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Bertrand U1

Posted on October 27, 2026 By

For many years, aviation engineers have known that propeller efficiency can be increased by placing it within an annular duct. However, the additional mass and aerodynamic drag of the duct often negate the efficiency gains of the propulsion system. Some designers sought to resolve this problem by turning part of the fuselage into an annular duct.

Table of Contents

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    • Early Aviation Innovations
    • The Unique Bertrand U1 Design
    • Technical Specifications
  • Image and diagram gallery of the Bertrand U1
    • How to cite this article:

Early Aviation Innovations

One such aircraft was the Bertrand U1 (Bertrand Unic 1) monoplane. Built in 1909, this French ‘tunnel’ aircraft had several unique features. A single 30 hp (22 kW) Unic engine drove two propellers, each installed at opposite ends of the 2-meter diameter tunnel.

The Unique Bertrand U1 Design

Aerodynamically, the aircraft featured a ‘canard’ configuration, equipped with an additional tail assembly. The ailerons were not installed on the wing (with a wingspan of 13.40 m), but rather on the tips of the forward control surface (PGO).

Technical Specifications

Modification Bertrand U1
Wingspan, m 13.40
Wing area, m2 40.00
Normal takeoff weight 461
Engine type 1 Piston engine Unic
Power, hp 1 x 30
Crew, crew members 1

Image and diagram gallery of the Bertrand U1

Bertrand U1
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Bertrand U1

How to cite this article:

APA: Bertrand U1 (). Bertrand U1. wp.archivoaereo.com. https://wp.archivoaereo.com/en/bertrand-u1-3/
VANCOUVER: Bertrand U1 [online]. wp.archivoaereo.com; [cited 2026-10-28]. Available at: https://wp.archivoaereo.com/en/bertrand-u1-3/
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Pioneer Light Aircraft Tags:French

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