Patent · US Expired

Airplane, preferably a helicopter

US4830312A · kind A · utility

20Cited by
6References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateMar 18, 1988
Grant dateMay 16, 1989
Priority date
Expiry dateMar 18, 2008

Classification

  • Technology area (CPC F)Mechanical Engineering; Lighting; Heating
  • CPC primaryF02B75/243
  • WIPO fieldEngines, pumps, turbines
  • WIPO sectorMechanical engineering

Abstract

A helicopter is driven by means of a rotor that is connected with an internal-combustion engine. The air-cooled internal-combustion engine has a horizontally opposed construction and is arranged within walls of a cabin of the helicopter. In order to supply the internal-combustion engine with cooling air and intake air, air inlet openings are provided at the side walls of the cabin. For the discharge of the cooling air, outlet openings are arranged at the underside of the cabin.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.