May 2014. Archive 1 Archive 2
- ^ X2 marks the spot for radical rotor designs, Flightglobal.com, 12 June 2007.
- ^ Fell, William (April–May 2018). "X2 From the Pilot's View". digitaledition.rotorandwing.com. Archived from the original on 8 May 2019.
- ^ Wilson, J.R. "Defense Interview: Mark Miller" Defense Media Network, 9 September 2011. Accessed: 4 October 2014. Archived on 2 November 2012.
- ^ "Sikorsky Innovations Introduces X2 Technology™ Light Tactical Helicopter Simulator" Sikorsky PR
- ^ a b "Sikorsky X2". Flug-Revue. Archived from the original on June 12, 2008. Retrieved 2007-06-25.
- ^ Harris, Franklin D. "Rotor Performance at High Advance Ratio: Theory versus Test Archived 2013-02-18 at the Wayback Machine" page 119 NASA/CR—2008–215370, October 2008. Accessed: 13 April 2014.
- ^ Croft, John (20 May 2010). "Sikorsky X2 breaks helicopter speed barrier". Flightglobal. Reed Business Information. Archived from the original on 28 May 2015. Retrieved 28 May 2015.
- ^ Dubois, Thierry (26 July 2011). "AgustaWestland". Aviation International News. Archived from the original on 11 October 2014. Retrieved 28 May 2015.
- ^ US 20150125299 "Counter-rotating Rotor System With Stationary Standpipe" PDF
- ^ Trimble, Stephen. Sikorsky unveils mock-up X2 armed scout. Flightglobal.com, 4 May 2009.
- ^ S-97 Rollout Archived 2014-10-04 at the Wayback Machine video Sikorsky
- ^ Parsons, Dan (2 October 2014), "Sikorsky rolls-out high-speed Raider rotorcraft", Flightglobal, Reed Business Information, retrieved 3 October 2014
- ^ Warwick, Graham. "Sikorsky Talks To Customers About Potential Raider Applications" Aviation Week & Space Technology, 6 October 2014. Accessed: 3 October 2014. Photos Archived on 3 October 2014
- ^ Majumdar, Dave. "Sikorsky and Boeing Team Submit New Army Helicopter Design" - News.USNI.org, 17 June 2014. Accessed: 19 June 2014. Archive
- ^ Sikorsky and Boeing to pitch ‘X-2’-based design for US Army JMR TD effort - Flightglobal.com, February 28, 2013
- ^ U.S. Army Selects Bell and Sikorsky/Boeing to Build Prototypes for Next Generation Helicopter Program - News.USNI.org, 3 October 2014
- ^ Trimble, Stephen. "Sikorsky high-speed X2 prototype starts flight-test phase". Flight International, 2 September 2008.
- ^ Lynch, Kerry. "Sikorsky X2 Flies With Engaged Propeller"[permanent dead link] Aviation Week, 13 July 2009. Paywall
- ^ Croft, John. "Sikorsky completes third-phase X2 tests with 181kt flight". Flight International, 27 May 2010.
- ^ "Rotorcraft Absolute: Speed over a straight 15/25 km course Archived 2013-12-03 at the Wayback Machine". Fédération Aéronautique Internationale (FAI). Note search under E-1 Helicopters and "Speed over a straight 15/25 km course". Accessed: 26 April 2014.
- ^ "X2 Technology Demonstrator Achieves 225 Knots, Sets New Top Speed for Helicopter - Target Milestone of 250 Knots Looms in Q3 2010". UTC.com, 15 June 2015.
- ^ Croft, John (September 15, 2010). "Sikorsky X2 hits 250kt goal". Flight International. Retrieved 2010-09-16.
- ^ Varnon, Rob (May 26, 2010). "Sikorsky's X2 chases world speed record". Connecticut Post.
- ^ "Sikorsky X2 Technology Demonstrator Achieves 250-Knot Speed Milestone". sikorsky.com. 15 September 2010. Archived from the original on 14 October 2013. Retrieved 23 September 2010.
- ^ Finnegan, Joy editor-in-chief (1 October 2010). "Sikorsky Breaks 250 KTAS Record". Rotor & Wing. Archived from the original on 31 October 2010. Retrieved 6 October 2010.
