Internal compression supersonic engine inlet

Fluid handling – Processes – Cleaning – repairing – or assembling

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

244 53B, B64D 3302

Patent

active

058817581

ABSTRACT:
An internal compression engine inlet (39) including a flexible external cowl with leading edge cowl lips (72); a duct comprising a supersonic diffuser (44) defined by upper and lower forward ramps (50), (52), a subsonic diffuser (46) defined by upper and lower aft ramps (54), (56), and a throat region (48); a first slot (58) formed between adjacent ends of the upper forward and upper aft ramps; and a second slot (60) formed between adjacent ends of the lower forward and lower aft ramps, is provided. Each slot (58), (60) opens to a plenum (120), (122) having a vent door (126) covering a vent (124) that opens to a low pressure volume. Further inlet components include an optional splitter (62) for creating additional airflow compression, a precision vent (128) for expelling small amounts of plenum air, and a control system (150) for varying the cross-sectional area of the duct and the position of the vent doors in order to create an aerodynamically efficient airflow passage within the duct for any particular flight condition. Further provided is a method of providing air to an aircraft engine using an internal compression engine inlet including: sensing current flight conditions; configuring the inlet components to their optimal positions for the current flight conditions; channeling air into a duct having a supersonic diffuser region followed by a throat region having first and second slots each slot opening into a plenum, the throat region being followed by a subsonic diffuser; sensing the static air pressure in the supersonic diffuser; sensing the static air pressure within each plenum; comparing the supersonic diffuser static air pressure with the plenum air pressures; and selectively exhausting air from each plenum to maintain the static air pressure in the plenums at a desired amount.

REFERENCES:
patent: 2989846 (1961-06-01), Hausammann
patent: 3032977 (1962-05-01), Neitzel
patent: 3430640 (1969-03-01), Lennard
patent: 3450141 (1969-06-01), Braendlein
patent: 3643676 (1972-02-01), Limage et al.
patent: 3941336 (1976-03-01), Nangia
patent: 4307473 (1981-12-01), Dunn
patent: 4641678 (1987-02-01), Haas et al.
patent: 4991795 (1991-02-01), Koncsek
patent: 5033693 (1991-07-01), Livingston et al.
patent: 5078341 (1992-01-01), Bichler et al.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Internal compression supersonic engine inlet does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Internal compression supersonic engine inlet, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Internal compression supersonic engine inlet will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-809290

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.