Platt-LePage XR-1

XR-1
XR-1
Role Experimental helicopter
Manufacturer Platt-LePage Aircraft Company
First flight May 12, 1941
Retired June 21, 1946
Primary user United States Army Air Forces
Number built 2

The Platt-LePage XR-1, also known by the company designation PL-3,[1] is an early American transverse rotors helicopter, built by the Platt-LePage Aircraft Company of Eddystone, Pennsylvania. The winner of a United States Army Air Corps design competition held in early 1940, the XR-1 was the first helicopter tested by the USAAF, flying in 1941. The flight testing of the XR-1 proved troublesome, and although continued testing showed that the design had promise, other, improved helicopters were becoming available before the XR-1 was ready for service. As a result, the development of the aircraft was terminated in 1945.

Design and development

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Developed during 1939 from an earlier, unsuccessful design, the PL-1,[2] the Platt-LePage Model PL-3 was the winner of a 1940 design competition, held under the terms of the Dorsey-Logan Act, for the supply of a helicopter design to the United States Army Air Corps.[3] Platt-LePage's submission was judged by the Army to be superior to its competitors, which included a helicopter submitted by Vought-Sikorsky, and autogyros developed by Kellett and Pitcairn.[N 1]

Following the selection of the Platt-LePage design in May 1940, a contract for the construction of a prototype and a static test airframe was issued in July of that year.[1] The contract specified delivery of the flying prototype in January 1941, however the aircraft was not completed until three months later than the contract schedule,[1] a delay that led to Sikorsky receiving Dorsey-Logan Act funding for development of its design, which became the XR-4.[4]

XR-1 early in testing

In its design, the XR-1 bore a strong resemblance to the Focke-Wulf Fw 61, a helicopter developed by Henrich Focke in Germany that, flown by Hanna Reitsch, had impressed Platt-LePage co-founder Wynn LePage during a tour of Europe.[5] The XR-1 was powered by a Pratt & Whitney R-985 radial engine, mounted in a buried installation within the fuselage.[1] The aircraft had two, three-bladed rotors, mounted in a side-by-side arrangement on wing-like pylons.[1] The pylons were aerodynamically designed to produce some lift when in forwards flight, slightly unloading the rotors.[6] The construction of the XR-1 was conventional by the standards of the time, with the aircraft's frame consisting of a steel-tube framework, which was covered with fabric.[1] The XR-1 had tail surfaces similar to those of a conventional aircraft, and was equipped with a fixed, taildragger landing gear.[1] The aircraft's wheels freely castered for easier maneuvering on the ground.[6]

The cockpit of the XR-1 seated the aircraft's two crew members in a tandem arrangement, the pilot located ahead of the observer, and was extensively glazed to provide good visibility in the aircraft's intended observation and army co-operation role.[1] During the development of the aircraft, Major General Robert M. Danford proposed to the War Department that the XR-1 be evaluated against the Stinson YO-54 and the Kellett YG-1B autogyro.[7]

Operational history

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Following several months of ground testing, the XR-1 conducted its maiden flight on May 12, 1941, although the aircraft was restrained by a tether for its early flights.[8] On June 23 the aircraft conducted its first free flight, albeit remaining within a few feet of the ground.[8] As flight testing continued and the aircraft's performance envelope was expanded, the XR-1's quickly proved troublesome, the testing showing a variety of troubles with the design.[8] These included issues with the aircraft's controls, insufficient control authority being present, and in addition there were resonance issues with the airframe[9] that made the XR-1 prone to pilot-induced oscillations.[8] The aircraft was modified in an attempt to resolve these issues, and the Army modified Platt-LePage's contract to provide additional funding for improvements to the design, but despite this the XR-1's problems continued.[8] In addition, the company's test pilot, Lou Leavitt, lacked confidence in the design, refusing to fly the aircraft to its full potential.[6] The situation was only resolved when Colonel H. Franklin Gregory, director of rotor-wing projects for the Army Air Forces, flew the aircraft himself, reaching 100 mph (160 km/h) on his first flight in the aircraft.[6]