{{cite web}}
:|author=
has generic name (help) - ^ Robb, Raymond L. Hybrid Helicopters: Compounding the Quest for Speed[permanent dead link] p49, Vertiflite, Summer 2006. Quote: "Ultimately, the XH-59A achieved an incredible 303 mph"
- ^ Datta, Anubhav et al. Experimental Investigation and Fundamental Understanding of a Slowed UH-60A Rotor at High Advance Ratios, page 2. NASA, 2011. Accessed: April 2014.
- ^ a b c d Jackson, Dave. "Coaxial - Sikorsky ~ X2 TD" Unicopter, 18 September 2010. Accessed: April 2014. Archived on 13 September 2013.
- ^ D. Walsh, S. Weiner, K. Arifian, T. Lawrence, M. Wilson, T. Millott and R. Blackwell. "High Airspeed Testing of the Sikorsky X2 Technology Demonstrator[permanent dead link]" Sikorsky, May 4, 2011. Accessed: October 5, 2013.
- ^ Paur, Jason (15 July 2010). "Sikorsky's Record-Setting Helicopter Retires". WIRED. Retrieved 15 July 2011.
- ^ "Sikorsky X2 rotorcraft prototype makes final flight after proving technology for S-97 scout/attack helicopter". www.militaryaerospace.com. 17 July 2011.
- ^ "Award-Winning X2 Technology Demonstrator Takes its Final Flight - Program paved the way for upcoming S-97 Raider helicopter", Sikorsky Aircraft Corp., 14 July 2011.
- ^ a b Connor, Roger (25 October 2016). "Sikorsky X2 Helicopter Reaching New Speeds". National Air and Space Museum. Archived from the original on 16 May 2020. Retrieved 5 December 2016.
Weight, empty: 2,404 kg (5,300 lb)
- ^ "Sikorsky X2 joins Smithsonian collection". Helicopter Association International. Helicopter Association International. 28 October 2016. Retrieved 5 December 2016.
- ^ Warwick, Graham. "Sikorsky's X2 - Collier Win, Commercial Next?" Aviation Week, Mar 16, 2011. Accessed: March 8, 2014. Archive Archived March 9, 2014, at the Wayback Machine
- ^ Larson, George. "Sikorsky's X2 and the Collier Trophy Archived 2014-03-09 at the Wayback Machine" Aviation Week, Mar 23, 2011. Accessed: March 8, 2014.
- ^ "Howard Hughes Award", American Helicopter Society
- ^ Johnson, Wayne (January 18–20, 2012). "Design and Performance of Lift-Offset Rotorcraft for Short-Haul Missions" (PDF). NASA. p. 4.
nominal gross weight of 5950 lb.
- ^ Drew, James (2016-02-19). "ANALYSIS: Sikorsky seeks next leap in rotorcraft technology". Flight Global. Archived from the original on 30 August 2020.
We started with [the] X2 technology demonstrator at about 6,000lbs (2.7t) gross weight.
- ^ Walsh, D (January 2011). "High airspeed testing of the Sikorsky X2 Technology™ demonstrator".
- ^ Tomkins, Richard. "Sikorsky powers on S-97 avionics" United Press International, 17 June 2014. Accessed: 19 June 2014. Archived on 18 June 2014.
- ^ Note: this is the disc area of one rotor set, not the effective area of the whole coaxial rotors set.
- ^ "Sikorsky X2 Technology™ Demonstrator Achieves 250-Knot Speed Milestone".
External links
editExternal videos | |
---|---|
Official Sikorsky X2 videos | |
- Sikorsky X2 company page Archive from 2009
- Sikorsky X2 (proposed) on unicopter.com (patent list at the bottom)
- "Sikorsky Calls X2 Shape of the Future", Aviation Week, 25 February 2008 Archived 7 March 2012 at the Wayback Machine
- "Sikorsky X2 In Blades-On Ground Tests", Aviation Week, 21 May 2008 Archived 7 March 2012 at the Wayback Machine
- "Hyper Helos: Prototypes coming off the drawing board and into the race", Flight International, 3 July 2008
- "Swamp Pirates", Aircraft Owners and Pilots Association, October 1, 2011
- Sikorsky X-2 at the Stuart Air Show, Nov 11, 2011