카만 K-맥스

Kaman K-MAX

국가 미국
역할 중형 리프트 헬리콥터
첫 비행 1991년 12월 23일
내장 Unknow

Tthe 카만 K-MAX (회사 명칭 K-1200)는 미국 제조업체 인 Kaman Aircraft가 설계하고 생산 한 인터 메싱 로터 (싱크로 옵터)가있는 헬리콥터입니다.

소스: Kaman K-MAX ― 위키피디아
Kaman K 1200 K-Max
사진 작가 Unknow
로컬라이제이션 우아 (우아)
사진 100
잠깐, 당신을 위해 Kaman K-MAX를 검색 ...

커피 사줘커피 사줘

Kaman K MAX HELICOPTER T-Shirt - Amazon

참고 항목:

World War II: The Definitive Visual History from Blitzkrieg to the Atom Bomb(DK Definitive Visual Histories) - 아마존 지도별 제2차 세계 대전 지도(DK History Map by Map) - 아마존


General Characteristics

The Kaman K-MAX is a unique, single-seat, twin-rotor helicopter specifically designed for repetitive external cargo lift operations, essentially functioning as an “aerial truck.” Its key design feature is the use of intermeshing, counter-rotating rotors (a synchropter configuration), which eliminates the need for a tail rotor, directing all engine power to vertical lift.

Property Typical Value (K-1200)
역할 External Cargo Lift / Aerial Crane
제조업체 Kaman Aircraft
First Flight 1991년 12월 23일
승무원 1 pilot (single seat)
Max Takeoff Weight (with external load) 5,443 kg (12,000 lb)
Empty Weight 2,334 kg (5,145 lb)
Rotor Diameter (Each) 14.73 m (48 ft 4 in)
Overall Length (Rotors Turning) 15.85 m (52 ft 0 in)

Design and Powerplant

  • Engine: One Honeywell T53-17A-1 turboshaft engine.
  • Power Output: Flat-rated to approximately 1,007 kW (1,350 shp) for long life and high-altitude performance, with a thermodynamic rating of 1,800 shp.
  • Rotor System: Twin, counter-rotating, intermeshing main rotors (synchropter). This design cancels torque without a tail rotor, making the aircraft highly efficient for lift.
  • Cargo Hook Capacity: 2,722 kg (6,000 lb). The helicopter’s lift capacity is greater than its empty weight.
  • Control System: Features a unique servo-flap control system on the rotor blades, eliminating complex hydraulics from the main flight controls (though later variants use a blend of systems).
  • Pilot Visibility: Designed with a narrow, wedge-shaped fuselage and large side windows to provide the pilot with an excellent downward view for precision external load placement (vertical reference flight).

Performance and Applications

  • Max Speed (Without External Load): 185 km/h (100 knots, 115 mph).
  • Max Speed (With External Load): 148 km/h (80 knots, 92 mph).
  • Service Ceiling: 4,572 m (15,000 ft).
  • Max Range (Normal): Approximately 480 km (300 nautical miles).
  • Operating Efficiency: Known for its efficiency, requiring less than two maintenance man-hours per flight hour and having a low fuel consumption rate for its lift capacity.
  • Unmanned Capability: The K-MAX has been successfully deployed as an unmanned aircraft system (UAS) for autonomous cargo delivery, including for military resupply missions.
  • Typical Applications: Logging, construction (setting utility poles, towers, HVAC units), firefighting (FireMax variant with fixed tank), and military resupply.

조회수 : 540

답을 남겨주세요

<a href="" title=""> <abbr title=""> <acronym title=""> <b> <blockquote cite=""> <cite> <code> <del datetime=""> <em> <i> <q cite=""> <s> <strike> <strong> 

필수

이 사이트는 Akismet를 사용하여 스팸을 줄입니다. 댓글 데이터가 처리되는 방법 알아보기.