XR-1top view

With the worst of the aircraft's problems believed to have been resolved, the XR-1 was submitted for service testing by the Army Air Forces in 1943.[8] During the course of the Army's evaluations, the XR-1's empennage failed during structural testing, the surfaces being strengthened as a result and testing, following the repairs, resuming in 1944.[8] Despite the modifications to the design, however, the XR-1 still proved to be deficient in control authority.[8] In July 1943, the XR-1 program suffered a setback when the aircraft crashed, seriously injuring test pilot Jim Ray, who had replaced Leavitt following the latter's dismissal from the company.[6] The crash was caused by an inspector's error in leaving a suspect part on the aircraft, the rotor hub failing in flight as a result of the decision.[6] The aircraft was repairable, but it would be a year before the XR-1 was ready to fly again.[6]

Testing was, however, able to continue in the meantime, as Platt-LePage had re-negotiated the XR-1 contract to cover a second flight-test aircraft.[6] Built to a revised and improved version of the XR-1's design and designated XR-1A, the second aircraft had flown for the first time in May 1943.[8] The XR-1A featured a revised cockpit covering compared to that of the XR-1, with the area of glazing being increased for improved visibility, and the pilot and observer's positions being reversed, the pilot now seated in the rear cockpit.[8] During flight testing the XR-1A was found superior in flight performance to the XR-1;[8] however, the controls were still proving troublesome,[8] although the worst of the bugs did seem to have been worked out.[6]

Following a cross-country flight to Wright Field in Ohio from Platt-LePage's Pennsylvania plant, testing of the XR-1A continued until a mechanical failure in the rotor hub led to a crash landing[6] on 26 October 1944,[8] the company deciding to sell the wreckage for scrap.[6]

The XR-1, having been repaired in the meantime, was once again flying,[6] and a contract had been awarded to Platt-Lepage for the construction of seven pre-production aircraft, to be built to an improved version of the XR-1A design, and designated YR-1A.[10] Motivated by Congressional concerns about potential favouritism towards Sikorsky Aircraft, which had in the meantime been given a contract for development of an improved version of their VS-300 experimental helicopter, the contract called for delivery of the first YR-1A to the Army in January 1945.[10] However, due to continued financial and flight-testing problems, Platt-Lepage proved incapable of meeting this schedule.[10]

Although the XR-1's problems seemed to be approaching resolution by late 1944,[11] the protracted development of the aircraft meant that alternative, improved helicopters, such as Sikorsky's XR-4, less expensive and more maneuverable than Platt-LePage's aircraft, were becoming available.[8] In addition, even the XR-1A's improvements had failed to cure the aircraft of all of its control and vibration problems,[6] and the AAF's Air Materiel Command considered the company "inept" in its work, applying a "hit-or-miss method" to research and development.[6] As a result of this assessment, the Army's contracts with the company were universally cancelled in early April 1945.[8]

Following the cancellation of the Army's contract, the XR-1 was returned to the company, Platt-LePage believing that the design had potential as a civilian aircraft.[8] The planned civilian version, the PL-9, would have been an enlarged, twin-engined aircraft;[6] however Platt-LePage was by now in serious financial difficulty following the cancellation of its Army contract,[8] and in mid 1946 the XR-1's flight test program was concluded,[6] the aircraft being retired to the Smithsonian Institution.[8]

In the meantime, the company's former test pilot, Lou Leavitt, had purchased the wreckage of the XR-1A at a price of 4 cents per pound.[6] Leavitt was a pilot with Helicopter Air Transport,[6] which was providing helicopter services in anticipation of a postwar aviation boom, and the XR-1A was returned to flying condition.[10] The projected boom failed to materialise, however, and HAT quickly entered bankruptcy, selling the XR-1A to Frank Piasecki, another former Platt-LePage employee who had now started his own helicopter company.[6] Leavitt flew the helicopter to Piasecki, who never flew it due to airworthiness concerns, and used the airframe in the development of the PA-2B, a planned tiltrotor which failed to proceed beyond the mock-up stage.[6]

