Bristol Sycamore | |
|---|---|
| Riik | Uk |
| Rolli | Pääste- ja allveelaevade helikopter |
| Esimene lend | 27. juuli 1947 |
| Ehitatud | 180 |
2007 Bristoli tüüp 171 Sycamore oli varajane helikopter, mille töötas välja ja ehitas Bristoli lennukikompanii helikopteridivisjon. Nimi viitab sükamoripuu Acer pseudoplatanus seemnetele, mis langevad pöörleva liikumisega. Selle eripära on see, et see on esimene Briti helikopter, mis sai lennukõlblikkussertifikaadi, samuti on see esimene Briti projekteeritud helikopter, mille tutvustavad kuninglikud õhujõud (RAF) ja mis teenib koos nendega.
Allikas: Bristol Sycamore Vikipeedias
| Bristol Type 171 Sycamore HC 14 Walk Around | |
|---|---|
| Fotograaf | Teadmata |
| Lokaliseerimine | Teadmata |
| Fotod | 16 |
Bristol Type 171 Sycamore HC 14 1
Bristol Type 171 Sycamore HC 14 2
Bristol Type 171 Sycamore HC 14 3
Bristol Type 171 Sycamore HC 14 4
Bristol Type 171 Sycamore HC 14 5
Bristol Type 171 Sycamore HC 14 6
Bristol Type 171 Sycamore HC 14 7
Bristol Type 171 Sycamore HC 14 8
Bristol Type 171 Sycamore HC 14 9
Oota, otsides Bristol Sycamore'i sinu jaoks ...
| Bristol 171 Sycamore Mk.52 Walk Around | |
|---|---|
| Fotograaf | Teadmata |
| Lokaliseerimine | Teadmata |
| Fotod | 21 |
Bristol 171 Sycamore Mk.52 1
Bristol 171 Sycamore Mk.52 3
Bristol 171 Sycamore Mk.52 2
Bristol 171 Sycamore Mk.52 4
Bristol 171 Sycamore Mk.52 6
Bristol 171 Sycamore Mk.52 5
Bristol 171 Sycamore Mk.52 7
Bristol 171 Sycamore Mk.52 8
Bristol 171 Sycamore Mk.52 9
Vaata ka:
Oota, otsides helikopterit sinu jaoks ...
General Characteristics
The Bristol Type 171 Sycamore was the first British-designed helicopter to receive a civil certificate of airworthiness and to enter service with the Royal Air Force (RAF).
| Property | Value (Mk.4 / HR14 Variant) |
|---|---|
| Rolli | Light Utility, Search and Rescue (SAR), Casualty Evacuation (CASEVAC) |
| Tootja | Bristol Aeroplane Company |
| First Flight | July 24, 1947 |
| Meeskonna | 2 pilots |
| Passenger/Troop Capacity | Up to 3 passengers/troops (or 2 stretchers) |
| Maximum Take-Off Weight | 2,540 kg (5,600 naela) |
Engine and Rotor System
- Powerplant: One Alvis Leonides 9-cylinder radial piston engine.
- Engine Position: Mounted horizontally behind the main cabin, driving the rotor system.
- Power Output: Approximately 410 kW (550 hp).
- Main Rotor: 3-blade, fully articulated main rotor with blades made of wood (often Australian maple). The blades could be folded for space-saving storage on ships.
- Tail Rotor: 3-blade anti-torque rotor.
Performance and Service
- Maximum Speed: 204 km/h (127 mph)
- Range: Up to 532 km (330 miles)
- Service Ceiling: 4,877 m (16,000 ft)
- Key Service: Used by the RAF and militaries of Australia and Germany. It proved vital in conflicts like the Malayan Emergency for troop insertion and medical transport over challenging terrain.
Vaadatud : 1024
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