Surviving aircraft

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Following the conclusion of flight testing, the XR-1 was returned to the Army Air Forces, who placed the aircraft in storage before donating it to the Smithsonian Institution's National Air and Space Museum.[6] The unrestored aircraft is stored at the Paul Garber Restoration and Storage Facility in "remarkable condition".[6]

Variants

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XR-1
First prototype; one built.[1]
XR-1A
Second prototype with increased cockpit glazing and improved engine; one built.[8]
YR-1A
Seven pre-production aircraft ordered; contract cancelled before any completed.[10]
Piasecki PA-2B
Proposed tiltrotor based on XR-1 airframe; not built.[6]

Operators

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 United States
United States Army Air Forces

Specifications (XR-1A)

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XR-1A

Data from Connor and Lee 2000; Lambermont 1958

General characteristics

  • Crew: Two (Pilot and observer)
  • Length: 29 ft 4 in (8.94 m)
  • Wingspan: 65 ft 0 in (19.81 m)
  • Height: 9 ft 0 in (2.74 m)
  • Gross weight: 4,730 lb (2,145 kg)
  • Powerplant: 1 × Pratt & Whitney R-985-AN-1 radial piston engine, 450 hp (340 kW)
  • Main rotor diameter: 2 × 31 ft 6 in (9.60 m)

Performance

  • Maximum speed: 110 mph (177 km/h, 96 kn)
  • Disk loading: 4.1 lb/sq ft (19.9 kg/m2)
  • Power/mass: 10.8 lb (4.9kg)/hp

See also

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Aircraft of comparable role, configuration, and era

Related lists

Notes

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  1. ^ Despite being rejected in favour of the XR-1, the Vought-Sikorsky design would be developed into the Sikorsky VS-300, while Kellett's autogyro would be purchased for evaluation by the Army as the Kellett XR-2; Pitcairn's proposed design was the Picairn PA-36.[2]

References

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  1. ^ a b c d e f g h i Francillon 1990, p.49.
  2. ^ a b Charnov 2003, p.171.
  3. ^ Leishman 2006, p.32.
  4. ^ Pattillo 2000, p.142.
  5. ^ Francillon 1990, p.48.
  6. ^ a b c d e f g h i j k l m n o p q r s t u v w Connor and Lee 2000
  7. ^ Raines 2002, p.42.
  8. ^ a b c d e f g h i j k l m n o p q r s Francillon 1990, p.50.
  9. ^ Leishman 2006, p.33.
  10. ^ a b c d e Francillon 1990, p.51.
  11. ^ Collier and Thomas 1986, p.13.

Sources

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  • Charnov, Bruce H. (2003). From Autogiro to Gyroplane: The Amazing Survival of an Aviation Technology. Westport, CT: Praeger. ISBN 978-1-56720-503-9.
  • Collier, Larry; Kas Thomas (1986). How To Fly Helicopters (2nd ed.). Blue Ridge Summit, PA: Tab Books. ISBN 978-0-8306-2386-0.
  • Connor, Roger D.; Russell Lee (2000). "Platt-LePage XR-1". Smithsonian National Air and Space Museum. Archived from the original on 2011-04-02. Retrieved 2010-12-02.
  • Francillon, René J. (1990). McDonnell Douglas Aircraft since 1920: Volume II. Annapolis, MD: Naval Institute Press. ISBN 1-55750-550-0. Retrieved 2010-12-01.
  • Lambermont, Paul Marcel (1958). Helicopters and Autogyros of the World. London: Cassell. ASIN B0000CJYOA.
  • Leishman, J. Gordon (2006). Principles of Helicopter Aerodynamics. New York: Cambridge University Press. ISBN 0-521-85860-7.
  • Pattillo, Donald M. (2000). Pushing the Envelope: The American Aircraft Industry. Ann Arbor, MI: University of Michigan Press. ISBN 978-0-472-08671-9. Retrieved 2010-12-01.
  • Raines, Edgar F. Jr. (2002). Eyes of Artillery: The Origins of Modern U.S. Army Aviation in World War II. Honolulu, HI: University Press of the Pacific. ISBN 978-1-4102-0151-5. Retrieved 2010-12-01.
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